| [1] |
Meisl C J.Life cycle cost considerations for launch vehicle liquid propellant rocket engine[R].AIAA 86-1408,1986.
|
| [2] |
Williams W C.Report of the SSME assessment team[R].NASA N93-21645,1993.
|
| [3] |
Sackheim R L.SSME 0523 incident investigation[R].NASA 1.2:019296,2002.
|
| [4] |
Karns J J.Space shuttle catastrophic failure frequencies final report[R].NASA-CR-25809,1993.
|
| [5] |
朱志斌,杨尔辅,张振鹏.液体火箭发动机故障模式与影响分析[C]//中国宇航学会1998年联合推进会议论文集.烟台:中国宇航学会,1998:278-284.
|
| [6] |
Early D.SSME FMEA/CIL redundancy screen[R].NASA Report B300-0302,1999.
|
| [7] |
Clark D F.Failure mode,description and effect[R].NASA Report B300,2001.
|
| [8] |
Paster R D,Stohler S L.SSME evolution[R].AIAA 89-2618,1989.
|
| [9] |
Jue F H.Space shuttle main engine:thirty years of innovation[R].NASA-46693,2002.
|
| [10] |
Biggs R E.Space shuttle main engine the first ten years[M]//Doyle S E.History of liquid rocket engine development in the United States.Springfield:the AAS Publication,1992:69-122.
|
| [11] |
Rickman D K.ALS liquid hydrogen turbopump[R].NASA-CR194646,1993.
|
| [12] |
Van Hooser K.Space shuttle main engine relentless pursuit of improvement[R].Huntsville,AL:Marshall Space Flight Center:M11-1028,2011.
|
| [13] |
Blair J,Ryan R.Lessons learned in engineering[R].NASA/CR-216468,2011.
|
| [14] |
Rocketdyne Propulsion and Power.Space shuttle main engine orientation[EB/OL].[2012-9-10].http://large.stanford.edu/courses/2011/ph240/nguyen1/docs/SSME_PRESENTATION.pdf.
|
| [15] |
Newell J F,WKurth R E,Ho H.Composite load spectra for select space propulsion structural components[R].NASA-CR-179496,1986.
|
| [16] |
NASA Lewis Research Center.Rotordynamic instability problems in high-performance turbomachinery[R].NASA-CP-3026,1989.
|
| [17] |
Pool K V.Space shuttle main engine structural analysis and data reduction/evaluation:Volume 4 high pressure fuel turbopump inlet housing analysis[R].NASA-CR-183667,1989.
|
| [18] |
Becht D G,Hawkins L A,Scharrer J K,et al.NASA Lewis Research Center rotordynamic instability problems in high-performance turbomachinery[M].California:Lewis Research Center,1991:191-202.
|
| [19] |
谢光军,胡海峰,秦国军,等.液体火箭发动机涡轮泵健康监控系统[J].国防科技大学学报,2005,27(3):40-44. XIE Guangjun,HU Haifeng,QIN Guojun,et al.The health monitoring system of turbopump for liquid rocket engine[J].Journal of National University of Defense Technology,2005,27(3):40-44.(in Chinese)
|
| [20] |
Cikanek H A.Space shuttle main engine failure detection[J].IEEE Control Systems Magazine,1986,6(3):13-18.
|
| [21] |
Agogino A,Tumer K.Entropy based anomaly detection applied to space shuttle main engines[R].Big Sky,MT:IEEE Aerospace Conference,2006.
|
| [22] |
Moore N R,Ebbeler D H,Newlin L E,et al.An improved approach for flight readiness certification-methodology for failure risk assessment and application examples:methodology and applications[R].NASA-CR-194499,1992.
|
| [23] |
Hale J K,Wood B K.Operational life improvement of SSME high-pressure turbopumps[J].Acta Astronautica,1987,15(12):1009-1018.
|
| [24] |
Chyu M K.A performance/loss evaluation of SSME HPFTP turbine[R].Washington DC:Alabama University Research Reports 89N21735/0,1988.
|
| [25] |
National Aeronautics and Space Administration.Liquid rocket engine turbines[R].NASA-SP-8110,1974.
