71
I DOE/NASA CONTRACTOR REPORT DOE/NASA CR-150830 PROTOTYPE SOLAR HEATING AND COOLING SYSTEMS (Monthly Progress Reports) Prepared from Documents furnished by AiResearch Manufacturing Company of California 2525 West 190th Street Torrance, California 90509 Under Contract NAS8-3209i with National Aeronautics and Space Administration George C. Marshall Spice Flight Center, Alabama 35812 For the U. S. Department of Energy N79-1 255 l (tASV'-CR-15 0 8 3 0 ) PROTOTYPE' SOLAR HEATING Monthly Progress AND COOLING' SYSTEMS Reports jAiResearTch Wtfgb-CO., Los Angeles,, A Tinalas -alifd 70 pHC A04/MF A1 G3/4 38830 - U.S. Department of Energy nt Solar Energy https://ntrs.nasa.gov/search.jsp?R=19790004380 2020-05-24T08:30:26+00:00Z

Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

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Page 1: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

I

DOE/NASA CONTRACTOR REPORT

DOE/NASA CR-150830

PROTOTYPE SOLAR HEATING AND COOLING SYSTEMS (Monthly Progress Reports) Prepared from Documents furnished by

AiResearch Manufacturing Company of California 2525 West 190th Street

Torrance, California 90509

Under Contract NAS8-3209i with

National Aeronautics and Space Administration

George C. Marshall Spice Flight Center, Alabama 35812

For the U. S. Department of Energy

N79-1 2 5 5 l(tASV'-CR-15 0 8 3 0 ) PROTOTYPE' SOLAR HEATING

Monthly ProgressAND COOLING' SYSTEMS Reports jAiResearTch Wtfgb-CO., Los Angeles,, A Tinalas -alifd 70 pHC A04/MF A1 G3/4 38830 -

U.S. Department of Energy

nt Solar Energy

https://ntrs.nasa.gov/search.jsp?R=19790004380 2020-05-24T08:30:26+00:00Z

Page 2: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

NOTICE

This report was prepared to document work sponsored by the United States Government. Neither the United States nor its

agents the United States Department of Energy, the United States National Aeronautics and Space Admini--tration, nor any

federal employees, nor any of thair contractors, subccatractors or their employees, make any warranty, express or implibd, or

assume any legal liability or responsibility for the accuracy,

completeness, or usefulness of'any information, apparatus, product or process disclosed, or represent that its use would

not infringe privately owned rights.

Page 3: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

TECHNICAL REPORT STANDARD TITLE PAGE 1 REPORT NO 2 GOVERNMENT ACCESSION NO, 3 RECIPIENT'S CATALOG NO

DOE/NASA CR-i50830 4 TITLE AND SUBTITLE 5 REPORT DATE

October 1978Prototype Solar Heating and Cooling Systems s PERFORMING ORGANIZATION CODE(Monthly Progress Reports)

7 AUTHOR(S) 8 PERFORMING ORGANIZATION REPORr i

9 PERFORMING ORGANIZATION NAME AND ADDRESS 10 WORK UNIT NO

AiResearch Manufacturing Company of California 2525 West 190th Street 11 CONTRACT OR GRANT NO

Torrance, California 90509 13

NAS8-3209i TYPE OF REPOR5i & PERIOD COVERED

12 SPONSORING AGENCY NAME AND ADDRESS Contractor Report

National Aeronautics and Space Administration July 1, 1978 - Sep 30, 1978 Washington, D. C. 20546 -SPONSORING AGENCY CODE

15 SUPPLEMENTARY NOTES

This work was done under the technical management of Mr. James W. Clark, George C. Marshall Space Flight Center, Alabama

10. ABSTRACT

This report is a collection of monthly status reports from the AiResearch Manufacturing Company, who is developing eight prototype solar heating and cooling systems under NASA Contract NAS8-3209i. This effort calls for the development, manufacture, test, system installation, maintenance, problem resolution, and performance evaluation The systems are 3-, 25-, and 75-ton size units.

Cost information has been removed from these reports.

17 KEY WORDS 1S DISTRIBUTION STATEMENT UC-59c

Unclassified-Unlimited

19 SECURITY CLASSIF (of this repwt) 20 SECURITY

WILLIAM A. PYOOKSBANK, JR. Mgr, Solar Heating and Cooling Pro

CLASSI F. (of this pa8) 21 NO OF PAGES 22

t Office PRICE

Unclassified Unclassified 68 NTI S

MSFC - Form 29 2 (Rev December1912) For sale by National Techmcal Information Service, Sprng field, Vktima 22151

Page 4: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

TABLE OF CONTENTS

Section A - Twentieth Monthly Status Report July 1, 1978 through July 31, 1978 A-i

Section B - Twenty-First Monthly Status Report August 1, 1978 through August 31, 1978 B-I

Section C - Twenty-Second Monthly Status Report September 1, 1978 through September 30, 1978 C-1

iii

Page 5: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

PART A

Twentieth Monthly Status ReportData Requirement No. 500-11

SOLAR HEATING AND COOLINGSYSTEMS DESIGN AND DEVELOPMENT

Contract NAS8-32091

76-13110(20)

August 10, 1978

Prepared for

George C Marshall Space Flight CenterNational Aeronautics and Space Administration

Marshall Space Flight CenterHuntsville, Alabama 35812

LAZTT

AIRESEARCH MANUFACTURING COMPANY

OF CALIFORNIA

A-i

Page 6: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

INTRODUCTION

This is the twentieth monthly status report prepared by AiResearchManufacturing Company of California under Contract NAS8-32091 for the NationalAeronautics and Space Adminstration Marshall Space Flight Center (MSFC). Thereport summarizes activities from July I to July 31, 1978.

For simplicity in reporting, activities are reported by subject matter

rather than by WBS item number.

MEETINGS, REVIEWS AND MAJOR ACTIVITIES

Activities during June were as follows

" A meeting was held in Albuquerque, N.M., with Bridgers and Paxton,consulting engineers for the Novato, Ca., SHAC site on July 7, 1978.Bridgers and Paxton were informed of changes in site concepts sincethe site was reactivated. Mssrs. Benson, Yee and Walker of AiResearchprovided latest site equipment infonaton

* A qjarterly review meeting was held at AiResearch on July I1,1978 toassess program progress. Program acceleration methods were reviewedin detail with Mr. James Clark of NASA/MSFC. Mssrs. P. Benson, R. Nelson,R. Susag and H. Yee of AiResearch attended.

* A contractor/owner interface meeting was held at Portland, Ore., on July 12, 1978 with the Bonneville Power Authority (BPA) to discuss details onthe contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner ofNASA/MSFC and Benson, Yea and Walker of AiResearch attended this meetingand the meeting at Novato the following day. AaResearch is to provide asystem schematic, and ISPI and an updated drawing of the 25-ton unit toBPA personnel. The meeting amounted to a design concept presentation byBPA with a critique by AiResearch rather than the usual preliminary designreview.

" A contractor/owner interface meeting was held July 13, 1978 at Oakland, Ca.regarding the Novato site. Site-related cost estimates were made and meansof consolidating NAVY and NASA funding explored to cover house modifications.

* A contractor/owner interface meeting (Houston Job Meeting No. 20) was heldat Houston on July 20, 1978, with Mssrs. Clark and Gunner of NASA and Mr.Benson of AiResearch attending. Cost of repairing the storage tank damagedin transit to Houston inJune were directed to AiResearch.

Meetings scheduled for the month of August include.

* An overall program status and site status meeting at Dunham-Bush, Inc. onAugust 2 and 3, 1978.

* A contractor/owner interface meeting at Lawrenceburg, Tenn., on August 17, 1978.

* A contractor/owner interface meeting at Redmond, Ore., on August 23, 1978.

AIRESEARCH MANUFACTURIN COMPANY(20)OFCALIFORNIA

A- 1

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Site and Site Equipment Status Charts

Site status Charts I through 5 were updated to coincide with latest test anddelivery activities as of July 31. The charts are included as Appendix A of thisreport.

Status of Instrumentation System Planning Information (ISPI)

Site Revision- - Remarks-

Allaire Park, N.J. B Delta Approved Instrumention Plan (&AIP) received7-17-78 via NASA TO No. 18. Exceptions will belisted and resubmitted to NASA this month.

Lawrenceburg, Tn. A MIP received 7-17-78 via NASA TO No. 17. Collectorloop new to use ethylene-glycol/water instead ofglycerol/water. Exceptions to AIP are imminent.

Harrisonburg, Va. Geo. Mizell of IBM/Huntsville requested changesor original ISPI per telecon on 7-28-78.

Novato, Ca. Preliminary site information received; PIP to bestarted this month.

St. Louis, Mo. No action; site no yet determined.

Redmond, Ore. Preliminary site information received; heatingand cooling schematic (with instrumentation) has been started.

Houston, Tx. D Minor wattmeter changes are being made percomments received from G. Mizell of IBM/Huntsvilleon July 28, 1978.

Las Vegas, Nv. D Extensive plumbing and instrumentation changes arebeing made to system schematic of ISPI per NASA and IBM comments received in July.

Program Documentation

a. Nineteenth Monthly Status Report 76-13110(18), dated July 10, 1978(DR500-1l).

b. Quarterly Contractor Financial Management Report (DR500-27).

Other publications were submitted during July to the parties listed astabulated below.

SubmittalDate / To Subject

7-1-78 J. Clark (NASA/MSFC) AiResearch agreement to use ethylene glycol, as directed by NASA, insteadof glycerol

AIRESEARCH MANUFACTURING COMPANY 76-13110(20)OFCALIFORNIA

A-2

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SubmittalDate To Subject

7-1-78 J. Peters, Project Site Revision E to storage Tank Dwg. Mgr., Houston, Tx., and H-TX-M2-2. G. Neff, President, TEI

SYSTEM DEVELOPMENT

The activities reported below involve heat pump component design, fabricationand testing, and heat pump package development.

Component Design, Fabrication and Test

I. Turbomachines

(a) 3-Ton Unit

Unit D-2 was bench tested prior to installation in the heat pump package(which had been transferred from Dunham-Bush to AiResearch). It exhibited nounusual characteristics. Upon installation, rubbing occurred and the unit wouldnot start. It was concluded that a torque caused by turbine inlet duct loadingwas causing deformation. The duct was realigned and tests were continued in thecooling mode without incident for two days to check system operation. On thethird day, rubbing occurred during start and the unit was removed for examination.Seal rubbing was apparent at both the turbine and compressor-end seals. Furtherinvestigation revealed that several of the journal bearing undersprings were softand could cause rubbing due to instability. Two other units were checked (onethat exhibited intermittent rubbing and one that had not). The unit which had rubbedhad soft springs, the other did not. All undersprings were replaced with stiffersprings. As a secondary precaution, the Dunham-Bush heat pump was reworked toeliminate the possibility of duct misaJignment.

Testing was then resume with the freon pump in operation. The pump failed and itwas found that the wrong power was being applied (208V instead of liOV). Upondisassembly, it was found to be contaminated with carbon particles. The turbomachinewas removed and the compressor also evidenced carbon deposits. The reversing valvewas determined to be the problem and is being replaced with a steel unit using chromeplating as opposed to a carbon unit.

The system has been flushed clean with freon and is currently being reassembled.

Two additional units are available for shipment.

(b) 25-Ton Unit

Unit No. 1 is at Dunham-Bush. Unit No. 2 will be ready for shipment onSeptember 1, 1978.

(c) 75-Ton Unit

Unit No. I is at Dunham-Bush. System testing is to begin the first week ofAugust.

Unit No. 2 is complete and will be shipped to Dunham-Bush on August 4, 1978.

AIRESEARCH MANUFACTURING COMPANYOF CAUIFORNIM7-31(0

A- 3

Page 9: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

2. Motor Controller

(a) 3-Ton Controller

Tests are being conducted on the heat pump package at AiResearch.

(b) 25-Ton Controller

Controller No. 1 has been shipped to Dunham-Bush while Controller No. 2 is 60 percent complete.

(c) 75-Ton Controller

Controller No. 2 will be ready for shipment on August 15, 1978.

3. System Controller

Five controllers are completed and await shipment to Dunham-Bush when needed.

4. R-ll Liquid Pump

(a) 3-Ton Unit

Three pump units were delivered in March. Testing is now at the subsystemlevel.

(b) 25-Ton Unit

One pimp has been tested and shipped to Dunham-Bush. Assembly of the othertwo pumps is being held in abeyance pending system test evaluation.

Heat Pump Design, Fabrication and Test (Dunham-Bush Activity)

1. Camponents (at Dunham-Bush)

(a) 3-Ton Heat Pump

All components for four 3 -ton units are in house except for one condenser and

the turbocompressors, freon pumps and controllers listed in Chart 5 (Appendix A). Twoadditional reversing valves have been ordered to replace the ones with carbon spools.

