37
Presented By Grant C. Bue Spacesuit Water Membrane Evaporator; An Enhanced Evaporative Cooling Systems for the Advanced Extravehicular Mobility Unit Portable Life Support System Grant C. Bue, Janice V. Makinen, Sean Miller, Colin Campbell NASA Johnson Space Center, Houston, Texas, 77058 Bill Lynch, Matt Vogel, Jesse Craft, Brian Petty Jacobs Engineering, Inc., ESCG Houston, Texas, 77058 Thermal & Fluids Analysis Workshop TFAWS 2014 August 4 - 8, 2014 NASA Glenn Research Center Cleveland, OH TFAWS Active Thermal Paper Session

Spacesuit Water Membrane Evaporator; An Enhanced

  • Upload
    others

  • View
    1

  • Download
    0

Embed Size (px)

Citation preview

Page 1: Spacesuit Water Membrane Evaporator; An Enhanced

Presented ByGrant C. Bue

Spacesuit Water Membrane Evaporator; An Enhanced Evaporative Cooling

Systems for the Advanced Extravehicular Mobility Unit Portable Life

Support SystemGrant C. Bue, Janice V. Makinen, Sean Miller, Colin Campbell

NASA Johnson Space Center, Houston, Texas, 77058

Bill Lynch, Matt Vogel, Jesse Craft, Brian Petty Jacobs Engineering, Inc., ESCG Houston, Texas, 77058

Thermal & Fluids Analysis WorkshopTFAWS 2014August 4 - 8, 2014NASA Glenn Research CenterCleveland, OH

TFAWS Active Thermal Paper Session

Page 2: Spacesuit Water Membrane Evaporator; An Enhanced

Overview• SWME Design Criteria• Previous Design

– Pre - Gen. 4 design– SWME Gen. 4 early concepts

• Current Design– Housing Modification– End cap Modifications– Back Pressure Valve Modifications

• Thermal Control Valve (TCV)• Sensor Selection

2

Page 3: Spacesuit Water Membrane Evaporator; An Enhanced

Scope and Background

• What is SWME?– Spacesuit Water Membrane Evaporator– Baseline heat rejection technology for the Portable Life Support System of the

Advanced EMU• Replaces sublimator in the current EMU• Contamination insensitive• Can work with Lithium Chloride Absorber Radiator in Spacesuit Evaporator Absorber Radiator

(SEAR) to reject heat and reuse evaporated water

Page 4: Spacesuit Water Membrane Evaporator; An Enhanced

Background

4

The Spacesuit Water Membrane Evaporator (SWME) is being developed to replace the sublimator for future generation spacesuits.

Current PLSS

Advanced PLSS

…relies on a sublimatorfor LCVG and PLSS component cooling

Sensitive to contaminants

Only certified for 25 EVA’s: Has failed before 25 EVAs (during EVA)

Requires a separate feedwater loopWill not work on Mars due to increased

atmospheric pressure

Create a new, robust heat rejection device for

future:

Reject at least 807W at 10˚ C (50˚ F) outlet water temperature at EOL

Operate for at least 100 8-hour EVA’sFunction in multiple EVA environments (Lunar,

Mars, Vehicle)

Resist contaminant fouling

Page 5: Spacesuit Water Membrane Evaporator; An Enhanced

SWME Overview

Process• Water in LCVG absorbs body heat

while circulating • Warm water pumped through SWME• SWME evaporates water vapor, while

maintaining liquid water– Cools water

• Cooled water is then recirculated through LCVG.

• LCVG water lost due to evaporation (cooling) is replaced from feedwater

5

Water vapor is exhausted to space from

SWME, removing heat

Cooled water is pumped back into LCVG

SWME

Warm water from LCVG pumped into

SWME

SWME is an evaporative cooler

Page 6: Spacesuit Water Membrane Evaporator; An Enhanced

SWME

6

Hollow Fibers

Polyurethane Plug

Back Pressure Valve

Instrumentation PortsWater Inlet

(warm water from LCVG)

Water Outlet

(cool water to LCVG)

CageValve

Position Sensor

Page 7: Spacesuit Water Membrane Evaporator; An Enhanced

New Design Goals for Gen4 SWME

• Function– Meet or exceed earlier design requirements– 810 W heat rejection at end-of-life– Minimize or eliminate water vapor leak– Protect for over/under pressure conditions– Sense valve position– Maximize controllability over the lower metabolic range; to increase crewmember

comfort.