|
| [26] |
Hartong A R,Rooney B D.Near-term RLV options[R].AIAA-2004-5947,2004.
|
| [27] |
Heppenheimer T A.The space shuttle decision:NASA's search for a reusable space vehicle[R].NASA/SP-4221,1999.
|
| [28] |
Furst R B.Space shuttle main engine turbopump design and development[R].AIAA 75-1301,1975.
|
| [29] |
Glover R C,Kelley B A,Tischer A E.SSME failure data review,diagnostic survey and SSME diagnostic evaluation[R].NASA-CR-178993,1986.
|
| [30] |
Cikanek H A.Characteristics of space shuttle main engine failures[R].AIAA 87-1939,1987.
|
| [31] |
Hopson G.Atlantis STS-104 space shuttle program SSME flight readiness review[R].Washington DC:Space Shuttle SR&QA Assessment,2001.
|
| [32] |
Sujata M,Madan M,Raghavendra K,et al.Identification of failure mechanisms in nickel-base superalloy turbine blades through microstructural study[J].Engineering Failure Analysis,2010,17(6):1436-1446.
|
| [33] |
Abdul-Aziz A,Thompson R L.Thermal-structural analysis of space shuttle main engine(SSME) hot section components[R].NASA-22404,1988.
|
| [34] |
Abdul-Aziz A.Structural evaluation of a space shuttle main engine (SSME) high pressure fuel turbopump turbine blade[R].NASA CR-198428,1996.
|
| [35] |
Abdul-Aziz A.Assessment of crack growth in a space shuttle main engine first-stage high pressure fuel turbopump blade[J].Finite Element in Analysis and Design,2002,39(2):1-15.
|
| [36] |
Hudson S T.Rocket engine turbine blade surface pressure distribution:experiment and components[R].AIAA-2000-3239,2002.
|
| [37] |
Hopson G.Discovery STS-103 space shuttle program SSME flight readiness review[R].Washington DC:Space Shuttle SR&QA Assessment,1999.
|
| [38] |
Davis G,Clough R.Blade tip rubbing stress prediction[R].NASA-CR-184100,1991.
|
| [39] |
Carter T J.Common failure in gas turbine blades[J].Engineering Failure Analysis,2005,12(2):237-247.
|
| [40] |
SHI Duoqi,DONG Chengli,YANG Xiaoguang.Constitutive modeling and failure mechanisms of anisotropic tensile and creep behaviors of nickel-base directionally solidified superalloy[J].Materials and Design,2013,45:663-673.
|
| [41] |
In-Hwan S,Dong-Keun L,Yongseck K,et al.Assessment of the characteristic of thermal barrier coating applied to gas turbine blade by thermo-gradient mechanical fatigue test[J].Procedia Engineering,2013,55:210-213.
|
| [42] |
Yongseok K,Dong-Keun L,In-Hwan S,et al.Microstructural analysis of TMF failure mechanism of GTD-111 applied to gas turbine blades[J].Procedia Engineering,2013,55:204-209.
|
| [43] |
Sadowski T,Golewski P.Multidisciplinary analysis of the operational temperature increase of turbine blades in combustion engines by application of the ceramic thermal barrier coatings(TBC)[J].Computational Materials Science,2011,50(4):1326-1335.
|
| [44] |
Robinson J K,Teal C A,Welch C T.Space shuttle main engine powerhead structural modeling,stress and fatigue life analysis:Volume 1 gas dynamic environment of the SSME HPFTP and HPOTP turbine[R].NASA-CR-170999,1983.
|
| [45] |
Robinson J K,Teal C A,Welch C T.Space shuttle main engine powerhead structural modeling,stress and fatigue life analysis:Volume 2 dynamics of blades and nozzles-SSME HPFTP and HPOTP[R].NASA-CR-171000,1983.
|
| [46] |
Robinson J K,Teal C A,Welch C T.Stress summary of blades and nozzles at FPL and 115% RPL loads SSME HPFTP and HPOTP blades and nozzles[R].NASA-CR-171001,1983.
|
| [47] |
Robinson J K,Teal C A,Welch C T.Summary of investigation of unshielduler events and special tests[R].NASA-CR-171002,1983.
