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PEAPOD Manufacturing Status Review Pneumatically Energized Auto-throttled Pump for a Developmental Upperstage Customer: Special Aerospace Services Chris Webber and Tim Bulk 1

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Page 1: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

PEAPODManufacturing Status Review

Pneumatically Energized Auto-throttled Pump for a Developmental Upperstage

Customer: Special Aerospace ServicesChris Webber and Tim Bulk

1

Page 2: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• ProjectOverview• PumpManufacturing• PumpControl• Valving• Electronics• Software

• Budget• Conclusion

Overview

BudgetPumpControl

Testing/ScheduleOverview Pump

Manufacturing 2

Page 3: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

•Designandmanufactureapneumaticallypoweredpumpsystemforuseonanupperstagerocketengineorlander.• Proofofconceptpumpsystemforhypergolicpropellants• 10%-100% throttleability• Pneumaticallypowered

Project Motivation

BudgetPumpControl

Testing/ScheduleOverview Pump

Manufacturing 3

Page 4: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Levels of SuccessLevel Functional Success Performance Success Functional Requirement

1 • Pneumatic power• Digital control• Meets safety

requirements

• 750 ± 15 psi outlet pressure• Structural FOS 2.5• 120 seconds of operation• 75% efficiency of pump at full

throttle

• FR1 – System is pneumatically driven

• FR7 - FOS of 2.5• FR8 – 75% efficiency at

full throttle• FR3 – Pump outlet is at

750 ± 15 PSI2 • Propellant stream

throttling• All level 1 requirements

• 10-100% throttleability• 0-100% throttle in 2 seconds• All level 1 requirements

• FR2 – Pump system is throttleable

• FR4 – Pump system can run through throttle profile

• FR5 – Pump is restartable3 • Hypergolic compatible

• All level 1 and 2 requirements

• 0-100% throttle in 1 second• All level 1 and 2 requirements

• FR6 – System is built to hypergolic standards

BudgetPumpControl

Testing/ScheduleOverview Pump

Manufacturing 4

Page 5: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Subsystems1. Pump2. Drive System3. Control 4. Test

Functional Block Diagram

5

Page 6: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

CONOPS

6BudgetPump

ControlTesting/ScheduleOverview Pump

Manufacturing

Page 7: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Current Schedule

7

Page 8: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Current Schedule

8

Page 9: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• Whatisincluded:• Housing• Gears• Driveshaft• Bearings• Seals• Assembly• HeliumRegulatorHolster

Manufacturing - Overview

9BudgetPump

ControlTesting/ScheduleOverview Pump

Manufacturing

Page 10: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• Gearpumpismadeupof:• Gears– TobeManufactured• Housing– TobeManufactured• Close-outpanel– TobeManufactured• Driveshaft– Tobefinalized,willbekeyedandaltered• AlignmentShaft– Tobefinalized,willbekeyedandaltered• Seals– Purchased;Geometryisbeingtriplechecked• Mainbearings– Purchased;Thrustandrollerbearingstobepurchased• Coupler– TobePurchased• Collar– TobePurchased

Pump Manufacturing

10BudgetPump

ControlTesting/ScheduleOverview Pump

Manufacturing

Page 11: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

•WireEDMprofilewithgroundfaces• Finalizingstockrequirements(17-4PHStainless)• CFDresultsmaydictateminorchanges• Nopostmachiningwithdecidedmanufacturer• Delivery4weeksARO

Gears

11BudgetPump

ControlTesting/ScheduleOverview Pump

Manufacturing

Page 12: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• CNChereatCU,usearoughcutfirsttominimizetimeonCNC• Benefit– workingfromourmodel• Basedoffof continuedCFDresults,asecondhousingwithloosertolerancesmaybemade– perhapshereoratSAS• Thisgivesusabackup• MustcontinuetomoveforwardandcompleteCFDconcurrently

• Timeframe:4weeks• Concerns:Depthofextrudedcut,maintainingtheprofile,materials,specialtoolstomanufacture

Pump Housing

12BudgetPump

ControlTesting/ScheduleOverview Pump

Manufacturing

Page 13: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Housing

13BudgetPump

ControlTesting/ScheduleOverview Pump

Manufacturing

Page 14: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• CNChereatCU• Basedoffof continuedCFDresults,asecondhousingwithloosertolerancesmaybemade– perhapshereoratSAS• Thisgivesusabackup,singularplatemayworkforbothhousingsTBD

