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Photo Courtesy of Department of Defense BH112JD Series JETCAL® 1 Engine Analyzer The BH112JD JETCAL® Engine Analyzer provides a superior combination of capabilities in a ruggedized, portable test set. The BH112JD JETCAL® Engine Analyzer is designed to: Functionally check and troubleshoot the temperature measuring system in aircraft turbine engines without running the engines, saving fuel and engine life. Accurately monitor, record and print critical engine parameters during engine trim. Input Parameter Flexibility Basic engine test parameters-temperature, speed and pressure-can all be scaled to the exact requirements of the engine being tested. Temperature can be displayed in °C or °F. Engine speed can be scaled in %RPM, direct RPM or in frequency (Hz). Externally measured pressure can be displayed in inHg, psi, ft-lb or %Torque. Internally measured pressure can be displayed in inHg or psi. Engine Select Switch allows the operator to select the specific calibration and scale factors appropriate for the engine under test. Scale factors can be easily entered into memory for up to ten different engine types. • Instructional prompts are provided on the tester display throughout the scaling procedure. • Scaling information is retained permanently in memory unless changed by the operator. Howell Instruments, Inc. 8945 South Freeway Fort Worth, Texas 76140 www.howellinst.com 817-336-7411 Fax: 817-336-7874 [email protected] PORTABLE ENGINE TEST SETS & TRIMMERS PORTABLE ENGINE TEST SETS & TRIMMERS PROBE TEMP SET 6 7 8 0 2 5 TEMP SELECT ON PROBE POWER HEATER CABLE HEATER CABLE INTERCONNECT INTERCONNECT POWER INLET CABLE SPREAD ADAPTER CABLE JUNCTION BOX ASSEMBLY HEATER CABLE INTERCONNECT CABLE POWER INPUT FUSE - 20 BUSS FUSE - 20 HEATER PROBE SPREAD ENGINE HARNESS STAINNER INPUTS HOWELL INSTRUMENTS, INC. FORT WORTH, TEXAS U.S.A. HEATER PROBE A Probe Control Module B C E D F A Interconnect - Provides connection to Trimmer Section. B Power Input - 115 or 230 VAC, 50 to 400 Hz, Single Phase Main Power Input C Spread Cable - Connection for Spread Cable. D Heater Cable - Connection for power and temperature signal to Junction Box or Heater Probe. E Junction Box - Heater probe terminal connection. F Heater Probe (model no. and quantity determined by engine application). Probe Control Module Howell Instruments, Inc. 8945 South Freeway Fort Worth, Texas 76140 www.howellinst.com 817-336-7411 Fax: 817-336-7874 [email protected] ©2009 Howell Instruments, Inc. PET112JD Cockpit Temperature Indicator Test The tester provides a simulated thermocouple output to check the calibration of high impedance (null balance) or low impedance (current drawing) temperature indicators. Thermocouple Harness Tests The accuracy of current drawing engine temperature indicators is dependent upon the resistance of the thermocouple harness. The BH112JD can be used to accurately measure the resistance of any harness to 40 ohms, as well as insulation resistance to 200,000 ohms. Probe Control The Probe Control Section contains the power supply and controls required for the operation of the heater probes, including the connector and switch required to perform spread tests. To test the engine thermocouple harness, a heater probe is placed over each engine thermocouple. The BH112JD JETCAL® Analyzer controls the power applied to the probes to maintain them at a preselected test temperature. Since the probe is precisely fitted to the engine thermocouple, the probe and thermocouple are maintained at the same temperature. A thermocouple embedded in the probe accurately measures the probe temperature. If the aircraft thermocouple temperature displayed on the JETCAL® Analyzer or cockpit indicator is outside the acceptable probe temperature specified in the manual, a malfunction is indicated. The JETCAL® Analyzer can then be used as a troubleshooting device to check cockpit temperature indicator calibration, thermocouple harness circuit and insulation resistance. In addition to checking the engine thermocouple system, the JETCAL® Analyzer can be used to test continuous-wire fire detection systems and thermal switches. By using a special air leak detector, maintenance personnel can locate air leaks at engine parting surfaces, bleed air ports, and anti-ice and air conditioning ducts. 1 JETCAL® is a registered trademark of Howell Instruments, Inc.

Cockpit Temperature Indicator Test Thermocouple … Series.pdfJETCAL®1 Engine Analyzer ... measuring system in aircraft turbine engines without running the engines, ... Probe Control

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Photo Courtesy of Department of Defense

BH112JD Series JETCAL®1 Engine AnalyzerThe BH112JD JETCAL® Engine Analyzer provides a superior combination of capabilities in a ruggedized, portable test set.

The BH112JD JETCAL® Engine Analyzer is designed to:

• Functionallycheckandtroubleshootthetemperaturemeasuringsysteminaircraftturbineengineswithoutrunning the engines, saving fuel and engine life.

• Accuratelymonitor,recordandprintcriticalengineparameters during engine trim.