|
| [48] |
Myers D D,Fletcher J C.Aerospace safety advisory panel[R].Washington DC:NASA 1986 annual report,1986.
|
| [49] |
Stallworth R,Wilson C,Meyers C.Compendium of fracture mechanics problems[R].NASA-TM-100393,1990.
|
| [50] |
孙瑞杰,闫晓军.涡轮叶片榫齿部位疲劳/蠕变试验的新特点[J].航空动力学报,2007,22(3):419-424. SUN Ruijie,YAN Xiaojun.New characteristics of fatigue-creep tests on serration of turbine blade[J].Journal of Aerospace Power,2007,22(3):419-424.(in Chinese)
|
| [51] |
Dong-Keun L,In-Hwan S,Yongseck K,et al.A study on fatigue life prediction of Ni-base superalloy[J].Procedia Engineering,2013,55:631-635.
|
| [52] |
Dominic R J.Turbine blade friction damper study[R].NASA 85N22798,1985.
|
| [53] |
Muszynska A,Bently D E,Franklin W D,et al.Influence of rubbing on rotor dynamics[R].NASA-CR-183648-PT-1,1989.
|
| [54] |
Wilmer G E.Turbine blade tip and seal clearance excitation forces[R].NASA-CR-171534,1992.
|
| [55] |
Moore J H.Turbomachinery design quality checks to avoid friction induced structural failure[R].NASA-0046248,1999.
|
| [56] |
Arakere N K,Swanson G.Fretting stresses in single crystal superalloy turbine blade attachments[J].Journal of Tribology,2001,123(2):413-423.
|
| [57] |
Robinson J K.Investigation of the HPFTP first stage impeller crack[R].NASA-CR-171281,1984.
|
| [58] |
Vance J,Zeidan F,Murphy B.Machinery vibration and rotordynamics[M].Hoboken,New Jersey:Wiley & Sons,2010.
|
| [59] |
Chileds D W.SSME HPFTP interstage seals:analysis and experiments for leakage and reaction-force coefficient:part Ⅰ[R].NASA-CR-170851,1983.
|
| [60] |
Matthew C E.Solution of the subsynchronous whirl problem in the high-pressure hydrogen turbomachinery of the space shuttle main engine[R].AIAA 78-1002,1978.
|
| [61] |
Jery B,Brennen C E,Caughey T K.Impeller forces on centrifugal pump[C]//Proceedings of the Second International Pump Symposium.College Station,Texas:California Institute of Technology,1985:21-32.
|
| [62] |
Black H F,Jenssen D N.Effects of high ring seals on pump rotor vibrations[R].ASME Paper 71-WA-FE-36,1971.
|
| [63] |
Chileds D W.SSME HPFTP interstage seals:analysis and experiments for leakage and reaction-force coefficient:Part Ⅱ[R].NASA-CR-170851,1983.
|
| [64] |
Groda D R,Prabhu B S.High-pressure annular seal leakage and rotordynamics with application to turbomachinery[J].International Journal of Rotating Machinery,2002,8(6):403-411.
|
| [65] |
Hendricks R C,Steinetz B M,Braun M J.Turbomachine sealing and secondary flows:Part 1 review of sealing performance,customer,engine designer,and research issues[R].NASA/TM-211991/PT1,2004.
|
| [66] |
Darden J M,Earhart E M,Flowers G T.Comparison of the dynamic characteristics of smooth annular seals and damping seals[J].Journal of Engineering for Gas Turbines and Power,2001,123(4):857-863.
|
| [67] |
Kwanka K.Improving the stability of labyrinth gas seals[J].Journal of Engineering for Gas Turbines and Power,2001,123(2):383-388.
|
| [68] |
Childs D W,Ramsey C.Seal-rotordynamic-coefficient test results for a model SSME ATD-HPFTP turbine interstage seal with and without a swirl brake[J].Journal of Tribology,1991,113(1):198-203.
|
| [69] |
Murphy B T,Scharrer J K,Hawkins L A.The SSME HPFTP wavy interstage seal:Part Ⅱ rotor dynamic analysis[R].ASME Publication DE-VOL.18-2,1989.