• Timeframe:4weeksleadtime• Drawingtobefinalized:stillawaitingreliefgrooves,sealgroovegeometrymaychangeforoptimalperformance• Concerns:material,specialtoolstomanufacture,rotaryshaftsealandgeometry

Close-Out Plate

14BudgetPump

ControlTesting/ScheduleOverview Pump

Manufacturing

Page 15: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Close-Out Plate

15BudgetPump

ControlTesting/ScheduleOverview Pump

Manufacturing

Page 16: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• Seals• 1largeO-ringforfaceplateandhousing• 1O-ringshaftseal• Groovegeometryisbeingtriplechecked;Mayutilizeadoubleseal• Readyforpick-upinDenver

• Bearings• Bearingmanufacturerthatcommonlysuppliesbearingsforgearpumpsissending'samples'forfree(shipped,awaitingarrival)• Thisisputtingconstraintsonourshafts– metricoptionsmaysolvethis• Thrustbearingsareoutsideofworkingfluidandworkwithacollartoretainthedriveshaft• Rollerbearingsareincludedtoavoidwearontheinsideofthehousingandnecessitatepost-machiningoftheshafts

Pump Manufacturing

16BudgetPump

ControlTesting/ScheduleOverview Pump

Manufacturing

Page 17: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• Driveshaftandplacement• Post-machinehere• Wecankeyintheshophere,allowsforpropercontactandsizingtomaintainintegrityofhousing• Metricoptionsarebeingexploredtoobtainproperundersizing fortheperformancing sleevebearings• Timeframe:20hours

Pump Manufacturing

17BudgetPump

ControlTesting/ScheduleOverview Pump

Manufacturing

Page 18: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• SealgroovegeometrywillbefinalizedbyTuesdayCOB•MeetingwithMattRhodeTuesdaytonaildownlogistics–propermaterialandspecialtools• OrderandgetmaterialsandtoolsbyFeb.13th• StartmachiningASAPFeb13thor14th

Overall Timeframe

18BudgetPump

ControlTesting/ScheduleOverview Pump

Manufacturing

Page 19: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

GapDetected

BearingSpacer

ShaftBearingGearSetupShim GearSpacingShim

DriveShaft

Gear

Pump Assembly

19

Page 20: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

SpacingVerified

BearingSpacer

ShaftBearingGearSetupShim GearSpacingShim

DriveShaft

Gear

GearSpacingShim(+.0005)

Pump Assembly

20

Page 21: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

BearingSpacer

ShaftBearingGearSetupShim GearSpacingShim

DriveShaft

Gear

GearSpacingShim(+.0005)

Pump Assembly

21

Page 22: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

SpacingVerified

BearingSpacer

ShaftBearingGearSpacingShim

DriveShaft

Gear

GearSpacingShim(+.0005)

DriveShaftKey

Pump Assembly

Timeframe:1weekforassembly 22

Page 23: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Pump Assembly

23

Bearing

Seal

Shaft

Collar

ThrustBearing

CloseoutPlate

Timeframe:1weekforassembly

Page 24: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• ConstructinganElectronicHeliumRegulator• Tocontrolthedrivesystem

• Manufactureaholstertohousethesteppermotor• Timeframe:80hours

Electronic He Regulator

24BudgetTesting/

ScheduleOverview PumpManufacturing

Pump Control

Page 25: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• Solenoidregulatorwastooexpensive• Manufacturingfromaluminum• Housessteppermotor• Need8Nmoftorquetoturnthepressureregulatoratitslowestsettings• Similarsetupforbackpressureregulator

Electronic He Regulator

25BudgetTesting/

ScheduleOverview PumpManufacturing

Pump Control

Page 26: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Electronics FBD

Allelectronicdesignfallsinhere

26

Page 27: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• SignalConditioning• Designwillbetestedinabreadboard• PCBboardwillbedesignedbasedonthebreadboard• PCBboardwillbepopulated

• Testing• Componenttestingwillbedoneonthebreadboard• Integrationwillbedone withthePCBboard

Electronics

BudgetTesting/ScheduleOverview Pump

ManufacturingPump

Control 27

Page 28: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• Electronics• Sensors• DAQs

• NI9211(temperaturereadings)• NI 9205(pressurereadings, similartoNI6002butmorepowerful)