(b) 25-Ton Heat Pump

All components are in house for one heat pump except for reversing valve andall for the second heat pump except the boiler/evaporator, reversing valve and

the imminent Chart 5 components.

(c) 75-Ton Heat Pump

All conponents are in house except those noted in Chart 5.

76-13110(20)

S MANUFACTURING COMPANYUAIRESEARCH

OF CALIFORNIA A-4 0

Page 10: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

2. Assembly of Units (at Dunham-Bush)

One 75-ton unit has been assembled and is currently piped into the testfacility. Assembly is proceeding on the second 75-ton unit.

The first 25-ton heat pump has been removed fromr the test facility. It iscomplete except for the 4-way reversing valve which Is past due.

One 3-ton heat pump has been coipleted. The second and third units are nearing

completion and the fourth is about one-fourth assembled.

3. Tests of 3-Ton Heat Pump

The 3-ton heat pump was shipped to AiResearch the last week in June and alltesting this month has been done in Torrance Calif. All heat pimp testing atAiResearch was concentrated on the turbomachine rubbing problems. Consequentlyheat pump testing is reviewed in Section I (a) of this report.

~76-13110( AIRESEARCH MANUFACTUING COMPANY7

OFCALIFORNIA

A-5

20

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APPENDIX A

SITE STATUS CHARTS (ATTACHMENTS)

Chart Title

Operational Test Site Status

2 Heat-Pump Development and Test Schedule (Lawrenceburg, Tenn.)

2a Heat Pump Development and Test Schedule (Harrisonburg, Va.)

2b Heat Pump Development and Test Schedule (Allaire State Park, N.J.)

2c Heat Pump Development and Test Schedule (Novato, Ca.)

2d Heat Pump Development and Test Schedule (St. Louis, Mo.)

2e Heat Pump Development and Test Schedule (Redmond, Ore.)

2f Heat Pum Development and Test Schedule (Houston, Tx.)

2g Heat Pump Development and Test Schedule (Las Vegas, Nev.)

3 Operational Test Site Subsystem Schedule (Allaire State Park N.J.)

4 Operational Test Site Installation Schedule (Allalre State Park, N.J.)

3a Operational Test Site Subsystem Schedule (Lawrenceburg, Tenn.)

4a Operational Test Site Installation Schedule (Lawrenceburg, Tenn.)

3b Operational Test Subsystem Schedule (Harriso-burg, Va.)

4b Operational Test Site Installation Schedule (Harrisonburg, Va.)

3c Operational Test Site Subsystem Schedule (Novato, Ca.)

:4c Operational Test Site Installation Schedule (Novato, Ca.)

3d Operational Test Site Subsystem Schedule (St. Louis, Mo.)

4d Operational Test Site Installation Schedule (St. Louis, Mo.)

'3e Operational Test Site Subsystem Schedule (Redmond, Ore.)

4e Operational Test Site Installation Schedule (Redmond, Ore.)

3f Operational Test Site Subsystem Schedule (Houston, Tx.)

4f Operational Test Site Installation Schedule (Houston, Tx.)

39 Operational Test Site Subsystem Schedule (Las Vegas, Nev.)

4g Operational Test Site Installation Schedule (Las Vegas, Nev.)

5 Heat Pump Delivery Schedule (All sites)

AIRESARCH MANUFACTURING COMPANY EDOF CALIFORNIA A- 6

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NOVATO, CA.

DESCRIPTION,

CALENOAYER --CALtENDAR

HEAT PUMPSITE -t

4ONTHJ F 1 2 3

A 4

1978 4 4 6 7

,

A 8 9

f-.-

I 10 11

0 2

J4 I3

C

F 14 I

1 M A

16 X

17

979 J J 1

A ,1920

S 21

0 22 23

D0 24

SITE

ALLAIRE PARK, N.J IHEAT PUMP

SITE '--

LAWRENCEBURG, TENN. iHEAT PUMP SITE

D I

HARRISONBURG, VA HE -PUM HEAT PUMP

-. ,

ST. LOUIS, MO. IHEATPUMP T , I{ I. 1

LOS ANGELES, CA

HEAT PUMP

SITE

HOUSTON, TEX. EATEPUM SIT

-IHEAT

LAS VEGAS, NEV.

PUMP

HSITE

H : :

4H4I C

-

H-Heat Pump Assembly, Test and Delivery to Site C-System Installation Checkout D-System Installation Design T-System Test Operations B-System Installation Bids I-System Installation

- SOLAR HEATING AND COOLING SYSTEMS OPERATIONAL TEST SITE STATUS

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.SOLAR HEATING AND COOLING SYSTEM HEAT PUMP DEVELOPMENT AND TEST SCHEDULE

UNIT: 3­ (LAw--nceue)

EQOOR QUALT:4pgMG1NAUPGEI

DEVELOPMENT/MFG TASKS

MARCH

I 2 3

APRIL

4 1 21 3 1

MAY

2 3 4 11

JUNE

2 3 1

JULY

2 3

.AUGUST

4 1 2 3

ISEPTEMBER

4 1 2 34

I Coinp~ent Development

I.Motor-Cn.l­l 2. Turbo - Campressor

3. Full Current Start Test

I. Fabrication & Assembly

CornPIAII

Cop e, e

p

, S

I 1. Turbo - Conpressor CWolete I I

2. Controller ICcpte I II3 Motor jc=olee j

4. Heat - Exchangers Cmplete

5 Ducting and Pipe Ciplete [

6 Wiring Coplete ]

7. Asserbly Hardware

8. Chassis Assnbly I . -

II. Sub~yst, Developnent

I. Freon Charge I I

2. Bearing Starting -

3 Bearing Cooling I­

4 Motor Cooling

S Motor Calibration

6. Electronic Stability

II­

j 7 Cmprssor Calibration

8 Turbine Calibration

9 Expansion Valve Calibrationi

10. Pressure Drop

11 Pump Controls ir Ie c

1213 FreonSysten,InventoryController. Interlace I I

IV Subsvstm Verification I I I

1. Heating Capacity (Design Point)%

2. Heating Capacity (Off Des.gn I a,

3

4

Cooling Capacity (Design Point)

Cooling Capacity (Of- Design,

I I j

5. Over Voltage Test I I \ 6. Under Voltage Test

7. Fa,klre Modes (S,mlated)

I ­J I.­

2 Governent Inspection I / II

V Prepmratior I Delivery Iit I

AIRESEARCH MANUFACTURING COMPANY OP GlOF CALIFORNIA e~b~k ~ rnc

A- 8 CHART 2

Date 8 9-76

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OIUGIN0 PAGE IS

0EQWf QIJAUTX-SOLAR HEATING AND COOLING SYSTEM

HEAT PUMP DEVELOPMENT AND TEST SCHEDULEUNIT 3- (Htt2,SOl-Ju ,®G

DEVELOPMENT/MFG MARCH APRIL MAY JUNE I JULY AUGUST SEPTEMBE3R'

TASKS 11 3 2341 3 Z23a 4A 1 Z 2 3 4

ICaponent Development

1. Motor

2 Turbo - Compressor

3 Full Current Start Test

II Fabrication & Assembly

I. Turbo - C. .pressor Coniplete

2. Controller Complete

3. Motor Complete

4 Heat - Exchangers Cople-e >8k5 Ducting and Pipe Complete

6. Wiring Ccanplete

7 Assnibl$Hardware

B. Chassis Assembly

III. Subsystem Development

I Freon Charge

2. Bearing Starting

3 Bearing Cooing

4. Motor Cooling

5. Motor Calibration

6 Electroic Stability ")

7. Compressor Calibration

8 Turbine Calibration

9 Expansion Valye Calibration

10 Pressure Drop

Ii Pump Controls

12 Freon Inventory

13 System, Controller, Interface

IV VSubsse

I. Heating Capacity (Design Point)

2 Heating Capacity (Off Design)

3 Cooling Capacity (Design Point)

4 CoolIng Capacity (Off Design)

5. Over Voltage Test /v-.

6 Under Voltage Test

7. FaIjlure Modes (Simulated)

Government Inspection

V. Preparation & Delivery

E V Original rilizetomAIRESEARCH MANUFACIURING COMIANY OF PNscbculed milestone

I CHART 2t(L'

A-9 - Date 8

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.SOLAR HEATING AND COOLING SYSTEM

HEAT PUMP DEVELOPMENT AND TEST SCHEDULE UNIT 3-3 (As t-nea)

OEVELOPMENT/MFG MARCH I APRIL I MAY JUNE oULY AUGUST !SEPTEMBERI

TASKS 1 2 3 4 Z2 3 4 I 23 4 33 44 1 Z 3 4 1 23 . 12 3 4

I. Component Development 1. motor I'

2. Turbo . Ctcpre0r( r 3 Full Current Start Test I

I Fabrication & Assbmbly

I. Turbo - Compressor Completu I j 2 Controller Complete 3. Motor C mnete

4. Heat - Exchangers

5 Ducting and Pipe

Complete

Coplete I 6. 7. AssepblVHardware

C,,ncomplete I

8. Chass., Assebly I

III Subsystem Development I I I Freon Charge I 2 Bearing Starting

3 Bearing Cooling F

Motor Cooling t

5 Motor Calibration

6 Electronic Stability /t or REI u/peA " 7 Compressor Calibration I R

8 Turbine Calibration

9 Expansion vagw Calibration

10 Pressure Drop

I I

I1, Pump Controls I 12,Freon Inventory } _ I

13. System, Controller, Interface OCT Nov I DEC

IV Subsystem Verification I I I

2

Heating Capacity (Desion Point)

Heating Capacity fOff Design) r­ pj

3. Cooling Capacity (Desion Point, i I

4. Cooling Capacity (Of

5. Over Voltage Test

Design, I [

- V 6 Under Voltage Test

78 Failure Modes (Simulated'Goverment Insrec'ion I s"

V Preparation & Delivery -" i I

I _ _ _ II,

M.TAIRESEARCH MANUFACTURING CAfRNCOMPANYO lsh u¢ e~ tnAIRESEARCH OFCALIFORNIA mictn

CHART 26A-O Date 8- 9-70

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1u0O0 SOLAR HEATING AND COOLING SYSTEM

HEAT PUMP DEVELOPMENT AND TEST SCHEDULEUNIT. 3-4 6 VV,47V)

DEVELOPMEN'/MFG TASKS

MARCH 1 2 3 4,

APRIL i 2 3411

MAY 2 3 4

JUNE

112 3 4

JULv

1 2 3 4 AUGUST

12 3 4 ISEPTEiMBER

1 2 34

I Coponent Development

I Motor 2 Turbo - Compressor 3 Full Current Start Test

A/r

I / 0

i

I II Fabricatin & Assrbtv F

I Tcrbo - Com.ressor I

2 Controller

3. motor a Pcoilete

4 Heat - Exchangers

5 Ducting n PP

6 Wiring

7 Assenb l?Hardware

£anoleie

Complete

I

,

,

I

III

8 Chss Assambly

Subsvst,, Oe,eloe-t

!"

OCT

_ _

NOV i EC._ .3A-4 F-Ez -I Preon Charge

IV

7 Bearing Startn

3

4

Bearing Cooling

Motor Cooling

S Motor Caibration

6 Electronic Stab.,ity 7 Compressor Calibration

8 Turbine Calibration

9 Expansion ValVe Calibration

I Pressure Drop

II Pump Controls

12 Freon Inventory

13 System, Controller Inter'ace S~bsvstea verification

i

I if

NO'' i

I I

-----

I IEa'c'ED

I

II I

i

i

I

I

1I Heating Capacity Desiol Point)

2 Heating Capacity 'Of' Design'i

3 Cooling Capacity (Desgr Point)4cooling Capacity (of- {)esicn,

5 Over Voltage Test

I

'

' ­

- 7­ '1

V

6 Under Voltace Testt7 Faa lue Modes, S,mulad)

2 Coverrxent InSoec ionj

Preotiration & Delivery I

I

F - F] CO AIRESEARCH

~ ~OF MANUFACTURING COMPANY

CALIFORNIA

7OrT._:raI riaA

rnilestonc, netn

ie'op

CHART 2C

A-11 Date: 5-7- 7C

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.SOLAR HEATING AND COOLING SYSTEM

HEAT PUMP DEVELOPMENT AND TEST SCHEDULE UNIT: 2 7-)Sz,Lcwl;)

MARCI APRIL MAY JUNE JUL- AUGUST !SEPTEJIBER DEVELOPMENT/MFG12 4',

TASKS 1 2 5 4 1 Z b 4 1 23 I 2 3 1 2 3 4 1 2 3 4 1 2 34

I. Coiiponent DeVeloppe't I I . Motor COpvPL T0 '

2. Turbo - Compressor

3. Full Current Start Test NA

IT Fabrication & Assemblv I

I. Turbo - Compressor Comolete I 2 Controller comnete j I i 3. Motor C lete

4 Heat - Exchangers compete

5 Dueting and Pipe I j I 6I W*r-­

7 Pssable Hardware I I ­

8 Chassis Assembly

i1. Subsys-e Oeveob-e-t C r NjO' C>0 JA F-. WAR APFR

I.2. Freon ChargeBearing Startargno ]