|
| [70] |
Gibson H G,Thom R,Moore C,et al.History of space shuttle main engine turbopump bearing testing at the Marshall Space Flight Center[R].NASA-M10-0338,2010.
|
| [71] |
Gibson H G.SSME bearing and seal tester data compilation,analysis and reporting and refinement of the cryogenic bearing analysis mathematical model[R].NASA-CR-210139,2000.
|
| [72] |
古乐,王黎钦,李秀娟,等.超低温氢氧泵轴承技术研究及进展[J].中国机械工程,2002,13(7):620-623. GU Le,WANG Liqin,LI Xiujuan,et al.Study and review of liquid hydrogen/oxygen turbo-pump cryogenic bearing technology[J].China Mechanical Engineering,2002,13(7):620-623.(in Chinese)
|
| [73] |
马美玲,邓四二,梁波,等.火箭发动机低温轴承的设计[J].轴承,2006(6):10-12. MA Meiling,DENG Sier,LIANG Bo,et al.The cryogen bearing design of liquid rocket engine[J].Bearing,2006(6):10-12.(in Chinese)
|
| [74] |
Lu D,Zhao W,Lu B,et al.Static characteristics of a new hydrodynamic rolling hybrid bearing[J].Tribology International,2012,48:87-92.
|
| [75] |
Santos E N,Blanco C J C,Macedo E N,et al.Integral transform solutions for the analysis of hydrodynamic lubrication of journal bearings[J].Tribology International,2012,52:161-169.
|
| [76] |
Butner M F,Murphy B T.SSME long life bearings[R].NASA-CR-179455,1986.
|
| [77] |
Dwivedi V K,Chand S,Pandey K N.Effect of number and size of recess on the performance of hybrid:hydrostatic/hydrodynamic journal bearing[J].Procedia Engineering,2013,51:810-817.
|
| [78] |
白长青,许庆余,张小龙.滚动轴承—火箭发动机液氢涡轮泵转子系统的动力特性分析[J].航空学报,2006,27(2):258-261. BAI Changqing,XU Qingyu,ZHANG Xiaolong.Dynamic properties analysis of ball bearing-liquid hydrogen turbopump used in rocket engine[J].Acta Aeronautica et Astronautica Sinica,2006,27(2):258-261.(in Chinese)
|
| [79] |
Meisl C J.Rocket engine vs.jet engine comparison[R].AIAA 92-3686,1992.
|
| [80] |
Breithaupt B S.Space shuttle main engine turbopump bearing assessment program[R].NASA-TM-108447,1994.
|
| [81] |
Yang Y,Yinxia L,Guang M,et al.A hybrid feature selection scheme for unsupervised learning and its application in bearing fault diagnosis[J].Expert Systems with Applications,2011,38(9):11311-11320.
|
| [82] |
Georgoulas G,Loutas T,Stylios C D,et al.Bearing fault detection based on hybrid ensemble detector and empirical mode decomposition[J].Mechanical Systems and Signal Processing,2013,41(1/2):510-525.
|
| [83] |
Elrod D A.Investigation of SSME alternate high pressure fuel turbopump lift-off seal fluid and structural dynamics interaction[R].NASA/ASEE N90-19400,1989.
|
| [84] |
Clark D F.Failure mode,description and effect:loss of containment in the pump with leakage into the turbine[R].NASA Report B300-0302,2001.
|
| [85] |
Chupp R E,Hendricks R C,Lattime S B,et al.Turbomachinery clearance control[M].Cleveland,US:NASA Glenn Research Center,2007.
|
| [86] |
Hendricks R C,Tam L T,Muszynska A.Turbomachine sealing and secondary flows:Part 2 review of rotordynamics issues in inherently unsteady flow systems with small clearance[R].NASA/TM-211991/PT2,2004.
|
| [87] |
Hopson G.Atlantis STS-106 space shuttle program SSME flight readiness review[R].Washington DC:Space Shuttle SR&QA Assessment,2000.
|
| [88] |
Keegan W B.Terrestrial environment criteria handbook for use in aerospace vehicle development[M].Alabama,US:NASA Technical Standards Program Office,2000.
|
| [89] |
Kaminski K E.Space shuttle contamination control requirements[R].Washington DC:SN-C-0005,1998.
|