• Form– Maximize packaging efficiency for incorporation into PLSS 2.5

• Square profile• Minimize volume of SWME housing • Integrate the Thermal Control Valve (TCV), delta pressure, and temperature sensors into the

SWME assembly

Page 8: Spacesuit Water Membrane Evaporator; An Enhanced

SWME Gen. 4 Early Concept

8

Sliding Gate ValveIntegrated

TCV Port

Page 9: Spacesuit Water Membrane Evaporator; An Enhanced

SWME Gen. 4 Early Concept

9

Dual BoreO-ringsSquare

Profile Fiber Cartridge

Page 10: Spacesuit Water Membrane Evaporator; An Enhanced

SWME Views (Cont.)

Page 11: Spacesuit Water Membrane Evaporator; An Enhanced

Current SWME Concept

11

New Dual Back Pressure

Valve

Independent TCV Manifold

Page 12: Spacesuit Water Membrane Evaporator; An Enhanced

Current SWME Concept

12

Open Walled Housing Design

Offset BPV Motor

Page 13: Spacesuit Water Membrane Evaporator; An Enhanced

Design Modifications

• The Independent TCV Manifold reduces design complexity and manufacturing difficulty of the SWME End Cap.

• The offset motor for the new BPV reduces the volume profile of the SWME by laying the motor flat on the End Cap alongside the TCV.

13

Page 14: Spacesuit Water Membrane Evaporator; An Enhanced

New Housing Design

14

Page 15: Spacesuit Water Membrane Evaporator; An Enhanced

• Side walls were opened up for:– Better access during assembly

• A bead of polyurethane can be run on the inside of the cartridge now to prevent urethane leak during potting.

• Easier leak identification and repair.– Ease of manufacturing

• More generous tolerances • Standard and quicker machining

methods can be used– Modularity of design

• 4 open sides allow for more options such as relief valves to equalize pressure in an off-nominal repress/depress

Housing Modification

15

New

Old

Page 16: Spacesuit Water Membrane Evaporator; An Enhanced

End Cap

• Simplified End Cap with separation of TCV Manifold.

• Moved O-ring gland from bore O-ring on housing to face seal O-ring on End Cap.– Better Sealing Method– Serpentine pattern

allows for generous bend radii on square cross section and COTS o-ring

• Increased surface area to allow for face seal

Note: Final design will have thicker edge distances on O-

rings

Page 17: Spacesuit Water Membrane Evaporator; An Enhanced

• Reduce total SWME volume envelope through low profile– Facilitates PLSS packaging

• Allow for pressure differential equalization• No heat leak during non-op periods• Finer control at lower metabolic rates• High cycle life capability• 4 in2 open area

Back Pressure Valve goals

17

Page 18: Spacesuit Water Membrane Evaporator; An Enhanced

Gen2 SWME BPV Characterization

18

05101520253035404550556065707580859095100

050

100150200250300350400450500550600650700750800850900950

1000

0 2 4 6 8 10 12 14 16 18 20 22 24 26 28

Valve T

ravel (%),M

otor Steps (%), qrej (W

)

Heat Rejectio

n (W),De

lta M

otor Step

s

BPV Position

Heat Rejection (W)

Motor Steps To Move to Next BPV Position

% Valve Travel per Pot Voltage

% Number of Motor Steps

Delta Heat Rejection (W)

• Opening the valve 25% resulted in an SWME heat rejection of 66% of its full open BPV value

• The last 75% of valve poppet travel accounted for the final 34% of SWME heat- rejection capability.

Page 19: Spacesuit Water Membrane Evaporator; An Enhanced

Secondary PortPrimary Port

• Ports open sequentially.

• Smaller Primary port allows for finer

control at lower metabolic rates.

• Larger Secondary port provides higher flow volumes when

needed at higher metabolic rates.