3 Bearing Cooling I 4 Motor Cooling

5 Motor Calibration I j 6 Electronic Stability - i. I

7 Compressor Calibration N II 8 Turbine Calibration

9 Expansion ValVe Calibration I-aR. .

l0. Pressure Drop

11 Pump Controls

I2.Freon Inventory i" i. I

j IV Subsystem Verlficat-cr I

13. System, Controller, Interface

I Heating Capacity (Desgn Point)

2 Heating Capacity 'Off Design $

3 Coolng Capacity (Design Point) ,

4 Cooling Capacity (Of' Design,

5 Over Voltage lest

6 Under Voltage Test I i

7 Falire Nodes t SimLlatedi

8 Gover'nent Insoect,m

V. Prentrator & Delivery /

M~fef AIRESEARCH MANUFACTURING COMPANY OFCALIFORNIA 0 OSC )eAiIC6one

oi £diery da4e. fl bea~cteA Ly cbcsngle

CHART 2d A-12 " Date: -Z-d76

Page 18: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

,SOLAR HEATING AND COOLING SYSTEM HEAT PUMP DEVELOPMENT AND TEST SCHEDULE

UN IT Z5-0 ( Papmo,4PCJ)

JUNE JULY iAUGUST !SEPTEMBERDEVELOPMENT/MFG MARCH APRIL MAY

TASKS 1 2 3 4, 1 2 ; 2 33 4 ] -2 31 4 1- -1I ,F

I Camiponent Developnient A)

I Motor 7 2QLi/ 5.02 Turbo . Cwpressor

3 Full Current Start Test JII rabr,.ator & Ass mibly

I. Trbo - Corrpressor I

Z Controller

Motor; a Conloeti

Heat - Exchangers I a p'et:

Oucting and Pipe Cmplete6. Wt ring CempleteI

7 Assenbl Hardware I I3 Chassis Assmbiv i}I­

. . . . ,- - ..

III Subsystm Developne-t i _U IA7-i A_; ILJ I L­_____ I tA,-_

t Creon Charge

2 Bearing Startino I

3 Bearing Cooling I

& Motor tooling

S Motor Calibration

6 Electronic Stab,it- NOT I ECn, - I7 Copressor Calibration IINAL GI

8 Turbine Calibration PAGELPA9 Expansion Valie Calibration KaiI Pressure Drop I I

II Pump Controls I12. Freon Inventory I I

13 Syst m, Controller Inter ace

IV Subsystem Verificator I­

1. fHeatng Capacity (Design Point) - ­

2 Heating Capacity 'Of' Design) I I _

3. Cooling Capacity (Oestan Point' /

t Cooling Capacity (Of- oesion, II­

5 Over Voltage Test I 1/

6 Under Voltaoe Test I It

7 Falt.r, Modes Sinlatedt

8 Governnent Inspec'," / s'

Delivery / _oV. Pre cratio, D

V Original rmdestone SAIRSEARCHMANUFACTURING COMPANY

OF CALIFORNIA ri'eshedu(ed 'rnleeoona [3 1, TchedueA n64e eyIeri donewiorth

ShOLe the delf er, e deI"tE.L lilts LjnI* 1edby Obcwge of $Lte.

CHART 2a7

-Date:__8-9-7____A-13

Page 19: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

,SOLAR HEATING AND COOLING SYSTEM

HEAT PUMP DEVELOPMENT AND TEST SCHEDULE UNIT 7 - /-/oa rosj)

DEVELOPMENT/MFG - - - MARCH I APRIL KAY JUNE- JULY AUGUST ISEPTEMBER

TASKS 2 1 3 4 1 2 3 4 I 2 3 4 1 Z 3 4 1 2 5 4 1 Z 3 4

Component Dve lopmert

2. Turbo - Compressor

3 Full Current Start TestC'mIceI

IT abrlcatlon & Assembly, t 1. Turbo - Compressor Complete

Controller Complete J I I3. Motor Comolete I

Meat - Exc'angers I - . iS Ducting and Pipe

6 Wiring ­7. Asswblf. Hardware

8 Chassis Assembly _ _ ­

oarTI I Subss'em Oevelope-t OCT. I rscn Charge .I

2. oaring Starting

3 Bea-ing Cooling

4 Motor Cooling

5 Motor Calibration

6 Electronic Stablity

7 Comp-essor Calibration

S Turbine Calibration

9 Expansion ValVe Cahbration

1O. Pressure Drop

II Pump Controls

IZ Freon Inventory13. System. Controller, Inter'ace I

IV S~bSuystem,svs VerifctolrVerif n teI -pr N v13. ti c,:ton h OCT 1 i r 'I'kJA W

I Heating Capacity (Design Point)

Z Heating Capacity (Of" Design

3 Cooling Capacity (Design Point)

4 Cooling Capacity (Of' Desigc, - I I 5. Over Voltage Test

0 Under Voltage Test i

7 Fallire Modes (S..-lated)

9Goverrnment Insoecti, 1 0 V Preparation Delivery I i]

V Origmncl rmilee nc AIRESEARCH MANUFACTURING COMPANY f rglneboe

*ResIedUkd~ mdesbne,OF CALIFORNIA0

CHART 2FA-14 Date 9-7

Page 20: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

-SOLAR HEATING AND COOLING SYSTEMHEAT PUMP DEVELOPMENT AND TEST SCHEDULE

UNIT 75-? (CAs Vc)

DEVELOPMENT/NFG TASKS

MARCH 12 3

APRIL 4d1i 2 4 11

MAY 2 5-

JUNE 1l1 3 4%I1-

JULy 4

UoUST 1 Z

ISEPTEMOER _ 4 1 43h

I. Componernt evelopmnent 1 11t[ I. Motor,

2 Turbo - Conpressor 1'l4 TIPEQUf,'D 3, Full Current Start Test I

1I Fabrication & Assenbly -

1. Tt.rbo - Compressor kiolet

2 C.,troller Colplee I 3 Motor ondote 4 Heat - Exchangers Core ete 1

5 Ducting and Pipe C Ie -

6.Wiring

7. Asseatbly Hardware

B. Chassis Assetibly

9 4-ple\

1 I

[4 "-

III Subsvs ter" D.eeoore,t 5VPT ~t ~ F~h M~k;TN-'-

I Preor Charge I

2 Bearing Startino

3 Bearing Cooling I A Motor Cooling

5 Motor Calibration

6 Electronic Stability

7 Copressor Calibration NOT C -ILII, I 8 Turbine Calibration

9 Expansion Valye Calibration

' 10 Pressure Drop

II Pump Controls i j I 13 Systoi, Controller, Inter'ace RGh A P GE

IV Subsvste, Verification I '-A. X 1. Heating Capacity (Design Point) i

2 Heating Capacity 'Off Design, -

3 Cooling Capacity (Design Point) 4 . 4 Cooling Capacity (Off Design, I S. Over Voltage Test

a Under Voltage Test

a overften t Inspection

V Preocratuon & Delivery

AIRCSARCH MANUFACTURING COMPANYOFCALIFORNIA v iescheduledl milestone

•Date: ?S 9-29 -7fCHARTA-15

Page 21: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

SOLAR HEATING AND COOLING SUBSYSTEMS OPERATIONAL TEST SITE SUBSYSTEM SCHEDULE

SITE AL-,e StArE MAgo, AIJ

I E MAR APR AY JUN JUL AUG SEP OCT NOV DEC

SUBSYSTEM ].J

•Heat Pump (See Chart J

"Collector S/S . .

]

I

I

1. Develop Rents.

2. Delivery

* Storage S/S

I.Develop Specs.

CO p_- .[_ CC/V7PA.

_ _

...

_ _

-[

_ _

-

2. Procure

DeliveryDaO--taSiS -- I .. ­ -­[­ _e

I Develop ISPI

2. Review & Approve 3.Procure

12 /ITi -' '

... .

_ -'­ ----­

$ -1 A

Received-JAPReceived

_

C'

4. Delivery

> Systen Controller S/S I. Manufacture

I 2. Ship to D/B

3 Delivery

O 01W - Preheater

C7P T -_ ___

'

--.­

_ _ _

I

-.

_

.. -.

...

.

-__

_JASA9­-

.... - -­

,. Develop Specs

2. Procure 5. D liveryI

CC)_ __­ ---­ -­ -

- -­ -

.. .. --­ -

OTHER MAJORCOMPONENTS ... . .. --

Cooling Tower _I­

i.evelop Specs

2. Procure

CnIPLE

.... .

..

_

- -

3. Delivery[ Auxlllary Heater I Develop Specs

_ _ _-_ _ _ - - - _ _ _ -­ . :-­

2 Procure

3 Deliver I -­ - "

A Original milestone

.1AlkFORiiiii

O Reschedulcd milestone General contractor procured itea

Cha't 3

1 Date

Page 22: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

SOLAR HEATING AND COOLING SUBSYSTEMS . OPERATIONAL TEST SITE INSTALLATION SCHEDULE

SITE .4LLA);E% )60%/.LJ {

INSTALLATION/CPERATION TASKS

JAN FEB MAR MA..

APR MAY JUN JU[ AUG SEP OCT DEC...

BLDG. CONSTRUCTION/IOD .

I. Design C 't.CTE i__ ....... -... - -

a. System Req. Inputs - - -... . ! - __.,

b Design Reviews _ - I--­ ..

2 Construction

a. Collector Interface , . ...

b Backup Syst. Interface i . I

c. Other Equip Interface I----­ -­ - ---

SOLAR SYSTEM INSTALLATION I

I A&E Selection ComPLer j -­.. -­-

2. Sys Installation Design

3. Select Contractor ________ - ,

4 Install Collector S/S -_

5 Install Storage S/S .. . .­ - _

6. Install OtfWPreheat S/S -­ _____

7 Install Data S/S . 8 Install Sys Control S/S I -... - ..-. .

9 Install Heat Pump S/S

SYSTEM CHECKOUT

I__"__.

--I ... - "

2

Leakage Test Balance Collector Field

..-. I -. . .­ -

... . . ... -..

I-jj - 2

3 Wiring C/O and Test . ... . . ... - ---.. . 4 Functional Test All Modes -­ .-­ ___ -­ --

S. Instrumentation Verification Ii --­ -­ - -­6 System Turn-On --. I - - --­ 0

7. System Acceptance Tests - - -_ -.-

OPERATIONAL TESTING

I. Date Acquisition - -­ _ -' "___ -­

2 Schedule Maintenance --­ - -

3 Performance Reports - -.--.

A Original milestone 0 Rescheduled milestone NANUFIR I aILChart

0, CALIONNIADate

406ZSz2

Page 23: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

SOLAR HEATING AND COOLING SdBSYSTEMS OPERATIONAL TEST SITE SUBSYSTEM SCHEDULE

SITE 1-4 oerCE67C-124WJ/

JAN FED MAR APR RAY JUN JUL AUG SEP OCT NOV DEC

SUBSYSTEM !

" Heat Pump (See Chart I)

* Collector S/S

1. Develop teqMtS.

2. D e livery

_

-O/A1PL._

-

. I_

______

F.---j

_

I . .. _ _.. ..

-­'

. . . .. . . . . .. .

1. Develop Specs.2 Procure 3.Delivery

* Data S/S I.Develop ISPI

____

_

. . . ..

il___ r.I.. I

..

. . .­

; . . _____

. .

-...

____ ____ _____

_

____

-

2. Review & Approve3.Pocr 3. Procure

-­6JSA-Recelved--­

. __A__A .;

__ v e-IP

-- ____

* System Controller S/S -" ... _ _..

O 1.Manufacture 2. Ship to 0/B

3. Delivery

* Dh - Preheater

I. Develop Specs

CotPMF~II___

i &._LrE

- I­ _---__

A

-Ei ..-...

2. Procure _ _ ._­

3. Delivery

FOTHERMAJOR COMPONENTS __-_______­ _. ___ - .

Cooling Tower

I. Develop Specs

2. Procure

3. Delivery

* Auxiliary Heater

I. Develop Specs

2. Procure

COAIrL.

- -

..

___ // -

. ....

. -

-

_---_

.__-____-__-­

_

. . ..

-­ ......... . . .

- -­-

.....