Input Parameter FlexibilityBasicenginetestparameters-temperature,speedandpressure-canallbescaledtotheexactrequirementsoftheenginebeingtested.

• Temperaturecanbedisplayedin°Cor°F.

• Enginespeedcanbescaledin%RPM,directRPMorinfrequency(Hz).

• ExternallymeasuredpressurecanbedisplayedininHg,psi,ft-lbor%Torque.

• InternallymeasuredpressurecanbedisplayedininHgor psi.

• EngineSelectSwitchallowstheoperatortoselectthespecificcalibrationandscalefactorsappropriateforthe engine under test.

• Scalefactorscanbeeasilyenteredintomemoryforupto ten different engine types.

• Instructionalpromptsareprovidedonthetesterdisplaythroughoutthescalingprocedure.

• Scalinginformationisretainedpermanentlyinmemoryunlesschangedbytheoperator.

Howell Instruments, Inc.8945 South Freeway

Fort Worth, Texas 76140www.howellinst.com

817-336-7411Fax: 817-336-7874

[email protected]

PorTABLE EnginE TEST SETS & TrimmErSPorTABLE EnginE TEST SETS & TrimmErS

PROBE TEMP SET

6

7

80

2

5

TEMP SELECT

ON

PROBE POWERHEATER CABLEHEATER CABLE

INTERCONNECT INTERCONNECT

POWER INLETCABLE

SPREADADAPTERCABLE

JUNCTIONBOX

ASSEMBLY

HEATERCABLE

INTERCONNECTCABLE

POWER INPUTFUSE - 20

BUSS FUSE - 20

HEATERPROBE

SPREAD

ENGINE HARNESSSTAINNER INPUTS

HOWELL INSTRUMENTS, INC.

FORT WORTH, TEXAS U.S.A.

HEATER PROBE

A

Probe Control Module

B

CE

D

F

A Interconnect - Provides connection to Trimmer Section.

B Power Input - 115 or 230 VAC, 50 to 400 Hz, Single Phase Main Power Input

C Spread Cable - Connection for Spread Cable.

D Heater Cable - Connection for power and temperature signal to Junction Box or Heater Probe.

E Junction Box - Heater probe terminal connection.

F Heater Probe (model no. and quantity determined by engine application).

Probe Control module

Howell Instruments, Inc. • 8945 South Freeway • Fort Worth, Texas 76140www.howellinst.com • 817-336-7411 • Fax: 817-336-7874 • [email protected]

©2009HowellInstruments,Inc.PET112JD

Cockpit Temperature Indicator Test Thetesterprovidesasimulatedthermocoupleoutputtocheckthecalibrationofhighimpedance(nullbalance)orlowimpedance(currentdrawing)temperatureindicators.

Thermocouple Harness TestsTheaccuracyofcurrentdrawingenginetemperatureindicatorsisdependentupontheresistanceofthethermocoupleharness.TheBH112JDcanbeusedtoaccuratelymeasuretheresistanceofanyharnessto40ohms,aswellasinsulationresistanceto200,000ohms.

Probe Control

TheProbeControlSectioncontainsthepowersupplyandcontrolsrequiredfortheoperationoftheheaterprobes,includingtheconnectorandswitchrequiredtoperformspreadtests.

Totesttheenginethermocoupleharness,aheaterprobeisplacedovereachenginethermocouple.TheBH112JDJETCAL®Analyzercontrolsthepowerappliedtotheprobestomaintainthematapreselectedtesttemperature.Sincetheprobeispreciselyfittedtotheenginethermocouple,theprobeandthermocouplearemaintainedatthesametemperature.Athermocoupleembeddedintheprobeaccuratelymeasurestheprobetemperature.IftheaircraftthermocoupletemperaturedisplayedontheJETCAL®Analyzerorcockpitindicatorisoutsidetheacceptableprobetemperaturespecifiedinthemanual,a

malfunctionisindicated.TheJETCAL®Analyzercanthenbeusedasatroubleshootingdevicetocheckcockpittemperatureindicatorcalibration,thermocoupleharnesscircuitandinsulationresistance.

Inadditiontocheckingtheenginethermocouplesystem,theJETCAL®Analyzercanbeusedtotestcontinuous-wirefiredetectionsystemsandthermalswitches.Byusingaspecialairleakdetector,maintenancepersonnelcanlocateairleaksatenginepartingsurfaces,bleedairports,andanti-iceandairconditioningducts.

1JETCAL®isaregisteredtrademarkofHowellInstruments,Inc.

7

BUILT INTEST

2

5

HOWELL INSTRUMENTS, INC.

FORT WORTH, TEXAS U.S.A.

95.5

5.12

PCNT.

