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叶栅式反推力装置阻流门运动规律对气动性能的影响 被引量:12

Effect of kinetic mechanism of blocker doors on aerodynamic performance for a cascade thrust reverser
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摘要 在分析叶栅式反推力装置结构及工作原理的基础上,通过计算初步研究了反推力装置运动规律对风扇出口及阻流门上气动载荷的影响.计算结果表明,反推力装置打开时,运动规律直接影响风扇在反推力装置打开/关闭过程中工作点位置,运动规律3,4分别适合风扇外涵喘振裕度较大、较小发动机的反推力装置选用;各运动规律中,阻流门气动载荷在阻流门开始转动瞬间加载. Based on the structure and working principle of the cascade thrust reverser,a preliminary research was conducted to analyze the impact of reverser's kinetic schedule on the exit static pressure of the fan and aerodynamic load of the blocker doors.The results show that,the kinetic schedule directly influences the position of fan's working point during deploying/retracting reverser process.Schedule 3 and 4 are suitable separately for reversers installed in engines with relatively small and big surge margin fan.For all kinetic schedules,aerodynamic load on blocker doors increases sharply once it starts operation.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2010年第6期1297-1302,共6页 Journal of Aerospace Power
关键词 叶栅式反推力装置 阻流门 运动规律 动网格 风扇发动机 cascade thrust reverser blocker doors kinetic mechanism moving grid turbofan
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参考文献13

  • 1Yetter J A. Why do airlines want and use thrust reversers.9 A compilation of airline industry responses to a survey regarding the use of thrust reversers on commercial transport airplanes[R].NASA TM- 109158, 1995.
  • 2陈光.航空燃气涡轮发动机结构设计[M].北京:北京航空学院出版社,1987,274-275.
  • 3刘长福主编.航空发动机构造[M].北京:国防工业出版社,1989.
  • 4刘大响主编.航空发动机设计手册:第7册[M].北京:航空工业出版社,2000.
  • 5Jackson J. Development of the boeing 767 thrust reverser[R]. AIAA-86-1536 , 1986.
  • 6Dietrich D A, Gutierrez O A. Performance of a model cascade thrust reverser for shorthaul applications[R]. AIAA- 74-1171,1974.
  • 7Chuck C, Hsiao E, Colehour J,et al. Navier Stokes calculations of under wing turbofan nacelles[R]. AIAA-98 2734,1998.
  • 8Johus C J. Solution of an engine inlet compatibility problem during C-17 low cost N/EAT nacelle thrust reverser development[R].AIAA-2000-01-5579,2000.
  • 9邵万仁,叶留增,沈锡钢.反推力装置关键技术及技术途径初步探讨[C].中国航空学会2007年学术年会(动力专题),2007.
  • 10杜刚,金捷.大型运输机发动机反推力装置[c]//中国航空学会2007年学术年会论文集.深圳:中国航空学会,2007.

二级参考文献13

  • 1[1]Harold G, Guerty. Area controlled, thrust vectoring vane cascade. US4828173, 1989.5.
  • 2[2]Robert A Jones. Thrust reverser. US4373328,1983.2.
  • 3[3]Jon A Marx, Wendell R Loso. Thurst reverser. US4527391,1985.6.
  • 4[4]Gregory H Matthias, Bonita. Split door thrust reverser for fan jet aircraft engines. US5120004, 1992.6.
  • 5[5]Jihad J Remlaoui. Cascade type aircraft engine thrust reverser with hidden link actuator. US5228641, 1993.7.
  • 6[6]Patrick Gonidec. Pivoting door thrust reverser with deflecting vane. US5893265, 1999.4.
  • 7[7]Robert R Standish. Thrust reverser for high bypass fan engine. US5863014, 1999,1.
  • 8[8]Runyon H Tindell. Blockerless thrust reverser.US5904320, 1995.5.
  • 9[9]Dale W R, Lawson. Aircraft turbine engine thrust reverser.US5230213, 1993.7.
  • 10[10]Jackson J. Development of the Boeing 767 thrust reverser.AIAA- 86 - 1536, 1986.6.

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