3. Deliver

AIRKSLAROHvANuACIURtNOCOMPANY OrAurOnmiA

A

NI/A

Original Mtlestone

.. .. -.. . . ...­

0 RpSrhdled mllestone * General ontractor procured Item

Chart_ _Dae_3-,:Z

Page 24: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

INSTALLATION/OPERATIONTASKS

BLDG. CONSTRUCTION/HOD I

JAN FEB

SOLAR HEATING AND COOLING SUBSYSTEMS

OPERATIONAL TEST SITE INSTALLATION SCHEDULE

9ITE L.~ran rs,..za 1 AR APE HAY JUN

_____IJ

I

JUL AUG SEP OCTC NOV

- -

DEC

1. Design

a. System Req. Inputs

b. Design Reviews _

coIlpLcre

I)PLEITLE­

-.­-

-­ i

°

2 Construction

a. Collector Interface

b. Backup Syst. Interface

' ....

c. Other Equip. Interface

SOLAR SYSTEM INSTALLATION

_ _

I I -

I

i

. A&E Selection

2 Sys Installation Design

3 Select Contractor

4. Install Collector S/SI

5. Install Storage S/S

6. Install DIM Preheat S/S

7. Install Data S/S

II Install Sys Control S/S

9 Install Heat Pump S/S

CO )L

NZ...AA

-

-

/E

_

..

..

.

-

-

_ _.__­

-

.. . .OMLE _

-...

-

.......

- -

/_I

I

I-­i

-

.

SYSTEM CHECKOUT

I. leakage Test 2. Balanci Collector Field

_

3. Wiring C/O and Test____ 4. Functional Test All Nodes

S Instrumentation Verification

- - .....

6. System Turn-On

7 System Acceptance Tests

....

OPERATIONAL TESTING

2 Schedule Haintenance - - -

3. Perfomance Reports - -o

A Original milestone 0Rescheduled milestone OfCAI$RNAChart 40-

Date

Page 25: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

SOLAR HEATING AND COOLING SUBSYSTEMS

OPERATIONAL TEST SITE SUBSYSTEM SCHEDULE SITE q/.e)5O'SUPC)$9

JAN FEB lAR MMAY JUN JUL AUG SEP OCT NOV DEC

SUBSYSTEM A

* Heat Pump (See Chart |)I

* Collector S/S

1. Develop Reqits 2 Delivery

* Storage S/S 1. Develop Specs.

CO

__---1'_

1

PLET

E

-t

___

I, -­

_

A / -_

2. Procure -

3. Delivery* Data S/S

-I _i! _

I Develop ISPI I_ __ __

2. Review & Approve _ -­ -1_

3. Procure A ....-_ ... -__

4.Delivery (NASA) -A

* System Controller S/S

N> 1. Manufacture _ _ _ _

0 2. Ship toD/B _ I - - ­

3. Delivery OWDH- Preheater

[ -_ I _---­ -I2 DevelopProcure Specs C M .­- -. ._ _

3. Delivery

MTHERAJOR COMPONENTS­

I Cooling Tower 1. Develop Specs VOAPI TE

-Z.__.-_

....

2. Procure

3 Delivery

* Auxiliary Heater I Develop Specs

2. Procure

3 Deliver

...­

__1 -­

-J,

-

MT,CChart

a Original milestone 0 Rescheduled milestone

Date 3h

Page 26: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

INSTALLATION/OPERATION TASKS

BLDG CONSTRUCTION/OD

I. Design a. System Req. Inputs

b Design Reviews

2. Construction a. Collector Interface

b. Backup Syst Interface

c. Other Equip. Interface

SOLAR SYSTEM INSTALLATION

I.A&E Selection

2. Sys. Installation Design

3. Select Contractor

4. Install Collector S/S

5. Install Storaoe S/S 6. Install DI Preheat S/S

7. Install Data S/S

8S Install Sys Control S/S

N 9. Insta ll Heat Pump S/S

SYSTEM CHECKOUT

I Leakage Test 2. Balance Collector Field

3. Wiring C/O and Test-

4 Functional Test All Modes

5 Instrumentation Verification

6. System Turn-On

7. System Acceptance Tests

UPERATIONAL TESTING

1. Data Acquisition

2. Schedule Maintenance

3. Performance Reports

SOLAR HEATING ANDCOOLING SUBSYSTEMS OPERATIONAL TEST SITE INSTALLATION SCHEDULE

SITE 1A2/SJ0 L R W.

I JAN

I FEB MAR I APRAY I MAY JUN JUL AUG SEP OCT NOV DEC

L I

Cdr'E7-SPO - - --

I .. .... . . .

I

I,

- I __ __ ,

-. -

-. m PL-ET2K

(OA)s LfTE

1A -

- - i_ -­ - . !__-_ - -.

- __. -­ . -

- . . - .

_ ___

- ---­ -­

_________

.-.. .

_, "----_.

..-. . .­ -­

'"i

___ -­ __ ---­ - -­ -, 21 zt-"s. T5D . . ..

_ __ _ _ ______ _ A A - -

A Original Milestone 0 Rescheduled Milestone Date

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SOLAR HEATING AND COOLING SUBSYSTEMS OPERATIONAL TEST SITE SUBSYSTEM SCHEDULE

SITE _goVATo f, LP.

SUBSYSTEM JAN FEB MAR APR HAY JON JUL AUG SEP OCT NOV DEC

* Heat Pump (See Chart ).

* Collector S/S

t. Develop Recqmts

2 Delivery|

* Storage S/S

I.Develop Specs. 2. Procure

Com LIE-­j1

I 1 1_

_ --­

"_

3 Delivery __ -­ . . .. - ---­

,. Develop ISP! 2. Review & Approve

3. Procure

__

__ _ _

4. Delivery * System Controller S/S i

: ---

I. Manufacture

2.Ship to D/B 3.Def,,eryl•HD -Prehoater __j

___

-e - - -

I.Develop Specs 2. Procure 3._Delivery __________

C0A?PFjr7C

________________

.........

_

__

_________

OTHER MAJOR COMPONENTS -

Cooling Tower

I Develop Specs

2. Procure

AJ/A ..... I/ A ..... .. . .. .. .

3. Delivery __ _J_//4_ __ ...... ..... ...... .....

* Auxiliary Heater

I Develop Specs 2. Procure

_______.. ... .. ...... . . ..

3. Deliver ,0­ _

or cACIFoSAIA A Original MIlestone

UjALF~kI7D.

0 Rescheduled Milestone * General contractor procured Item

t r.., Chart 3C Date8.­ 7

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SOLAR HEATING AND COOLING SUBSYSTEMS OPERATIONAL TEST SITE INSTALLATION SCHEDULE

SITE HovAro7 C4L/r

INSTALLATION/OPERATIONTASKS BLDG. CONSTRUCTION/hOD

JAN FEB ______

MAR APR PAY JUN JUL AUG SEP OCT NOY OFt

I. Design

aSystpe Reg. Inputs

b. Design Reviews

2. Construction

a Collector Interface

b. Backup Syst. Interface c.Other Equip. Interface

~

____

rr

A)

-_

_ _

I

I_____

_

-.

_I

____

-

____-­

i-. -­

....I.

I --.--.

-

_

10

_

_

_ -

-

...

I

-

_

O

-

- _____

SOLAR SYSTEM INSTALLATION I -

I. A&E Selection _­ -­ 0 _--­

2. Sys. Installation Design

3. Select Contractor

4. Install Collector S/S 5. Install Storage S/S _­ -­

_ -__I

- A

_

-6. Install DIM Preheat S/S 7. Install Data S/S

8. Install Sys Control S/S

9. Install let Pu p S/s .-..

-

____

_

_ _ _ -_____________

....

SYSTEM CHECKOUT --9-79 -I. Leakage Test

2. Bdlance Collector Field

__

_ . I 3. Wiring C/O and Test - _­ --­

4. Functional Test All Modes

5 Instrumentation Verification

6. System Turn-On . 0

-

- --

I -­

__j'u

_-.

7. System Acceptance Tests -

OPERATIONAL TESTING

1. Data Acquisition

2 Schedule Maintenance

3. Perfomance Reports

76Dc/

I-­ -­

__

----­

-

-_

UCEIJANCOMP&ItIYA

A Oriqinal Milestone 0 Rescheduled Milestone Chart 4C

Date

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SOLAR HEATINC ANDCOOLING SUBSYSTEMSOPERATIONAL TEST SITE SUBSYSTEM SCHEDULE

/C)7 C SITE 5tLeu/s. t4& 1976jJAN FPEB MAR APR KAY JUN JUL AUG SEP OCT NOV DEC

SUBSYSTEM

Heat Pump(S a nCh a rt )

" Collector S/S

I Develop Req1ts

2 Delivery * Storage S/S

_ JAN

_

-_

F ,

i_

_ _

I

I CUN L

C0__F_

A

I577

_ __

j I Develop Specs.

2. Procure

3 Delivery -­ - - - :

. Deve lop ISP I

2. Review & Approve

3. Procure ______

F i

S. L5-

L"I

AINASA

1

4. Delivery

* Systew Controller

1. Manufacture

2. Ship to D/B

S/S

.. ....

. . .

-o---

I

-!

3 Delivery

* Dh4 - Preheater

-

-

I Develop Specs _

2 Procure 3 Delivery

...... . .... _ _

OTHER M4AJORCOMPONENTS - - - -- A-

Cooling Tower

1. Develop Specs 6-AI___.- G E

2. Procure

3. Delivery .... _____

* Auxiliary Heater

I Develop Specs

2 Procure

3. Deliver

//A ­

tJ/A %I/A

t.....I.-A Original Milestone Chart 3d

FD te 5. Z 7

Page 30: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

/979 -4.

SOLAR HEATING ARD COOLING SUBSYSTEMS OPERATIONAL TEST SITE INSTALLATION SCHEDULE

SITE 57 Lous, MoA_ _ _--_-__-

INSTALLATION/OPERATIOh TASKS

BLDG CONSTRUCTION/OD 1. Design

a System Req Inputs _

FEB MAR -----------

APR

_

KAY

. . ..

JUN JUL

O p

AUG

.-

SEP OCT NOV DEC

b. Design Reviews _ _ (NAS _ I 2. Construction

a. Collector Interface

b. Backup Syst Interface

c Other Equip Interface

. -..

,I

_[_

I I

----

N I -­

___

,

SOLAR SYSTEM INSTALLATION

I. A&E Selection

2. Sys. Installation Design

3. Select Contractor I

- -­ -

CO-t7

L--4

4 Install Collector S/S -----­

5. Install Storage S/S _----'

~' 6. Install OW Preheat S/S

7. Install Data S/S .... -­

-241A

-

N (31

8 Install Sys Control S/S 9. Install Heat Pump S/S

.._ _ _ ----

SYSTEM CHECKOUT

I. Leakage Test

Z. Balance Collector Field -"

-i

I --­

3. Wiring C/O and Test

4. Functional Test All Bodes - -

5. Instrumentation Verification _ "

6.System Turn-On ......-.

7. System Acceptance Tests _ -­...... ........

OPERATIONAL TESTING

I.Data Acquisition

2. Schedule Maintenance TbD - ..... ... ...

3 Perfonmance Reports -

A5Z1ro.IICAtYORNIA

A Original Milestone Chart 4d Date .

Page 31: Department of Energy - NASA · 2013-08-31 · the contemplated Redmond SHAC site. Mssrs. J. Clark and R. Gunner of NASA/MSFC and Benson, Yea and Walker of AiResearch attended this

t979

SOLAR HEATING AND COOLING SUBSYSTEMS

OPERATIONAL TEST SITE SUBSYSTEM SCHEDULE

SITE JEDMOtO, C5 R.

JAN FEB MAR APR HAY JUN JUL AUG SEP OCT NOV DEC

SUBSYSTEM

* Heat Pump (See Chart I)i

" Collector S/S

1. Develop Reqnts.

2. Delivery

* Storage S/S l. Develop Specs.

2. Procure

3. Delivery

* Data S/S I Develop ISPI

2. Review & Approve

3. Procure

COrF.-1P.. Y__

___

_ _i j __

___

_

A

I

I i __.. ... .......... ...

__

_

_-.

4.DeliveryI * Systm Controller s---­

__ _ j --

N3a'

1. Manufacture

2. Ship to D/B 3. Delivery

L

/-__ _

* DIM - Preheater

I. Develop Specs

2 Procure . ....

3.Obalivery OTHER MAJOR COMPONENTS

....... ;­ .... ..... ---. , .

* Cooling Tower I. Develop Specs

2. Procure . . .....

3. Oelivery * Auxiliary Heater

I.Develop Specs .j -

_

-

-

2. Procure

3. Deliver

,S A Original Milestone -

Chart

Dateo

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SOLAR HEATING AND COOLING SUBSYSTEMS OPERATIONAL TEST SITE INSTALLATION SCHEDULE 00

1979 SITE RevMotn O ie

INSTALLATION/OPERATIONTASKS

BLDG. CONSTRUCTION/HOD

JAN FEB MAR

I AR

A

AY

K

JUN JUL

JU

AUG

AUG

SEP S

CT G

DEC D

1. DesignIII -I -_ ___

a System Req. Inputs ____ { _ _,-­ -­

b Design Reviews -

2 Construction - I i

a. Collector Interface

b. Backup Syst Interface

_ -A __ -­ ,

-

-----. _.