°C66

PSI

9

8

7

5

6

4

3

2

1PRESSURE

AIRCRAFT INSTRUMENT

INTERNAL

LEFT

1

1

22

3

3

4

4

5

5

66

ENGINE TYPE

77

88

99

1010

RIGHT

FUNCTION SELECT

NORMREADING

STD DAYREADING

TAMB SETOR PROBE

PAMBSET

EXTERNAL

INSULATIONT/C RESISTANCE

INDICATOR CHECK

TAMB

SET

RESISTANCE TEMP ZERO

RPM INPUTINSTRUCABLE

EXTERNALPRINTER

POWER INPUTINTERCONNECT

ON

OFFSTORE

N1

NORMAL

TEMP SELECT

RPM SELECT

PRESSURE SELECT

EXTERNAL(TORQUE)

SET TO PAMB

INTERNAL EP2

SET TO ZERO

HEATERPROBETEMPSET

MASTERPOWER

TEMP/RPM

Temperature/Standard Day CalculationTheengine’sthermocoupleharnessoutputmeasuresengine temperatures.

• Temperature:Displayedinunitsof°Cor°F • Maximumrange:0to1315°Cor0to2400°F

inonedegreeincrements • Calibration:Chromel®-Alumel®2(ISAtypeK)orthe

specialcalibrationrequiredbytheTF30engineWhenusedinconjunctionwiththeProbeControlSection,theTrimModulemeasuresheaterprobetemperaturesaswellastheindividualinputsfromtheenginespreadthermocouples.

AnRTDtemperatureprobeisavailableasanaccessorytoaccuratelymeasureanddisplayambienttemperature.

• AmbienttemperaturesignalssuppliedbytheRTDdisplayedin°Cor°F

• Range:–60to100°Cor–75to212°Fin0.1degreeincrements

Shouldtheenginetestproceduresrequireenginespeedandtemperaturereadingsatstandarddayconditions,theinputfromtheambienttemperatureprobeisusedtoautomaticallyprovidethestandarddaycorrectionfactor.Ifaprobeisnotavailable,thetestercancalculatecorrectedtemperatureandspeedreadingsusinganambienttemperature,whichisenteredmanuallybytheoperator.

Typical BH112JD Connection Scheme Trim module

1 Power Input/Interconnect - Power cable connects here for independent operation of Trimmer Section. Interconnect cable is connected for use with Probe Control Section.

2 Cable to connect tester to remote printer.

3 RPM/Frequency Cable - Connects in parallel to aircraft system at tachometer generator or cockpit RPM indicator.

4 Temp/RPM Signal Cable - Capable of one temp input and three RPM inputs. Design of this cable depends upon application.

5 General Purpose Temperature Cable - Allows operator to monitor engine temperature, check cockpit indicator, measure thermocouple harness loop and insulation resistance.

6 Temperature Adapter for specific application.

7 Ambient Temperature Probe Assembly.

8 External Pressure Transducer Assembly.

9 Pressure Hose for Internal Pressure Transducer.

Speed/Frequency Measurement

Thespeed/frequencymeasurementsystemisdesignedtodisplayenginespeedwhensuppliedwithinputsignalsfromstandardaircrafttachometergeneratorsorfrommonopolepickups.TheRPMSelectSwitchallowsanyoneofthreespeedinputstobeselected:

• %RPM • RPM • HzThespeed/frequencycircuitsaredesignedtoconditionthreedifferentfrequencyinputs(30,000Hzmaximum).Eachfrequencychannelcanbescaleddifferentlyandcanhave different engineering units.

Data Printout

TheBH112JDisdesignedtostoredataforprintoutbyaninternal(optional)orremoteprinter.Theengineserialnumber(orotherI.D.number),dateandtrimtargetcanbeenteredinmemorypriortotestingsothatprinteddatacanbeeasilyidentified.

TheBH112JDprovidesanRS-232orcurrentloop outputwithabaudratewhichisadjustablefrom 300to3600BITS/SEC.

Calibration

Thetestersoftwarehandlesallcalibrationautomatically,improvingsystemreliabilityandeliminatingpotentiometer-typecalibrationadjustments.

Pressure/EPR System

Thetestsetincludesapressuretransducercapableofmeasuringambientpressureorengineexhaustpressure(100inHgAmaximum).Therangeoftheinternalpressuretransduceris0to50psia(0to100.00inHg)inincrementsof0.05.

External(optional)pressuretransducerscanbesuppliedtomeasureparameterssuchasenginetorque,burnerpressureorambientpressure.

WhencalculatingEnginePressureRatio(EPR),theengineexhaustpressureismeasuredontheinternaltransducer.Theambientpressureiseithermeasuredonanexternaltransducerormanuallyenteredwhenanexternalmeasurementisnotavailable.

Environmental

TheBH112JDisaruggedizedunitcapableofoperatinginsevereenvironmentalconditions(–40to+70°Cambienttemperature)encounteredontheflightline.

Built-In Test

TheTrimModulecontainsacomprehensivebuilt-in-test feature.Whenthetesterdetectsafault,thedisplayindicateswhichcircuithasfailed.

BH112JD SeriesJETCAL® Engine Analyzer

2Chromel®andAlumel®areregisteredtrademarksofHoskinsManufacturing,Co.

PorTABLE EnginE TEST SETS & TrimmErSPorTABLE EnginE TEST SETS & TrimmErS