• willuseNI6002 forfinaltests

• 100hoursleftforalltestingandintegration

Electronics Integration

BudgetTesting/ScheduleOverview Pump

ManufacturingPump

Control 28

Page 29: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• Software• LabVIEW• Developmentorder:

• Filesystem- complete• Componenttests/DAQ system– inprogress(~10hours, <1week)• Controlsystems– model,simulate,implement– inprogress(~45 hours, 4weeks)• Fullsystemtests - TBD(~60hours, 5weeks)

• DAQSoftwareDrivers• Already have

• Posttestanalysis- MATLAB(file readfunctions complete)

Software

BudgetTesting/ScheduleOverview Pump

ManufacturingPump

Control 29

Page 30: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Software

BudgetTesting/ScheduleOverview Pump

ManufacturingPump

Control

• Controlcodeoverview:• Safetyimplicitto error

check• Throttle manual

or automatic• Backpressurefaster

than power - preventoscillation

30

Page 31: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Software

BudgetTesting/ScheduleOverview Pump

ManufacturingPump

Control

• Pressurevalvecontrol:• Somedatakeptin

memory– checkvalveposition

31

Page 32: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Software

BudgetTesting/ScheduleOverview Pump

ManufacturingPump

Control

• Backpressurecontrol:• Fastestcontrol

component

32

Page 33: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• Software– thermocoupletestblockdiagram

Software

BudgetTesting/ScheduleOverview Pump

ManufacturingPump

Control 33

Page 34: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• Software– thermocoupletest userinterface

Software

BudgetTesting/ScheduleOverview Pump

ManufacturingPump

Control 34

Page 35: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• Combinedpressureandtemperatureuserinterface

• 115hoursremain

Software

BudgetTesting/ScheduleOverview Pump

ManufacturingPump

Control 35

Page 36: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Piping Assembly

BudgetTesting/ScheduleOverview Pump

ManufacturingPumpControl

Water Pipe Size: ¾"NPTPressure Ranges: 50-800PSIMax Flow Rate: 22Gal/min

Air Pipe Size: 1"NPTPressure Ranges: 0-2200 PSI

Max Flow Rate: 45CFM

Nomenclature

SV = Solenoid ValveRV = Relief ValveMBV = Manual Ball ValveMR = Manual RegulatorEP = Electronic Pressure RegulatorBPR = Back Pressure RegulatorTM = TachometerBD = Burst DiskLB = LubricatorF = Air FilterP = Pressure TransducerT = Temperature SensorADPT = GHT to NPTFP = Flexible PipeQD = Quick Disconnect

Low Pressure ~ 50PSI High Pressure ~ 750PSI

High Pressure ~ up to 2200 PSI Regulated Pressure ~ 0-125PSIMedium Pressure ~ up to 125PSI

36

Page 37: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Testing Timeline

BudgetOverview PumpManufacturing

Component Testing – QC and CalibrationComponent Testing to be Conducted Man Hours Status

Pressure Transducer (Air P1, Water P1)

Calibration through ranges of known shop air pressures

6 Hours : 1.5*(2*1 + 2*1 + 2*1) 50%

Air Pressure Regulator (EPR) Operation through 0-110PSI to calibrate outlet pressure/thread engagement

10.5 Hours : 3*1 + 3*1.5 + 3*1 0%

Water Back Pressure Regulator (BPR)

Operation through 0-750PSI to calibrate inletpressure/thread engagement

10.5 Hours : 3*1 + 3*1.5 + 3*1 0%

Thermocouples (T1, T2) Calibration at known temperatures (Ice bath, boiling…)

4 Hours : 2*0.5 + 2*1 + 2*0.5 100%

Manual Ball Valve (Water MBV1) Verify correct operation (on/off) and no leaking 25 Minutes : 1*0.2 + 1*0.1 + 1*0.2 0%Solenoid Valve (Water SV1, Air SV2) Correct opening and closing upon energization

and de-energization1.5 Hours : 2*0.5 + 2*0.25 + 2*0.5 0%

Tachometer Calibration at known RPMs 6 Hours : 2*1 + 2*1 + 2*1 0%Manual Air Regulator (MR1) Calibration to ranges 100-125 with known shop

air pressures7 Hours : 2*1.5 + 2*1 + 2*1 0%

Full Air Assembly Torque Verification @ RPM, conducted with friction test, fan test