I - -.

c. Other Fqulp. Interface A - - -

SOLAR SYSTEM INSTALLATION

I A&E Selection 12--7I ­ __

2. Sys. Installation Design io-i-7 3. Select Contractor '2-i-l 4. Install Collector S/S

5. Install Storage S/S

6. Install DIW Preheat S/S i_

7. Install Date S/S _ _

B. Install Sys. Control S/5 9. Install Heat Pump S/S _ _ i

SYSTEM CIIECKOUT

I. LeaKage Test . .

2. Balance Collector Field 3.Wiring C/O and Test

4. Functional Test All Modes

5 Instrumentation Verification

6. System Turn-On A

7. Systen Acceptance Tests

OPERATIONAL TESTING

I.Data Acquisition ___ '__ _ 2 Schedule Maintenance T519

3. Performance Reports -- A

A Original Nilestone

MWCLIFOR9IA Chart 4e-Date

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SOLAR HEATING AND COOLING SUBSYSTEMS OPERATIONAL TEST SITE SUBSYSTEM SCHEDULE

SITE OLJ,5701JT"hV.

JAN FEB MAR APR HAY JUN JUL AUG . SEP OCT NOV DEC

SUBSYSTEM

* Heat Pump (See Chart I)

" Collector S/S _

2 Delivery _ _ _ _ _ . ...

* Storage S/S

1. Develop Spec (115-7. 2. Procure ___..

i . . .

-

3. Delivery " Data S/S1. Dev e lop ISPI (/ / -/,3-7 7 ) .

i

1­--.. ) " - - z­: - --

2. Review & Approve

3.Procure -____

-___ --­ -

4. Delivery -. __

> .

*

System Controller S/S . anufacture

22. Ship to 0/B 3. Delivery

DhM - Preheater

I Develop Specs

-

-

- - .--­ -

CO re . -C.

___________

I

-

- " - -­ --­ - ..

I

. .... . .

I

.

? Procure

Delivery OTHER AJOR COMPONENTS

______ __._---T'_

___ _ -

i

---

Cooling Tower 1. Develop Specs ./.....

2. Procure

3. Delivery

* Auxiliary Heater 1. Develop Specs

2. Procure

3 Deliver

.... A.

k-4/ NIA

r ti

I(.AUeI

A Original milestone 0Rescheduled milestone

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SOLAR HEATING ANDCOOLING SUBSYSTEMS OPERATIONAL TEST SITE INSTALLATION SLHEDULE

SITE t/oLsrvij. Tex.

ISTAL'.TIOHOPRATIOII BLGTASKSBLDG DONSTRUCTION/MOD ...

JAN FEB MAR APR 4AY JUN JUL

_

AUG SEP OCT ,9140O

_

DEC

IDesignCo'p

a. System Req. Inputs b, Design Roylews

2. Construction

rt CoM P ("JAS A'

I . .-­

__

I

-

-

_________

__ __

..

i­-

_ __...

_ _­

( -.-­

_ -

-

......

a. Collector Interface

b. Backup Syst Interface

c Other Equip. Interface

. __---

I _-­

_ -

I

. . ... ,

_

-­.....

:

I -

SOLAR SYSTEM INSTALLATION I

I. A&E Selection

2.Sys. Installation Design 1_11A

COMPL.ET0 - I .3--,-­ -­

3. Select Contractor

4. Install Collector SIS ____

___-­

>

5.3nstall Storage S/S 6. Install Dh14Preheat S/S

7 Install Data S/S 8 Install Sys Control S/S

9. Install Heat Pump 5/S­ - - -..

-.---­---­

- -"­

. . . . .. .. .

1.0 SYSTEM CHECKOUT

I. Leakage Test

2 Salance Collector Field

3.Wiring C/O and Test 4,Functlonal Test All Nodes 5 Instrumentation Verification

. .. ___­

__---_ _____­ _­ -­

..

I -

I

- -

I

.. - - -­

..

6.System Turn-On 7. System Acceptance Tests

---­ .

-­ ---­

-­ -­

_

- . i

OPERATIONAL TESTING

I.Data Acquisition

2.Schedule Maintenance 3. Performance Reports (Ao4Jry.

7-A9

-____

. .. . -. . ....-

I IAIREQARCHMANOFACTURINGCONPANh I~W OfCLIFORNIA

A Original milestone 0 Rescheduled milestone 0 Except for Instrumentation

Dat

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_______ --

--

--

--

--

SOLAR HEATING AND COOLING SUBSYSTEMSOPERATIONAL TEST SITE SUBSYSTEM SCHEDULE

SITE L s V- -2s. __V

--MR !- APR MAY JUN JUL AUG SEP OCT NOV DEC

JAN FEB ___________________---ISUBSYSTEM

"Heat Pump I I I - ­(See Chart I)

" Collector S/S

1.Develop Newts Co __r_____. . 2 DeliverytI

* Storage S/S

i. Develop Specs. P. .. -. .. "

2. Procure.__.... ...........

I Data S/S 3. Delivery

I. Develop ISPI (Z-/2-77) -- _ _..__ -_

_ .. _r____2. Review & Approve -- ..

1 3.*Procure (4S)--__4. Delivery -NASA'F __- _.....

* System Controller S/S .......C:)I. Manufacture

2. Ship to D/B - ­

3. Delivery

*D Preheater

I Develop Specs COMPLe F

-

.. -­

2o Procure

3 Delivery __-_------_-- _ _..

OTHER MAJOR COMPONENTS

* Cooling Tower-77-z ­1. Develop Specs _T

- .2. Procure -3 De l i v e r y --- _- --

* Auxiliary Heater_ ­I.Develop Specs

2. Procure

_.. .t .3. Deliver _--

A Original Milestone Rescheduled Milestone * General contractor procured Item

Chart 39aW ttrraft.i Date lk w

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SOLAR HEATING AND COOLING SUBSYSTEMS OPERATIONAL TEST SITE INSTALLATION SCHEDULE

SITE 4,45 V& s n

ITA SKS JANPRAIO FES MAR APR MLAY JUN JLAUG SEP }OCT NOV do

BLDG. CONSTRUCTION/MOD 10I 1. Design

a, System Req Inputs

b. Design Reviews

2. Construction a. Collector Interface__

.. &er o­

____ ____ ____

-

__

I i

-

- ____­

I

- --­

----I -

b. Backup Syst. Interface

c. Other Equip. Interface SCLAR SYSTEM INSTALLATION

A--_. I_...--.----. --

I. A&E Selection 2. Sys. Installation Design

3, Select Contractor .

C /v-4 ___2.. .-CI4I ..,T6 I­_OMP. E....-_ ....

4 Install Collector S/S!

S. Install Storage S/S

6. Install DI Preheat S/S

7. InstallOataSS . ...-­

.. . ........

8 Install Sys Control S/S

9. Install Heat Pump S/S -

- - ..

__-­ ....

... -

_

-_"-­

- - -

SYSTEM CHECKOUT

I.Leakage Test 2. Balanue Collector Field -­ -______

.....-..--­ /

3.WirIng C/O and Test 4. Functional Test All Modes

_-_

- -"

______

-

- - -

5. Instrumentation Verification

6. System Turn-On

7 System Acceptance Tests

__ __

-­_

_ .... __-_

_ _--­ ....

--

OPERATIONAL TESTING

I.Data Acquisition . 4 • - I I

2 Schedule Maintenance t i_

3. Performance Reports -­ __ _ _ --c

IEI~l tIrTime COIIPflV

afcMIIC

A Original milestone 0 Rescheduled Milestone

Chart 41

Date

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SU Turbocom­pressor

Motor Control

Freon Pump

Heat Pump Complete

Start Test

Test Time, Weeks

Test Complete

Ship Date

Intended Site

3 Ton

25 Ton

75 Ton

#1

#2

#3

4

#1

#2

#1

#2

Returned

8-1

8-11

-15

Shipped

9-1

Shipped

8-4

Returned

8-1

8-11

8-15

Shipped

9-1

Shipped

8-15

Returned

8-1

8-11

8-15

Shipped

9-1

Received

Received

Complete

8-10

8-31

9-15

7-28

10-1

7-24

9-5

7-13**

8-11

9-15

11-10

12-15k

3-30

8-1

9-15

4

5

8

4

11

5

7

11

8-10

9-15

11-10

12-15

3-30

5-15

9-15

12-8

8-J0

9-22

11-17'

12-22

4-7

5-22

9-22

12-15

Lawrenceburg, TN

Harrisonburg, VA

Allaire Park, N.J.

Novato, CA

St. Louis, HO

Redmond, OR

Hojston, TX

Las Vegas, NV

*Testing of the 25-ton system will start earlier if a break occurs in the 75-ton system testing.

**At AiResearch

00 Heat Pump Delivery Schedule

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PART B

Twenty-First Monthly Status ReportData Requirement No. 500-11

SOLAR HEATING AND COOLINGSYSTEMS DESIGN AND DEVELOPMENT

Contract NAS8-32091

76-13110(21)

September 10, 1978

6pAGE BLA i K NOT E#

Prepared for

George C. Marshall Space Flight CenterNational Aeronautics and Space Administration

Marshall Space Flight CenterHuntsville, Alabama 35812

AIRESEARCH MANUFACTURING COMPANYOF CALIFORNIA

B-i

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INTRODUCTION

This is the twenty-first monthly status report prepared by AiResearch ManufacturingCompany of California under Contract NAS8-32091 for the National Aeronautics and SpaceAdministration Marshall Space Flight Center (MSFC). The report summarizes activitiesfrom August I to August 31, 1978.

For simplicity in reporting, activities are reported by subject matter rather than

by WBS item number.

MEETINGS, REVIEWS AND MAJOR ACTIVITIES

Activities during August were as follows (personnel attending the meetings if notlisted herein are tabulated in Appendix B of this report):

o An overall program review and site status meeting was held at Dunham-Bush,Harrisonburg, Va., on August 2 and 3 to discuss methods and costs forprogram acceleration. Mssrs. Paul Benson and John McPherson of AiResearchattended along with Charles Reichelderfer of Dunham-Bush and James Clarkof NASA/MSFC.

o A contractor/owner interface meeting was held at Lawrenceburg, Tenn., onAugust 18. Pertinent details are summarized in the SITE ACTIVITIES section.

" A contractor/owner interface meeting was held at Portland, Ore. on August23 to review equipment envelopes, location and method of installation forthe Redmond, Oregon, site with Bonneville Power Authority (BPA) personnel.

o An overall progran review meeting was held at Torrance, Calif., on August24, 25 and 28 with NASA/MSFC representatives and system component engineersin attendance. A complete review of development and delivery problems was presented for each component by the cognizant engineer.

o A technical review meeting was held at Clear Lake City, Texas, on August 23between Mr. Gordon Neff of Timmerman Engineering, Inc. and Robert Susagof AiResearch to resolve equipment interface details.

Meetings schedule for the month of September include­

o A contractor/owner interface meeting at Clear Lake City, Texas, on September7 and 8, 1978.

o A contractor/owner interface meeting at Redmond Ore., on September 12, 1978.

* A site review meeting in late September at Harrisonburg, Va.

SITE ACTIVITIES

Status of Sites

1. Lawrenceburg, Tenn. (OTS No. 13)

The site house has been surveyed. Solar collectors are in place and hoses

are now being clamped to the panels. The storage tank and expansion tanks are plumbed

76-13110(2)=AZaw AIRESEARCH MANUFACTURING COMPANY

or CALIFORNIA

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and await the heat pump. This site requires a pressure test and leak check procedurefrom AiResearch (which are in process). The IBM supplied SDAS and junction box areon hand. Four automatic air vents (to be used in the collector loop) have arrived.The site instrumentation program (Dwg. IP7933779) was received from IBM/Huntsvillevia James Clark on August 28, 1978.

2. Allaire Park, N.J. (OTS No. 1I_

The fwo storage tanks for this site have been ordered by AiResearch. A and Ebid packages were mailed August 21, 1978. The bid due date is September 7. Finalresolution of AIP and PIP differences is being delayed pending IBM response to AiResearchlist of questions given to Mr. Clark during August 28 program review meeting. The siteinstrumentation program (Dwg. IP7933777) was also received on August 28, 1978.

3. Harrisonburg, Va. (OTS No. 14)

The solar collector system is completed. A 550-gallon storage tank has beenpurchased locally and installed in the basement. Plumbing has been completed tothe heat pump interface. Trunk ducts have been installed but branch ducts to the individual outlets are not yet complete. Comments have been received per teleconfrom IBM regarding differences between AIP and AiResearch ISPI submitted June 27, 1978.AiResearch questions for IBM were given to James Clark on August 28, 1978.

1

4. Novato, Ca. (OTS No. 12)

The preliminary bid package will be shipped early in September. The preliminaryinstrumentation plan (PIP) was transmitted to NASA on September 6, 1978. Determinationof bid participants will occur throughout September, and contract award is anticipatedby October 27, 178.

