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NASA Technical Reports Server (NTRS) 20070010453: Summary of Stirling Convertor Testing at GRC PDF

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Preview NASA Technical Reports Server (NTRS) 20070010453: Summary of Stirling Convertor Testing at GRC

Summary of Stirling Convertor Testing at GRC Jeffrey G. ~chreiber* NASA Glenn Research Center at Lewis Field, Cleveland,O hio,4 41 35 The NASA Glenn Research Center (GRC) has been testing free-piston Stirling convertors for potential use in radioisotope power systems. These convertors tend to be in the 35 to 80 watt electric power output range. Tests at GRC have accumulated over 80,000 hours of operation. Test articles have been received from Infinia Corporation of Kennewick, WA and from Sunpower of Athens, OH. Infinia designed and built the developmental Stirling Technology Demonstration Convertors (TDC) in addition to the more advanced Test Bed and Engineering Unit convertors. GRC has eight of the TDC's under test including two that operate in a thermal vacuum environment. Sunpower designed and developed the EE- 35 and the Advanced Stirling Convertor (ASC). GRC has six of the EE-35's and is preparing for testing multiple ASC's. Free-piston Stirling convertors for radioisotope power systems make use of non-contacting operation that eliminates wear and is suited for long- term operation. Space missions with radioisotope power systems are often considered that extend from three to 14 years. One of the key capabilities of the GRC test facility is the ability to support continuous, unattended operation. Hardware, software, and procedures for preparing the test articles were developed to support these tests. These included the processing of the convertors for minimizing the contaminants in the working fluid, developing a helium charging system for filling and for gas sample analysis, and the development of new control software and a high-speed protection circuit to insure safe, round-the-clock operation. Performance data of Stirling convertors over time is required to demonstrate that a radioisotope power system is capable of providing reliable power for multi-year missions. This paper will discuss the status of Stirling convertor testing at GRC. v o g . a s a n C w. w w R G e t c a n e g r e n nf o i t C s g e n i T r e r e e r n nt o gi e n C nvert d at the ersion E go, CA y hreiber esearch nd, OH o e v e b c R a C ent on Di S n vel s C n ff n e g re y Sa Je le Cl p g G n er A n i S l E r A i al N t n S o i n at o f ati o n r r minist y nte I d r A 6 e a 0 ac m 0 p 2 S d n m a s utic u na S o r e A al n o ati N 1 v o g . a s a n f w.n s, o o w g ti s w n a w ) E h di nt e O ug n e vi D i s o f e e ( r , r h y h s p t rg d t on s ct e n ni hi e En m a pi n t efl n. of a y o d i y r io nt ogr An se aril rat e s t m pr g. e ss is r n rt ) n p e i a 0 i x c m p 1 d e e e 1 n n d G u s A D F n ot e R o n e h th r (S rate dati do pac g o o n d S u at ct e n d o r e m a n e thr en Dir om er s a d G n c nt c i e o e e t e u l i r s ministration s enab isotop e Miss ons or he pre Aerona d o e A wa di nc si f t l nd Spac ork Ra Scie nclu se o iona eronautics a This w Stirling NASA and co are tho he Nat A t al n o ati N 2 v o g . a s a n . w w w s C a w R n o h G 8 9 n ati c t 9 io er ar a 1 at p e d o s g gh ali e e n v h r ti ou e g t c s r d n ti e h o i a c d m T 5 t or an e r 7 f st n r o 9 ta er ki e t 1 a s d w r d t n y onve g from , cycle project rtor tes mics, u gine e earl ace po Administration ng Engine and C l perspective, testin maticengine tests search, heat exchangers GPU-3 Advenco tomotive Stirling engine P-40 Mod I, Mod IA piston engine & conve search, cycle data, dyna Type 10 RE-1000 HP-1000 Hydraulic output engine Space Power Research En he motivations for th nto the future for sp ace rli ca e Re – – Au – – e- Re – – – – – t g i Sp ti ri n e of n and S to Ki • • Fr • e ki s s n o c i – – uti H O o a l n o r e A • • al n o ati N 3 v o g . a s a h n . s w w i s l w b ’ 0 a M 9 t 9 s E 1 e d C e h o n R 99 h th arc ns t on C a g e i P G 9 a s 1 u s e r T t e hro re m ve C a c s n , n rs E t ou a o 10 g si o O i s c - n e ert D ev a er RG sti ativ onv with n pr y ated ow nia Te niti er c on tha abilit niti g p Infi or pe i pow rati wer g reli as i irlin ne, ert oto ng abo e, lo ancin g w e St engi Space Administration Stirling Conv ties under the radiois l about free-piston Stirli ame from a general coll ower level was ~100 W Transition to flight –High TRL –Manufacturability –System integration –Rise reduction and enh Advanced technology –Reduced mass –Reduced physical size –Increased efficiency –More robust design nded operation testinnd reliability data points of long lif arwell TMG, NIH heart nd vi Al C P • • ea w H s a cti xte e c – – – – uti A Eif F a l n o r e A • • • al n o ati N 4 v o g . a s a n ) , e, w. C s w s r w T e n l o n S l o e p o r v s i y t t n i e a t C rl o c r r e c A t e n p R m , , e o n n G r o o si y o i i n b t t f a a a at a( iz iz tr ed i er er s, w g n t t t o c c s n fi a a e ll n o i r r t st I ha s ha er , f m t e c t c l s tor T #6 fro ober 