13.5 Hours : 3*2 + 3*1.5 + 3*1 0%

TimingPersonnel: Operators required

Hours: Timerequired to prepare and assemble test

Hours: Timerequired to conduct test

Hours: Timerequired to disassemble test and save results

Multiplier: Repeat test for identical sensor /component

*Subsystem Testing included in backups Total Man Hours: 113.4Testing/Schedule

PumpControl 37

Page 38: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Scope

Electrical

CreateSignalConditioningonBreadboard

DevelopaPCBBoard

PopulatethePCBBoard

Software Manufacturing

Componenttest

Systemtest

Gears

Driveshaft

Housing

Valving/Piping

Integration

Bearings/Seals

Controlsystems

38

Page 39: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Budget

BudgetTesting/ScheduleOverview Pump

ManufacturingPump

Control 39

Page 40: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Budget

BudgetTesting/ScheduleOverview Pump

ManufacturingPump

Control 40

Page 41: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Schedule

41

Page 42: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

• Weareslightlybehindschedule(3days– 1week)• Encounteredproblemswithpumpmanufacturing• Airmotortesting• Unabletofindcheaperpartsresultedinmanufacturingthem

• Increaseinteamhourstoaccomplishsensorandintegrationtasks• MovingForward:• Increaseinsub-componenttestingfromallteammembers• Timeframe:~100hoursforElectronics

~200hoursforSoftware~100hoursforManufacturing/Assembly~150hoursforTesting

Conclusions

42

Page 43: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Questions?

43

Page 44: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Backup

44

Page 45: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Pump Housing

• Worries about shafts wearing into the housing necessitated this solution• Possible to post machine

down the ends to press fit into bearings and key in the proper locations for the gears and coupler

Page 46: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Pump Housing

• To prevent pressure pushing the driveshaft out, an extra retention method was included to prevent axial pushback since the shaft is essentially wedged between the mounted pump and mounted motor on the stand

Page 47: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Pump Seals

• The geometry is being updated to optimal specs. Will be finalized/double checked by COB Tuesday• May included a double seal to mitigate possible leaking as

we enter testing

Page 48: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Prelim Housing Drawing with GD&T

Page 49: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Prelim Close-out Panel Drawing with GD&T

Page 50: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Pump Control - Software

50BudgetTesting/

ScheduleOverview PumpManufacturing

Pump Control

• Pressureandtemperature

combinedtestsetup

Page 51: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Pump Control - Software

51BudgetTesting/

ScheduleOverview PumpManufacturing

Pump Control

• Pressureandtemperaturecombinedtestmainloop

Page 52: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Phase 1 – Sensor Testing and Simulation

• Designingmotor-regulatormechanicalinterface• Designingpressureregulationthroughcontrolofmotorvoltage

Electronicpressureregulatordesign

• CircuitDesign:Powerrequirements,readingoutputs

• Calibration:samplingrate,noisecompensation,errorrejection

SensorTesting

• ModelDriveandPumpsystem• Designcontrollawforthrottlingpumpflowrate• Designrealisticthrottleprofiles

SimulinkModeling

• Systemcircuitdesign• ImplementationofsafetymonitoringsoftwareLabView Design

KeyResultstoobtained

• Completionofpressureregulatingsystem,obtainingresultingaccuracy,slewrate,powerrequirements

• PressureTransducerperformance• Tachometermountingandperformance• Firstiterationofelectronicscircuitdesign• Firstiterationofsystemcontrollaw• Estimateofsystemslewrate(startupandshutdown)• Generationofvariousthrottleprofiles• FirstiterationofDAQdesignforbothdataacquisition

andsystemcontrol• Firstiterationofsystemuserinterface• Designofsystemmonitoringsoftware• Confirmingtestinglocation

Phase 2 Functional Reqs. met – None

Page 53: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Phase 2 – Subsystem Testing

• Motor:RPM/TorqueTest• Motor:HeliumRunTest• ManualRegulator:PressureFluctuations• ElectronicRegulator:Calibrationtohitmaximum

accuracy.• Tachometer:Calibrationtohitmaximumaccuracy• Power-Offtesting:Verifyingthatsolenoidvalve

correctlyclosesincaseofpowerloss.• ThrottlingTest1:Throttlingfrom10-100%usingthe

electronicpressureregulator,confirmingcontrolwithpressuretransducer.

• ThrottlingTest2:Fullyassemblingdrivesystemcomponents.Runningthroughthrottleprofiles.