1

5. Redmond, Ore. (OTS No. 17)

The Bonneville Power Authority (BPA) meeting with AiResearch at Portland, Oregon,revealed that heat pimp access to the site mechanical roan was not possible without modifying the entry to this room. Alternate heat pump locations in the storage/lunchroom, the vehicle storage room and a "doghouse" addition were discussed but all wererejected. BPA will finalize storage tank dimensions by mid-September, and will provideexpansion tank details shortly. BPA will purchase its own storage tank and cooling tower.'BPS sent a conceptual design package to AiResearch on August 14, 1978. AiResearch willreview the design and advise BPA of any recommendations in September.

6. St. Louis, Mo. (OTS No. 16)

A Cleveland, Tennessee, site is now being evaluated in lieu of the St. Louisvocational center.

7. 4 Houston, Tex. (OTS No. 18)

The technical review meeting at the site on August 23 1978 was to resolve systeminterface details between the heat pump and adjacent components. An AIP, dated June15, 1978, was received on August 28, 1978 which reflected Revision B ISPI valuespublished March 6, 1978. Since that time, three revisions have been published, The

~76-131 IO(21) AIRESEARCH MANUFACTURING COMPANY

OF CALIFORNIA

B-2

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latest, Revision E, was published on August 31, 1978, to finalize power requirements.

8. las Vegas

Building construction is still in progress at this site. A purchase order for thestorage tank has not been received at this time. Revision E is to be submitted toNASA in early September reflecting finalized wattmeter requirements.

Site and Site Equipment Status Charts

Site status Chart I has been updated to reflect agreements made during the Augustprogram review meeting. Charts 2 through 5 have not been revised this month and thus,are not included in this report. Chart I is included as Appendix A of this report.

Status of Preliminary and Approved Instrumentation Plans (PIP-AIP)

Site Revision Remarks

Allaire Park, N.J. B Delta Approved Instrumentation Plan (AIP) received7-17-78. Final PIP to be submitted by September 22,1978.

Lawrenceburg, Tn. A AAIP received 7-17-78. Final PIP to be submittedby September 22, 1978.

Harrisonburg, Va. Geo. Mizell of IBM/Huntsville requested changes ororiginal ISPI per telecon on 7-28-78; revised PIPto be Issued by September 29; 1978.

Novato, Ca. - Preliminary PIP issued September 5, 1978.

St. Louis, Mo. - No action; site not yet determined.

Redmond, Ore. - Preliminary PIP to be issued by September 29, 1978.

Houston, Tx. E PIP submitted August 31, 1978, with finalized powerrequirements and corresponding wattmeters.

Las Vegas, Nv. E PIP submitted Septemner 8, 1978 to agree with latestAIP (dated 7-26-78) except for updated power require­ments.

PROGRAM DOCUMENTATION

a. Twentieth Monthly Status Report 76-13110(20), dated August 10, 1978(DRSOO-ll).

b. Quarterly Contractor Financial Management Report (DR500-27).

Other publications were submitted during July to the parties listed as tabulatedbelow:

SubmittalDate To Subject

8-9-78 W. Johnson (Tiberti Construction Storage Tank Drawing H-TX-M2-2,

Co., Las Vegas) Rev. F, for Las Vegas InstallationDetails

8-16-78 J. Clark (NASA/MSFC) Conditional Approval Comnents reNASA Technical Directives 17 and 18

8-17-78 T. Swanson (Mueller Assoc., Inc., Transmittal of NASA SHC-3097 (June 1,Baltimore, Md.) 1978) Instrumentation Installation

Guidelines

8-31-78 C.W. Downing (NASA/MSFC) Revised Estimate of ContractVariance at Completion

AIRESARCH MANUFACTURING COMPANY OF CALIFORNIA B 3 76-13110(21)

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SYSTEM DEVELOPMENT

The activities reported below involve heat pump component design, fabricationand testing, and heat pump package development.

Component Design, Fabrication and Test (at AiResearch)

1. Turbomachines

(a) 3-Ton Unit

After flush cleaning and reassembly of the heat pump system (after failureof the carbon reversing valveTesting was then delayed by failure of a commutator sensor. After part replace­ment, the unit experienced mode "hitting" problems at high speed. Subsequentexamination attributed the rotating assembly hitting to excessive sway space. Theturbomachine unit was being rebuilt with stiffer bearing support spacers toreduce the sway space at month end.

(b) 25-Ton Unit

Testing of the 25-ton unit is at the subsystem level at Dunham-Bush. (Referto the heat pump test section below).

c) 75-Ton Unit

Testing of the 75-ton turbomachine is at the subsystem level at Dunham-Bush.(Refer to the heat pump test section below.)

2. Motor Controller

(a) 3-Ton Controller

Tests are being conducted on the heat pump package at AiResearch.

(b) 25-Ton Controller

Controller No. I is at Dunham-Bush awaiting completion of the dual heat pumptest setup. The fabricatior of Controller No. 2 is now complete and thetesting of this controller has commenced.

c) 75-Ton Controller

Controller No. I is being tested with the heat pump package at Dunham-Bush.The checkout of Controller No. 2 is awaiting availability of a motor.

3. System Controller

Five controllers have been completed and checked out. Fabrication o thefinal three system controllers has started.

AIRESEARCH MANUFACTURtING COMPANY 76-13110(21)L~J OFCALIFORNIAB­

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4. R-11 Liquid Pum2

(a) 3-Ton Unit

Three pump units were delivered in March. Testing is now at the subsystemlevel.

(b) 25-Ton Unit

One pump has been tested and shipped to Dunham-Bush. Assembly of the othertwo pumps is being held in abeyance pending system test evaluation.

Heat Pump Desiqn, Fabrication and Test (Dunham-Bush Activity)

1. Assembly of Units (at Dunham-Bush)

(a) 3-Ton Heat Pump

Two of the four 3-ton heat pumps have been revised to include changes similar to the 75-ton heat pump changes noted below. Revision is in process on the thirdheat pump and the fourth will be changed when it is returned from AiResearch.

(b) 25-Ton Heat Pump

The first 25-ton heat pump has been modified to incorporate changes similarto those made on the 75 -ton unit. The second is approximately 50 percent assembled.

(c) 75-Ton Heat Pump

In accordance with the request from Mr. Jim Clark, all piping interfaces havebeen brought to the edge of the heat pump and equipped with flanges.

To facilitate the flow of RIl to the refrigerant pump, the liquid outlet fromthe condenser was changed from the side to the bottom. A vortex eliminator wasplaced in the outlet and a direct connection was made to the refrigerant pump.The first unit is again ready for operation as soon as the compressor is receivedfrom AiResearch.

The second 75-ton heat pump is about 75 percent completed.

2. Test Activities (at Dunham-Bush)

The 75-ton heat pump operated for two days. On the third day, the turbo­compressor speed would not stay at 12j000 rpm and on each successive start,it stalled sooner untii, on the fourth attempt, itwould not start.

The compressor was disassembled and a badly burned thrust bearing was found. The grooves feeding refrigerant to the thrust bearing were too small. Thesegrooves were milled out to 9 times the original area and the compressor was thenreassembled with new thrust bearings. The same alteration was made on the second75-ton machine.

776- 13110(21)B-

COMPANYMANUFACTURING

OF CLIFORNIAAIRESEARCH

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Both machines were bench-tested to adjust the commutator position sensor.Turbocompressor No. I was to be installed in the heat pump, but itwas out ofbalance, probably as a result of adjusting the sensors. The turbine wheel scrapedon the housing and this turbocompressor was shipped back to AiResearch.

The sensors-on turbocompressor No. 2 were adjusted and the turbocompressorseemed to operate satisfactorily. It was installed in the heat pump and the unitwas charged with 800 pounds of Ri. The turbocompressor was started and acceleratedto 12,000 rpm. It ran for about one minute, and suddenly decelerated as if heavilyloaded and the power was turned off. Power was reapplied for short periods severaltimes, but the unit would not start. The turbocompressor was removed and shippedback to AiResearch.

COMPANY B-6 t6-13110(21)AiRESEARCH MANUFACTURING OF CALIFORNIA

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Heat Test Size Unit Turbocom- Motor Freon Pump Start Time, Test Ship Intended

pressor Control Pump Complete Test Weeks Complete Date Site

33 Ton #1 8-15 at Air at Air 9-26 9-27 I 10-6 10-6 Harrisonburg

2 :2 at D-B at D-B at D-B 8-29 8-30 4 9-27 9-30 Lawrenceburg

#3 9-23 9-23 9-23 10-5 10-0 4 11-3 11-7 Allaire Park N.J.

#4 10-15 10-15 9-8 11-5 11-6 8 1-20 1-24 Noiato, CA

2b Ton #1 Shipped Shipped Shipped 9-5 9-12k II 12-5 12-8 Redmond, OR

#2 10-15 10-15 10-15 12-4 12-5 5 1-23 1-26 Unknown

75 Ton #1 Shipped Shipped Received 8-25 8-24 7 10-12 10-1 Houston, TX

#2 9-15 9-15 Received 10-16 10-17 II 1-23 1-26 Las Vegas, NV

*Testing of the 25-ton system will start at completon of dual testing svstem.

**This unit at AiResearch until 9-4p at D-8 9-11 modified by 9-18

> Heat Pump Delivery Schedule

-no M0C­

M-rt a

Sr

-4 M

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ATTENDEES TO AUGUSTSHAC COORDINATION MEETINGS

Lawrenceburq Tenn., Site Review Meettng (August 18, 1978)

Attendees:

Jim Clark (NASA/MSFC)Bob Gunner (NASA/MSFC)Floyd Rushing (Lawrenceburg)Hack Yee (AiResearch)

Redmond, Ore., Site Review Meeting (August 23, 1978)

Attendees:

Bob Gunner (NASA/MSFC) Motto Stanley (BPA/Electrical)Hack Yee (AiResearch) Jon Giard (BPA/Walia Walla Area Eng.)Jeffrey Johnson (BPAp Redmond, Ore.) Jose Aguilar (BPA/Mechantcal)Jim Clark (NASA/MSFC) Jack Elwood (BPA, BSCE RandD Coord.)Dave Hartmann (BPA System Engineer) Marvin E. Nelson (BPA, BSCE, Mech. Eng.)Gary Tyler (BPA/Architect)Robert Bourn (BPA/Structural)

Program Review Meeting at Torrance Calif. (August 24, 25 and 28)

(a) August 24, 1978

James Clark 1 (NASA/HtSFC) Claude Dorning (NASA/MSFC) Bill Richardson (NASA/MSFC) Dick Nelson 2 (AiResearch) Paul Benson 2 (AiResearch) Hack Yee 2 (AiResearch) Rov Brown (AiResearch) Carl Dolland (AiResearch) Al Silver (AiResearch) Frank Wetgand (AiResearch)

(b) August 28, 1978 (new attendees

Robert Susag (AiResearch)Paul Hildebrand (AiResearch)

'Attended all three days2Attended meetings on August 24 and 25

AIRESEARCH MANUFACTURING COMPANY 76-13110(21) OF CALIFORNIA APPENDIX B

B-8

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siGTI PAg BLA K RQT f5W

PART C

Twenty-Second Monthly Status ReportData Requirement No. 500-11

SOLAR HEATING AND COOLINGSYSTEMS DESIGN AND DEVELOPMENT

Contract NAS8-32091

76-13110(22)

October ' 10, 1978

Prepared for

George C. Marshall Space Flight CenterNational Aeronautics and Space Administration

Marshall Space Flight CenterHuntsville, Alabama 35812

AIRESEARCH MANUFACTURING COMPANYOF CALIFORNIA

C-i

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INTRODUCTION

This is the twenty-second monthly status report prepared by AiResearch Manufacturing Company of California under Contract NAS8-32091 for the NationalAeronautics and Space Adminstration Marshall Space Flight Center (MSFC). Thereport summarizes activities from September I to September 30, 1978.

For simplicity in reporting, activities are reported by subject matterrather than by WBS item number.

MEETINGS, REVIEWS AND MAJOR ACTIVITIES

Activities during September were as follows (personnel attending the meetingsif not listed herein are tabulated in Appendix B of this report):

* A contractor/owner interface meeting was held at Clear Lake City, Texason September 7 and 8, 1978 to clarify AiResearch/NASA/TEI site responsi­bilities and to review site equipment schedules.

* An owner/AiResearch interface meeting was held at Torrance, Calif., onSeptember 12, 1978 to provide BPA and C.T. Main Co. with preliminary dataconcerning heat pump weight and size data, heat pump control operation,and storage tank data.

" A presentation was made at the Third Annual SHAC R&D Contractors' Meeting,Washington, D.C. on September 27, 1978 by Robert Susag concerning thestatus and accomplishments of the subject SHAC system. Maurice Gundersonof AiResearch also attended.

" A design review meeting was held at Portland, Ore., on Sept. 27 to discussinstallation details for the heat pump and storage tank. AiResearchreleased a preliminary schematic diagram, SDAS preliminary instrumentationlist and heat pump wiring diagram of the meeting.

o An equipment status and site related discussion was held at Torrance, Calif.,with NASA on September 28, 1978. Drafts of intended technical directiveswere received from Mr. Clark.