Back Pressure Valve

Page 20: Spacesuit Water Membrane Evaporator; An Enhanced

Lever Arm

Springs on Shoulder

Bolts

Pivot

Sealing Plate

Springs on Shoulder

Bolts

Sealing Plate

Torsion Springs on pivot arms

Back Pressure Valve (Cont.)

Page 21: Spacesuit Water Membrane Evaporator; An Enhanced

3.25” diameter0.75” diameter

BPV Base Plate

Page 22: Spacesuit Water Membrane Evaporator; An Enhanced

View from inside

BPV Base Plate (Cont.)

Page 23: Spacesuit Water Membrane Evaporator; An Enhanced

Side View – Valves Closed

Cutaway View

Sealing Plates - Closed

No ContactPin in Lever Arm contacts

Short Arm

Pin contact holds plate closed

Valve Mechanism

Page 24: Spacesuit Water Membrane Evaporator; An Enhanced

Cutaway View

Valve Mechanism (Cont.)

Page 25: Spacesuit Water Membrane Evaporator; An Enhanced

Small Lever Travel

full gap

Mid Range Lever Travel

Full Lever Travel

small gap

medium gap

full gap

closed

Initial Pin Contact

theshold position

Valve Mechanism (Cont.)

Page 26: Spacesuit Water Membrane Evaporator; An Enhanced

Pros:• Smaller Primary port allows for finer control at lower operation

rates.• Larger Secondary port provides higher flow volumes when needed.• Parallel linkages keep the sealing plates from tilting.• Multiple linkages stop sliding motion on O-rings when compared to

single linkage.Cons:• Multiple linkages increase part count and complexity• Multiple pivots increase risk of valve “sticking”

BPV Pros and Cons

Page 27: Spacesuit Water Membrane Evaporator; An Enhanced

Integration - TCV

• Improved PLSS Packaging– Fewer tubing runs– Fewer retaining brackets

• Less instrumentation– Removal of redundant temperature

sensors

• Closer proximity of thermal loop controller to components

Page 28: Spacesuit Water Membrane Evaporator; An Enhanced

Integration – TS 439, 441

• Measure SWME inlet and outlet temps– TS-441 replaces TS-401 (TCV Inlet Temperature)

• COTS 1k RTDs– Standard temperature sensor for PLSS 2.5– O-ring Boss Port Interfaces

Page 29: Spacesuit Water Membrane Evaporator; An Enhanced

Integration – DP-425

• Measures dP across SWME• Loss of flow triggers SWME safing• Provides coarse thermal loop flow measurement• 1/8 in tubing runs from inlet and outlet • Sensor selection in-work

Page 30: Spacesuit Water Membrane Evaporator; An Enhanced

Integration – DP-425

• Current volume constraints require sensor be placed on top of SWME

DP-425(stand-in)

Page 31: Spacesuit Water Membrane Evaporator; An Enhanced

Integration - Endcaps

• Allow design of individual components in parallel with packaging and integration

• Reduced machining risk– Complexity of endcaps and risk of scrapping will not affect the

entire SWME housing

• Pressure and temperature sensors can be placed anywhere– Allows optimal placement of SWME gate valve

Page 32: Spacesuit Water Membrane Evaporator; An Enhanced

Inlet Endcap

SWME Inlet- 3/8 in line- face seal interface

TS-439

DP-425 Penetration

- face seal interface

Page 33: Spacesuit Water Membrane Evaporator; An Enhanced

Inlet Endcap

Page 34: Spacesuit Water Membrane Evaporator; An Enhanced

Outlet Endcap

• Currently, length is most packaging-critical dimension• All large-volume components kept on one endcap to

minimize swept volume– Valve Motor– TCV-421

Page 35: Spacesuit Water Membrane Evaporator; An Enhanced

Outlet Endcap

TCV-421

SWME Gate Valve Motor

TS-441DP-425 Penetration

Page 36: Spacesuit Water Membrane Evaporator; An Enhanced

Outlet Endcap

Page 37: Spacesuit Water Membrane Evaporator; An Enhanced

Integration Forward Work

• Components still under development: – SWME Valve– SWME Fiber Count

• FDTA testing– Mini-ME2

• Will be based on lessons learned and data from Gen4– TCV-421– DP-425

• As these components continue to be developed and optimized, the integration concept will update as well