DriveSystemTesting PumpSystemTesting

KeyResultstobeobtained

• ManualRegulator:PressureFluctuations• Power-Offtesting:Verifyingthatsolenoidvalve

correctlyclosesincaseofpowerloss.• ElectronicBackPressureRegulator:Calibrationtohit

maximumaccuracy

• Numerousiterationsofthrottlingcontrolsoftware,monitoringsoftwareandelectronicregulatorsoftware

• Assessmentofunforeseenissues,correctionofaffectedcomponents

• Validationofcomponentcapabilities,allowingforfullsystemassemblytooccur

Phase 2 Functional Reqs. met – FR6, FR7

Page 54: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Piping Assembly

54BudgetTesting/

ScheduleOverview PumpManufacturing

Pump Control

Water Pipe Size: ¾"NPTPressure Ranges: 50-800PSIMax Flow Rate: 22Gal/min

Air Pipe Size: 1"NPTPressure Ranges: 0-2200 PSI

Max Flow Rate: 45CFM

Nomenclature

SV = Solenoid ValveRV = Relief ValveMBV = Manual Ball ValveMR = Manual RegulatorEP = Electronic Pressure RegulatorBPR = Back Pressure RegulatorTM = TachometerBD = Burst DiskLB = LubricatorF = Air FilterP = Pressure TransducerT = Temperature SensorADPT = GHT to NPTFP = Flexible PipeQD = Quick Disconnect

Low Pressure ~ 50PSI High Pressure ~ 750PSI

High Pressure ~ up to 2200 PSI Regulated Pressure ~ 0-125PSIMedium Pressure ~ up to 125PSI

Page 55: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Subsystem Testing Timeline

55BudgetTesting/

ScheduleOverview PumpManufacturing

Pump Control

Water Testing – Subsystem TestingComponent(s) Testing to be Conducted Man Hours Status

Solenoid Valve Shut-Off Simulate excessive pressure and/or temperaturereadings to initiate safety shutdown

9 Hours : (2*4 + 2*0.5 + 2*0.5) 0%

Adapter, Quick Disconnect, Flexible Pipe, Pressure Ducer

Quantify pressure losses (water) associated with pre-piping assembly

7.5 Hours : 2*1 + 2*1.5 + 2*1 0%

Pre-Pump pressure loss Quantify pressure loss (water) of full assembly leading to pump inlet

10.5 Hours : 3*2 + 3*0.5 + 3*1 0%

TimingPersonnel: Operators required

Hours: Timerequired to prepare and assemble test

Hours: Timerequired to conduct test

Hours: Timerequired to disassemble test and save results

Multiplier: Repeat test for identical sensor /component

Total Man Hours: 27

Page 56: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Subsystem Testing Timeline

56BudgetTesting/

ScheduleOverview PumpManufacturing

Pump Control

Air Testing – Subsystem TestingComponent(s) Testing to be Conducted Man Hours Status

Solenoid Valve Shut-Off Simulate excessive pressure and/or temperaturereadings to initiate safety shutdown

4 Hours : (2*1 + 2*0.5 + 2*0.5) 0%

Pressurized Gas, Manual Regulator,Solenoid Valve (Air), Relief Valve, Filter, Pressure Transducer

Quantify pressure losses (air) associated with pre-regulator assembly

10.5 Hours : 3*1.5 + 3*1+ 3*1 0%

Full air system excluding Air Motor Detection of pressure regulator miss-calibration/erroneous operation

13.5 Hours : 3*2 + 3*1 + 3*1.5 0%

TimingPersonnel: Operators required

Hours: Timerequired to prepare and assemble test

Hours: Timerequired to conduct test

Hours: Timerequired to disassemble test and save results

Multiplier: Repeat test for identical sensor /component

Total Man Hours: 28

Page 57: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Subsystem Testing Timeline

57BudgetTesting/

ScheduleOverview PumpManufacturing

Pump Control

Air Testing – Subsystem TestingComponent(s) Testing to be Conducted Man Hours Status

Solenoid Valve Shut-Off Simulate excessive pressure and/or temperaturereadings to initiate safety shutdown

9 Hours : (2*4 + 2*0.5 + 2*0.5) 0%

Pressurized Gas, Manual Regulator,Solenoid Valve (Air), Relief Valve, Filter, Pressure Transducer

Quantify pressure losses (air) associated with pre-regulator assembly

7.5 Hours : 2*1 + 2*1.5 + 2*1 0%

Full air system excluding Air Motor Detection of pressure regulator miss-calibration/erroneous operation