" A meeting was held at Houston, Texas, on September 28, 1978, to reviewswitching and control details for the heat pump. A representative fromBarber-Colnuan was there for Indoctrination.

Meetings scheduled for the month of October include:

* A go-forward discussion between the owner and Mueller Associates, Inc.,at Allalre State Park, N.J., on October 3, 1978.

* An operational and maintenance presentation, to the Univ. of Houston Main­tenance groups. This meeting will be scheduled to coincide with the nextsite interface meeting.

* A site review meeting at Harrisonburg, Va., in late October.

*A copy of the presentation, and reproductions of the associated viewgraphs, asattached to this report as APPENDIX C.

OFCALIFORNIA C-I

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SITE ACTIVITIES

Status of Sites

1. Lawrenceburq, Tenn. (OTS No. 13)

- A SHAC.to~site inteFf-ce wiring diagram(AiResearch Drawing H-TENN-EI) was hand delivered to Jim Clark at Houston on September 7, 1978. In addition, various specification and clean, test and fill procedures regarding this site have been transmitted to the site director this month. (Refer to PROGRAM DOCUMENTATION section.)

2. Allaire State Park, N.J. (OTS No. 1])

Site activities are "on hold" pending discussions in October between thesite owner and Mueller Associates, Inc., regarding bid package changes toreduce the overall cost.

3. Harrisonburg, Va. (OtS No. 14)

Progress at this site remains essentially unchanged since last month. Thesolar collector system is complete and all the plumbing is done up to theheat pump connections. Only some small feeder air ducts and registers awaitfinal installation. SDAS instrumentation was received from IBM/Huntsvilleexcept for a current transformer and two probes. Installation will begin whenheat pump is received.

4. Novato, Ca. (OTS No. 14)

The technical specifications and drawinqs were received from Bridgersand Paxton Consulting Engineers, Inc. the A and E firm for this site, onSeptember 11, 1978. AiResearch is currently reviewing this package, alongwith Novato-PWC engineers and NASA personnel.

5. Redmond, Ore. (OTS No. 17)

Two BPA-Charles T. Main - AiResearch interface meetings were held. Duringthe first, technical data was submitted to BPA concerning direct-heat heatexchanger and the cooling tower design points, water circuit flow data andinsulation data. During the second meeting, a revised SHAC system schematicdiagram and instrumentation list were released to the owner and NASA, alongwith Heat Pump Wiring Diagram H-ORE-El, Heat Pump Assembly Drawing C473038and various photos marked with coded interfaces. At this timeBPA informedAiResearch of their decision to provide a room addition for the heat pumpand storage tank.

6. Cleveland, Tenn. (OTS No. 16)

A preliminary design data package was submitted to J.C. Thomasson andAssociates, Nashville, Tenn., an A and E firm contracted by the Cleveland,Tenn., Utilities Co. the owner of the potential SHAC site.

C-2 76-13110(22)AIRESEARCH MANUFACTURING COMPANY OF CAIFORNIA

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7. Houston, Texas (OTS No. 18)

Contractor interface difficulties have hampered progress at this sitecompounded by instrumentation changes in the Site Data Acquisition System.As a result of the September 7-8 meeting at Clear Lake City, Texas, andsubsequent related telecons, it appears that NASA considers AiResearch'sprovision of direct heat exchanger specific procurement information asImproper acceptance by AiResearch of the design responsibility of thisheat exchanger. Consequently, transfer of information between AiResearchand the University of Houston has been suspended, with all informationtransfer channels being routed through NASA. Final AiResearch commentson the Houston site AIP are being held pending written instructions fromNASA on correct submittal procedures. The September 28 meeting atTimmerman Engineers Inc., Houston was held to orient the local controlsfirm (Barber-Colman) of the heat pump mode selection automatic procedures.

8. Las Vegas, Nevada (OTS No. 19)

Direct-heat heat exchanger,design point data was released to NASA forthis site and the Houston site on September 14 and 15, 1978, in separate

letters. Dissemination of this data to the proper site authorities isrequested of NASA.

Sites and Site Euipment Status Charts

Site status Chart I has been updated to reflect agreements made during theAugust program review meeting. Charts 2 through 5 have not been revised this month

and thus, are not included in this report. Chart I is included as Appendix A ofthis report.

Status of Preliminary and Approved Instrumentation Plans (PIP-AIP)

RemarksSite Revision

Allaire Park, N.J. B Letter 89312-10837-045, dated 9-28-78,

Lawrenceburg, Tenn. A submitted to NASA with suggested revisions to AIP's for these three SHAC sites.

Harrisonburg, Va. - I

Novato, Ca. Preliminary PIP issued September 5, 1978.

Cleveland, Tenn. - Preliminary data submitted for owner

evaluation prior to interface meeting.

Redmond, Ore. Preliminary system sketch, wiring diagram and list of instrumentation released to

site owner and NASA.

Houston, Tx. Final PIP revisions made; awaiting NASA writ

directives on how to submit.

Las Vegas, Nv. E PIP submitted September 8, 1978 to agree witl

latest AIP (dated 7-26-78) except for update(

power requirements.

AIRESEARCH MANUFACTURING COMPAN4YC-L-JCF CALIFORNIA 7613-322

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PROGRAM DOCUMENTATION

a. Twenty-first Monthly Status Report 76-13110(21), dated September 10, 1978(DRSOo0-1).

b. Quarterly Contractor Financial Management Report (DR500-27).

Other publications were submitted during September to the parties listed astabulated below:

Submittal I Date To Subject

9-8-78 J. Clark Nipple Lengths for Novato, Ca., and Houston, Tx.,

(NASA/MSFC) SDAS Temperature Probes

9-14-78 J. Clark Direct Heat Exchanger Design Point (Houston Site)

9715-78 J. Clark Direct Heat Exchanger Design Point (Las Vegas Site)

9-15-78 Floyd Rushing r rdware Specs and Data Submittal for Lawrenceburg, (Lawrenceburg, Tenn. Tenn.)

9-19-78 J. Clark Direct Heat Exchanger and Cooling Tower Design Points - Redmond, Oregon SHAC Site

9-20-78 Floyd Rushing Directions for Cleaning Filling and Pressure Testing Various System Piping Loops for Lawrenceburg,' Tenn. Site

9422-78 Clyde Sercy Preliminary Data for Proposed SHAC Site at (Nashville, Tenn.) Cleveland, Tenn.

9-28-78 J. Clark 3-Ton SHAC System Test Site AIP Revisions 9-28-78 George Mizell Solar Collector and Heat Pump Drawings

SYSTEM DEVELOPMENT

The activities reported below involve heat pump component design, fabricationand testing, and heat pump package development.

Component Design, Fabrication and Test (at AiResearch)

I. Turbomachines

(a) 3-Ton Unit

System testing at AiResearch with the Dunham-Bush heat pump package wascompleted. The unit was operated in the motor-driven mode successfully but couldnot be operated in the turbine-driven mode with freon change levels up to andincluding 155 lbs. This was attributed to piping problems within the package.Changes had been initiated at Dunham-Bush to correct this. Other system changesat Dunham-Bush were not incorporated in this unit, so testing was ended and the heatpump package was returned to Dunham-Bush for rework. All subsequent testingwill be at Dunham-Bush.

76-13110(22)AIRESEARCH MANuFACTURING COMPANY

OFCALIFORNIA C-4

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During the testing at AiResearch, itwas concluded that duct alignment to thecompressor is very critical. It is anticipated that flex ducting will be requiredwithin the package to eliminate distortion.

(b) 25-Ton Unit

No testing has been acomplished during the past month. One unit is atDunham-Bush for system testing.

(c) 75-Ton Unit

One unit with increased thrust bearing cooling potential has been shippedto Dunham-Bush and is being installed in their system. Testing should begin thefirst week of October. The tests will determine the adequacy of the change andthe changes required to the motor controller to allow for full-load testing.

2. Motor Controller

(a) 3-Ton Controller

Unit No. I is at Dunham-Bush for heat pump system tests. Units No. 2 and 3are complete and are awaiting start of heat pump package testing. Unit No. 4fabrication is complete but has not received its final static test.

(b) 25-Ton Controller

Controller No. I is at Dunham-Bush awaiting completion of the dual heat pumptest setup. Controller No. 2 is completed and in its final static test. Thephase delay rectifier has been completed. Tests of the inverter and commutationcircuits are imminent.

(c) 75-Ton Controller

Controller No. I is being tested with the heat pump package at Dunham-Bush.The checkout of Controller No. 2 is awaiting availability of a motor.

3. System Controller

Five controllers have been completed and checked out. Fabrication of thefinal three system controllers is now 60 percent ccmplete.

4. R-11 Liquid Pump

(a) 3-Ton Unit

Three pump units were delivered in March. Testing is now at the subsystem level,

(b) 25-Ton Unit

One pump has been tested and shipped to Dunham-Bush. Assembly of the other twopumps was completed last month. Installation into the heat pump will be effectedthis month.

76-13110(22) t C-5

5COMPANY

OF CALIFORNIA AIRESEARC8 MANUFACTURING

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Heat Pump Design, Fabricat;on and Test (Dunham-Bush Activitiy)

I. Assembly of Units (at Dunham-Bush)

(a) 3-Ton Heat Pump

I Two of the four 3-ton heat pumps have been revised to include the latest develop­ment changes. Revision is in process on the third heat pump and the fourth will bechanged when it is returned from AiResearch.

(b) 25-Ton Heat Pump

I The first 25-ton heat pump has been modified to incorporate latest development

changes. The second is approximately 60 percent assembled.

(c) 75-Ton Heat Pump

The first 75-ton unit is complete and presently in system testing with a modifiedturbocompressor.

The second 75-ton heat pump is about 75 percent complete and wait-ing receipt of theturbocompressor for the remaining plumbing.

2. Test Activities (at Dunham-Bush)

(a) 3-Ton Heat Pump

Systems testing with the latest plumbing changes has started with the major effort

directed toward operation in the turbine-driven cooling mode. Testing will continueinto October.

(b) 25-Ton Heat Pump

The 25-ton package is complete and installed in the test system. The system is onvacuum and testing will start the first week in October.

(c) 75-Ton Heat Pump

A turbocompressor with improved bearing cooling passages was installed in the testsystem. Motor-driven operation indicated that the controller current range is limited,which will require evaluation by AiResearch Engineering. Photographs of specific waveforms have been transmitted. Operation of the R-ll pump is now satisfactory due to therecent plumbing changes. The turbocompressor thrust bearing appears to be running warmethan anticipated and a modification is in process on the second unit to provide addedlocalized cooling flow.

76-13 110(22)

c-6AIRESEARCH MANUFACTURING COMPAN' I I OF CALIFORNIA

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Size Unit Turbocom­pressor

Motor Control

Freon Pump

Heat Pump Complete

Start Test

Test Time, Weeks

Test Complete

Ship Date

Intended Site

A o

-

3 Ton #1

#2

43

+4

complete

complete

complete

10-15

complete

complete

complete

10-15

complete

complete

complete

10-15

10-26

complete

11-3

12-11

10-27

9-28

11-6

12-12

1

4

4

8

11-3

10-26

12-11

2-20

11-3

10-30

12-14

2-23

Harrisonburg

Lawrenceburg

Allaire Park, N.J.

Novato, CA.

25 Ton #l

2

complete

0-15

complete

10-15

complete

10-15

complete

12-4

9-27

1-2

11

5

12-20

2-6

12-22

2-9

Redmond, OR.

Cleveland, Tenn.

75 Ton #1

*2

complete

10-15

complete

10-15

Received

Received

9-25

11-14

9-26

11-15

7

11

11-14

2-14

11-17

2-16

Houston, TX.

Las Vegas, NV.

HEAT PUMP DELIVERY SCHEDULE

701-M

>O

- U"

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ATTENDEES TO SEPTEMBERSHAC COORDINATION MEETINGS

Design Review Meeting at Portland, Oregon (Sept. 27, 1978)

Attendees:

Jim Clark (NASA/MSFC) Jon Giard (BPA) Robert Gunner (NASA/MSFC) Marvin Nelson (BPA) Georgb Forsman (BPA) Harry Reeder (C.T. Main)* Del Ramey (BPA) Tom Ocheltree (C.T. Main) Stanley Mirecki (BPA) Ray Loofburrow (C.T. Main) Roger Sarkinen (BPA) Hal Bonslett (C.T. Main) Jose Aguilar (BRA) Dave Kelly (C.T. Main) Jeff Johnson (BPA) Hack Yee (AiResearch)

Equipment Status Meeting at Torrance, Calif. (Sept. 28, 1978)

Attendees:

Robert Gunner (NASA/MSFC) R. C. Nelson (AiResearch)Jim Clark (NASA/MSFC) Paul Hildebrand (AiResearch)

Hack Yee (AiResearch)

Houston, Texas, SHAD Control Interface Meeting (Sept. 28, 1978)

Attendees:

Ed Samfield (Univ. of Houston)Gordon Neff (Timmerman Engrg., Inc.)Robert Ice (Timmerman Engrg., Inc.)Paul Benson (AiResearch)Shing Leung (AiResearch)(and a controls engineer from Barber-Colman)

Contractor/Owner Interface Peeting at Torrance Calif. (September 12, 1978)

Attendees:

Hal Bonslett (C.T. Main) Paul Benson (AiResearch)Jose Aguilar (BPA) Robert Susag (AiResearch)

Hack Yee (AiResearch)

*A Portland, Oregon, A and E firm contracted by BPA for the Redmond site.