00 mance tion tes d #8 ch 01 mance control vibe te er d ct or ra n ar or on n, b nv an n O erf vi 7 a n M erf ecti atio p , p o 5 d i r se # d i r rr er o C # e o n s e o p C t f o ’ t f o n g DC tar sts sp DC tar sts or sts or Administratio tirlin se T ation s sed te ent re se T ation s sed te r Fact ion te plans f e S a r u si a r u e at ac h e c n h e c w r d Sp p o a p o o b a nd rc O F tr rc O F P vi H a s u u c – – – – – uti P P a n o r e A • • al n o ati N 5 RC ower Output, Measured and Empirical Correction Measured Corrected Linear (Corrected) y = -0.0005x + 66.681 5001000150020002500 Time (hrs) Impurity Concentrations in TDC #1350 45N240eHBlackout 35ni mArp30p ,rA f25o noita20rtnec15noC 10HO25 01000.01500.02000.02500.0 Run Time, Hours www.nasa.gov P G TDC #13 0 CO2 500.0 0 0 0 0 0 0 0 69. 68. 67. 66. 65. 64. 63. )caW( tuptuO rewoP t a 400 350 300 250 200 150 100 50 00.0 eH ni mpp ,2N dna 02H ,2OC fo noitartnecnoC g c n pv et n, d i T n, n t o 4 o d a nautics and Space Administration Stirling Convertor Tes ended Operation of TDC’s#13 and #1 TDC’s#13 and #14 were sent to GRC for Extended Operation Test •Develop data base of operating hours •Look for indications of change in operation •Test capability was developed for –24/7 operation, with control of Thot, Tcold, and –Measurements of temperatures, power, vibrati –Analysis of working fluid composition First operated in April 03 Following 40 hours of check out, extended operation began in June 03 By October 03, after 2,300 hours of operatiperformance was decreasing very slowly •At a rate of ~0.5 W per 1000 hours •It was also noticed that the working fluid haincreasing levels of argon and nitrogen •Argon came from an insulation loss test •Speculated that increasing level of nitrogen performance change were linked o r t e x A – – – – al E n o ati N • 6 eH ni mpp ,rA fo noitartnecnoC GRC C #13 Power Output, Measured and Empirical Correction MeasuredCorrectedLinear (Corrected)Linear (Corrected) y = -0.0005x + 66.616 y = 6E-05x + 65.046 500100015002000250030003500 Time (hrs) Impurity Concentrations in TDC #13 140N2 120 100 80 60 40 Flow Argon20OCOHon 22o-rings01000.01500.02000.02500.03000.03500.0 Run Time, Hours www.nasa.gov TD9.0 8.0 7.0 6.0 5.0 4.0 3.00 Ar 500.0 6 6 6 6 6 6 6 )caW( tuptuO rewoP t a 550 500 450 400 350 300 250 200 150 100 50 00.0 eH ni mpp ,2N dna 02H ,2OC fo noitartnecnoC g stin ed ngs d on tinued hours hours uum or y slowly cs and Space Administration Stirling Convertor Te rmeation tests with convertors evacuat re inconclusive With the convertor still or being motored Up to full operating temperatures at the o-ri –Noted that argon and nitrogen levels remaineconstant during permeation tests Returned to operation in November 03, arg appeared to level off, but nitrogen level con to rise Installed purge rings in November at 2,800 Initiated purge with argon because: –The test was originally intended to last 5,000 –Leakage of purge rings was unknown for vacother gasses Results of argon cover gas on o-rings was immediate –Nitrogen concentration remained constant –Argon concentration began to rise at a greatlincreased rate –Performance appeared to be degrading more auti Pe we • • • • • • n o r e A – al n o ati N 7 v o g . a s a n . n w n agai e to 9000.0 yzed ror ww i v l a m e o 8000.0 n na e u c m i a w g at GRC changed to heli ed off, argon on at 9,045 hours Impurity Concentrations in TDC #13 Ar 3000.04000.05000.06000.07000.0 Run Time, Hours ic seal welding omposition to be ed no signs of n l et c w ti was eve 04, N2 2000.0 rm uid ho es s e l st CO2 OH2 1000.0 he g fl s s a c u n t or T urge g orman ht Aug 1300 e1200H ni1100 mpp1000 ,2N 900dna r800A ,02700H ,2O600C fo500 noit400artne300cno200C 100 00.0 own for w worki mponen ert e p perf oug utdrs allo co autics and Space Administration Stirling Conv As the test was extended, thMarch 04 after 5,873 hours Nitrogen concentration and rose very slowly Operated in this condition thnew facility TDC #13 Power Output, Measured and Empirical Correction 69.0 Measured68.0Corrected)caW67.0( tup66.0tuO r65.0ewoP64.0y = -0.0005x + 66.605 y = -0.0002x + 65.62y = 8E-05x + 64.2563.002,0004,0006,0008,00010,000 Time (hrs) Operation continued until shJanuary 06 after 19,108 hou –Fill tube was not welded to Visual inspection of internal degradation n o r e A • • • • • al n o ati N 8 v o g . a s a 13 14 0 n C # C # 00 w. h h on TD TD 25, ww ac wit siti 00 e o 0,0 n n p 2 o o m i at GRC one failed nitial operat ngor deco C #13 & #14 Efficiency 10,00015,000 Time, (hrs) g urs rs, o i ssi TD 000 n ho ate e t ga 5, esti 040 e he n du o out 40 35 30 25 20 15 10 5 0 0 , g a t )%( ,ycneiciffE T 2 d h e r at 2 rtri er t du o a h g ert ently ace c on ot ngin #13 Corrected #14 Corrected 25,000 v rr l i a on e cu rep adat d ch 20,000 o C r r i and Space Administration Stirling C’s#13 and #14 a sently shut down tC pears to be no deggen permeation sign of working fluhe organics TDC #13 & #14 Power Output 5,00010,00015,000 Time, (hrs) utics TD PreTD Apoxy No of t 0 0 0 0 0 0 0 0 0 0 a 8 7 6 5 4 3 2 1 n o )caW( ,tuptuO rewoP r e A • • • • al n o ati N

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