10.5 Hours : 3*2 + 3*0.5 + 3*1 0%

Full Air Assembly, air motor connected to friction assembly

TimingPersonnel: Operators required

Hours: Timerequired to prepare and assemble test

Hours: Timerequired to conduct test

Hours: Timerequired to disassemble test and save results

Multiplier: Repeat test for identical sensor /componentTotal Man Hours: 27

Page 58: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Phase 3 – Full System Testing

• DriveShaftAlignment• Massflowratetesting• Throttleprofiletesting• Systemstartupandshutdowntesting• Emergencyshutdowntesting• Restartability testing

Fullscaletestingtobeconducted KeyResultstobeobtained

• Determinationofanymisalignmentofmotor/pumpdriveshaft

• Pumpperformance:massflowrate,backpressure,efficiency

• Observationofsystemundernumerousthrottleprofiles

• Iterationonshutdownprocedurestooptimizerestartability

• Iterationoncontrollawtoaccountforunaccountedsystemproperties

Page 59: PEAPOD - Home | University of Colorado Boulder...•Design and manufacture a pneumatically powered pump system for use on an upper stage rocket engine or lander. •Proof of concept

Final Testing

• Throttle profile testing: (10 - 100% Throttle), slew rate testing.

• Quantifying magnitude of outlet pressure fluctuations

• Throttle profile testing (ran through various profiles)

• System startup and shutdown testing, with emergency shutdown and restart-ability

Full scale testing to be conducted Key Results to be obtained• Pump performance: mass flow rate, back

pressure, efficiency • Observation of system under numerous throttle

profiles• Iteration on shutdown procedures to optimize

re-startability• Iteration on control law to account for

unaccounted system properties

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• Pump-Drive system• Control Volume• Flow Bypass system• 3 Team membersmonitoring test

Standard Testing Procedure - Example

1. Pump is started up and commanded to throttle setting

2. The pump is run at throttle setting3. Flow enters control volume for 10 secs4. Flow is diverted back to regular vent5. Pump is shutdown6. Control volume is measured and recorded 7. Test is re-iterated as needed for other throttle

settings

Throttle Calibration Test Critical Test Elements

Key Results to be obtained• Validation of throttle model design• Refinement of throttle model design• Meeting of critical project element

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Safety Set-UpWorst Case Failures1. Drive system flywheel – 225 J 2. Drive system casing – 16 J 3. Pump gears – 36 J

Cinder Block Housing Strength• Chipping - 300 J • Cracking - 600 J • Penetration - 800 J• Failure - 1000 J • Complete destruction - >1300 J

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Analog to Digital Conversions

• Converting from ADC to pressure• Find the MSMT out of the

ADC to get the Voltage into the ADC• Find the pressure out of the

Pressure transducer• Find pressure by dividing it

by the voltage per pressure ratio

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Automatic Pressure Regulator

• Electronic pressure regulators with high volume flow are not found, but manual do exists• Combining a manual pressure regulator with an encoder and

stepper motor• Motor shall have a minimum angular velocity of 300 RPM• No error, and time of settle of less than 1 second

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Automatic Pressure Regulator FBD

• Controlling a stepper motor based on the position• This position will allow the

output pressure

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Automatic Pressure Regulator Diagram• Control points of view for the pressure regulator• Can be simplified by combining both plants • Needs to be tested to find the correlation of angular

position with output RPM

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Automatic Pressure Regulator• This can be simplified by combining • the drive system transfer function and • the motor transfer function

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Automatic Pressure Regulator

• Simplified version of the model• Allows to control the drive system based on the voltage

input

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Signal Processing – Differential Amplifier• Use for creating an offset

and applying a gain to the voltage out of the pressure transducer• This will allow us to look at

a range from 600 – 800 psi a with higher accuracy.

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Signal Processing – Voltage divider

• Being able to from 28 V to .6 V• The output will be used to

provide the offset needed for V1

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Signal Processing – Noise Mitigation

• Easy to make• First order filter• Only one pole

• Harder to make• Second order filter• Two poles

Low pass filter Sallen-key filterVs

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Signal Processing – Noise Mitigation

• Prevents to look at high frequencies that are irrelevant• This will have a cutoff

frequency at 2 kHz

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Signal Processing – Electronic diagram

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Electronic Test