M "AIRESEARCH MANUFACTURING COMPANY

OF CALIFORNIA C-8 76-13 110( 22) APPENDIX B

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RANKINE HEAT PUM1RIIALPWBISOLAR POWERED A PROGRESS REPORT Q8 EQQR QtW Ta

by Robert W Susag and Paul A Benson

AlResearch Manufacturing Company of California2525 W 190th Street, Torrance, California

OBJECTIVE

This paper presents a brief description of the solar­powered Rankine cycle heat pump and an outline of the latest six-ionth progress of the AiResearch Hanu­facturing Company of California, Solar Heating and Cooling Project, on NASA Contract Number NAS-32091.

SUMMIARY

During this period, subsystem level development was dominant, with problem solving both at the component and subsystem level providing the program emphasis The progress was highlighted by completion of the following milestones

I Rankine cycle cooling achieved with 3-tonsubsystem

2 75-ton subsystem (to be Installed at the University of Houston) operated in electric cooling mode

Progress has been at a pace slower than desired, due to design changes found necessary in system develop- ment However, no problems of any appreciable technical magnitude have been confronted The program is technically healthy, and proceeding toward a successful conclusion

BACKGROUND

The AIResearch system features a solar powered vapor-cycle heat pump using R-l as the workingfluid The heat pump turbomachine consists of aturbine, a compressor and a permanent magnet motor mounted on the same shaft The rotor is supported on process fluid bearings, no lubricants other than the process fluid are required The motor Is powered In the electrical mode from utility power through a solid-state converter generating variable highfrequency, thus providing variable speed operation

Solar energy Is collected using flat-plate copper

collectors and the thermal energy is transported by a water-ethylene glycol fluid flowing In a closed loop The heat energy is exchanged through an Inter­cooler to a water loop which transports the energy to an insulated storage tank Temperature in thistank can vary from 40 F to 210aF depending only onthe differences in energy every collection endenergy usage

The system Is presently being constructed in threesizes, 3-ton cooling (110,00 Btu/hr heating), 25-toncooling (800,000 Btu/hr heating) and 75-ton cooling (2,003,000 Btu/hr heating). The

25 -ton system Is

best used as the descriptive baseline since this

syste alone utilizes all of the modes heating and cooling Differences In the operational modes ofthe 3-ton and the 75-ton are explained later

Heating Operation

In the heating mode, two methods of energy transport are utilized Direct heating Is utilized wheneverthe storage tank temperature Is sufficiently higherthan the temperature required to passively conductheat to the conventional hydronlc thermal transportloop This loop carries the heat energy to the airhandlers in the various zones of the building Theheat transfer Is accomplished through a direct heatexchanger between the storage tank output loop andthe hydronic transport loop.

Whenever the temperature in the storage tank is in. sufficient to accomplishing the full heating require­ments of the building in the direct heating mode, the syston is automatically switched to heat pump operation In this mode, electrical energy Is supplied to the motor on the turboconpressor shaft to cause heat energy to be actively elevated in temperature so that the heat energy may pass from the lower temperature in the storage tank to the higher temperature hydronic transport loop The electrical energy provided to the motor in this mode is controlled to a value just sufficient to accomplish the heat energy transmission required by the build-

Ing As the temperature of the storage tank decreases,

1"Xlo .n ALw

oss', Iw---o-.. I tvaOus"TOR -­ ---­

ton --f- r- tRANSPONo

T"K .01

v

H sxeHA emft

Figure 1. Heating Operation

Page I

3rd Annual Solar Heating and Cooling R&D Contractors' Meeting September 1978

76-13110(22)

an" AIRESEARCH MANUFACTURING COMPANY APPENDIX C OF CALIFORNIA C-9 Page C-1

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the heat pump becomes Incapable of supplying allthe heat required and a control signal isprovidedto activate a conventional water boiler which then supplies only the difference Inthe heat required and the heat available from the heat pump Should the storage tank water tdmperature approach the

-MVNfreezing point, the heat Pump is automatically stopped, and all of the building heating require­ments are supplied by the water boiler

In the heat pump mode of operation, the R-11 working fluid isevaporated at a low pressure In the sub-M system Input heat exchanger called the boiler/ araporetor. Heat is extracted from the water In the thermal storage tank by the evaporation process, and the higher energy fluid Is compressed by the con­pressor and condensed In the output heat exchanger named the evaporator/condenser The higher pressure condensing process provides a heat source at asufficient temperature level for the building heattransport loop The liquid R-I1 Isconducted backto the expansion valve, thus closing the vaporcycle loop.

dooling Operation

In the cooling mode of operation, the R-1I working fluid isused simultaneously In two operationally separate vapor cycle loops, although these loops are actually physically combined through the use of a common condenser. In the Rankine cycle drive loop, thermal energy Is transported from the storage tank to the Input heat exchanger (boiler) where It Is used to vaporize the Working fluid at high pressure (about 85 psla) The high pressure (high energy) vapor isexpanded in the turbine to provide shaft power for the centrifugal compressor of the refrig­eratlon loop The expanded vapor from the turbine Is liquifled In the commnon condensor, and pumped back to the expansion valve at the boiler Inlet, thus closing the Rankine power loop In the refrigeration loop, the R-Il Is vaporized in the output heat exchanger (evaporator) at a low pressure, thus pro-viding cooling by lowering the temperature of thehydronic heat transport loop which supplies the various air handlers located In the building Thelow pressure vapor fron the evaporator Is compressed end combined with the turbine outflow before enter-Ing the condenser, where the vapor Is condensed through energy extraction by a water tower transport Ioop. Liquid R-l Is returned to the evaporatorthrough en expansion valve

Whenever sufficient energy Isavailable In the storage tank (as depicted by the storage tank water temperature), the Rankine power loop is capable of supplying all of the shaft power required to drive the compressor, and the electric motor requires no power other than that required to initially startthe turboconipressor The speed of the turbocompressor varies naturally dependent upon the operating conditions If the stored solar energy Is insufficientto maintain a minimum compressor speed, electric power is automatically supplied to the motor to augment the turbine power. If no thermal energy Is available to the turbine, the Rankine loop Is functionally terminated and the entire requirementsof the refrigeration loop are supplied by the electric motor drive subsystem.

-----A,-.....­---- .....

/Cr ace.MntI

m WW*osVApotos

I L inuaio Woensaa vO0rTAAK

Pan, toWW.

Figure 2. Cooling Operation

Hinor variations In the-preceeding description exist In the 3-ton and the 75-ton systems. The 3-ton (single family, one zone) system utilizes an output heat exchanger (evaporator/condenser) In which building air Iscooled or heated directly, negating the requirement for a hydronic transport loop Design studies have Indicated that a passive energy transfer from the storage tank directly to the unit output air Is Impractical, and consequently no direct heating mode exists In the 3-ton unit Conversely, the 75-ton system does hot employ a heat pump heating mode due to the environmental nature of the two test sites selected for this system Both the Las Vegas and Houston areas do not require the heat pump heating mode since the heating requirements are most satisfactorily supplied by the direct heat-Ing mode

TECHNICAL ACCOMPLISHMENTS

During the past six months, significant progress hasbeen mad., both in the component and subsystemdevelopment areas. The following is a brief synopsisof the highlights of the development program

Turbocompressors

1.Compressor performances have been confirmed (3-ton and 25-ton)

2. The process fluid bearings have been optimizedin all three sizes of machines

3 The motor/motor controller Interface has beenperfected to a high degree of confidence

4 A single-center rotating section was designedto replace the multiple piece rotating section to reduce (3-ton) unit rotor runoutproblems.

5.Maximum speeds have been reached withoutIncident on all machines

6 Motor end bearing coolant circuits have beenImproved on all three sizes of machines

Ox u-Page 2

3rd Annual Solar Heating and Cooling R&D Contractors' MeetingSeptember 1978

76-13110( 22) AIRESEARCH MANUFACTURING COMPANY APPENDIX C

OF CALIFORNIA C-10 Page C-2

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Froom Pumss

I. High officlency freon pumps wmre developed-andlife tested satisfactorlty in 3-ton amm23-tc s Fees.

Motor Controllers

Motor controllers utilizing transistor comtatlng circuits (3-ton) and thyristor oimmtating circuits (25 and 75-ton) have been developed ad are presentlyetibiting excellent overall caabllIty In subsystem development tests.

Revers1ng Vaies

Reversing valves In S-ton and 25-ton sies are presently being tasted at the subsystes level. Initial units using carbon pistons proved Inadequate and have been replaced with units constructed with cast iron pistons In chros.plated bore steal housings. These units have recently received minor changes in configuration, and are now.expected to meat the sub­system requIrments.

Subsystem

The subsystem developmnt progress has reached the deliverable hardware testing phase. Presently, 3­ton heat pump units scheduled for delivery to the Lawrenuebrg, Tennessee test site, and the bowhae Bush -test house are In final subsystem testing.A 25-ton heat puM unit, scheduled for the Redond,Oregon test site and a -ton unit scheduled forthe University of Houston test site .re also In finalsubsystem testing. Delivery of these units Isexpected In the next several weeks.

ORIGINGAL PAGE LI

04 ROOji QUALrz

page 3

3d ASd Solm Headng and Coolig M Cmaa MeeihgSopko.W*1978

76-13110(22)AIRESWARCH MANUFACTURING COMPANY APPENDIX C

OFCALIFORNIA c-i1 Page C-3

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3-TON RANKINE CYCLE SOLAR HEATPUMP FOR LAWRENCEBURG,

TENNESSEE SITE (SIDE VIEW SHOWING CONDENSER,

INTERCHANGER, AND EVAPORATOR-CONDENSER)

OS 79 QUAUfl

76-13110(22)MRESAKHc MANUFACTURIN COMPAKY APPENDIX C

Page C-4

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3-TON RANKINE CYCLE SOLAR HEATPUMP FOR LAWRENCEBURG,

TENNESSEE SITE(BOILER-EVAPORATOR SIDE VIEW)

DiPOO)R QUAIZI

rr~i76-13110(22) NyjSLCH MNWAtURING COMPAN APPENDIX C

OFCAuORNIA C-13 Page C-5

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25-TON RANKINE CYCLE SOLAR HEAT PUMP FOR REDMOND, OREGON SITE

(SIDE VIEW)

I IMmr

~76-13110o(22) AIRsURRCn ANUFACrURING CO.PANY C­ 14 APPENDIX C

OF CALIFORNIA Page C-6

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25-TON RANKINE CYCLE SOLAR HEATPUMP FOR REDMOND, OREGON SITE

(CONDENSER-EVAPORATOR END VIEW)

176-13110(22)

ARESEARCH MANUFACURING COMPANy C-15 APPENDIX C OF CALIFORNIA Page C-7

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25-TON RANKINE CYCLE SOLAR HEATPUMP FOR REDMOND, OREGON SITE

(EVAPORATOR-BOILER END VIEW)

~76­ 1311|0(22) AIRESEARCH MANUFACTURING COMPANY APPENDIX C

Of CAFORNIA C-16 Page C-8

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TEST OF 75 - TONRANKINE-CYCLE SOLAR HEAT PUMPFOR UNIVERSITY OF HOUSTON SITE

F-28113

3~E.F-28130

Of POO% ..

76-13110(22)MRESEARCH MANUFACTURING COMPANY C-17 APPENDIX C

OF CALIFORNIA Page C-9

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TEST OF 75-TON RANKINE CYCLE SOLARHEAT PUMP FOR UNIVERSITY OF

HOUSTON SITE(EVAPORATOR END VIEW)

C-18 76-13110(22) AIRESEARC MANUfACTUlING COMPANY APPENDIX C

OF CALIFORNIA Page C-1O

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TEST OF 75-TON RANKINE CYCLE SOLARHEAT PUMP FOR UNIVERSITY OF

HOUSTON SITE(BOILER END VIEW)

CILIGNAr P=D m3OF POOR QUAUTr4

C-19 76-13110(22) AIRESEARCH MANUFACTURING COMPANY APPEND IX C

OF CALIFORNIA Page C-II

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75-TON RANKINE CYCLE SOLAR HEATPUMP FOR UNIVERSITY OF HOUSTON

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