期刊文献+

微波推力器独立系统的三丝扭摆推力测量 被引量:6

Thrust Measurement of an Independent Microwave Thruster Propulsion Device with Three-Wire Torsion Pendulum Thrust Measurement System
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摘要 为了探究微波推力器的推力性能,采用三丝扭摆推力测量方法对微波推力器独立系统开展推力测量实验,同时分析三丝扭摆推力测量装置的数理模型并实验测定其不确定度,由此判断实验测量结果的可信度。推力测量结果表明,现有实验条件下三丝扭摆推力测量装置能测出不低于3m N的推力,其相对不确定度为14%;在三丝扭摆推力测量装置的推力测量范围内,没有测出微波推力器独立系统显著的推力,而是在230W微波功率输出条件下测出推力在±0.7m N范围内波动,相对不确定度大于80%。 In order to explore the thrust performance of microwave thruster,the thrust produced by micro-wave thruster system was measured with three-wire torsion pendulum thrust measurement system and the mea-surement uncertainty was also studied,thereby judging the credibility of the experimental measurements. The re-sults show that three-wire torsion pendulum thrust measurement system can measure thrust not less than 3mN un-der the existing experimental conditions with the relative uncertainty of 14%. Within the measuring range of three-wire torsion pendulum thrust measurement system,the independent microwave thruster propulsion device did not detect significant thrust. Measurement results fluctuate within ± 0.7mN range under the conditions 230W microwave power output,and the relative uncertainty is greater than 80%.
出处 《推进技术》 EI CAS CSCD 北大核心 2016年第2期362-371,共10页 Journal of Propulsion Technology
关键词 微波推力器 三丝扭摆 推力测量 不确定度 Microwave thruster Three-wire torsion pendulum Thrust measurement Uncertainty
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参考文献18

  • 1Freedman J H. Design of a Multi-Spool High-Speed Counter-Rotating Aspirated Compressor[D]. USA: Massachusetts Institute of Technology,2000.
  • 2Talbotec J,Vernet M. Counter Rotating Fan Aerodynamic Design Logic & Tests Results[R]. ICAS-2010.
  • 3Mileshin V I, Pankov S V, Fateev VA. Ducted Counter-Rotating Fan Blades Optimization Based on 3D Inverse Problem Solution Aiming at Fan Gasdynamics Improvement[R]. ISABE-2009-1334.
  • 4Eberhard Nicke, Robert Meyer, Andreas Bischoff, et al. Design of an Economical Counter Rotating Fan-Comparison of the Calculated and Measured Steady and Unsteady Results[R]. ASME GT-2012-69587.
  • 5季路成.对转叶轮机技术挑战分析[J].推进技术,2007,28(1):40-44. 被引量:13
  • 6刘波,陈云永,项效镕,侯为民.对转压气机数值模拟及实验研究[J].推进技术,2008,29(4):454-457. 被引量:19
  • 7刘波,侯为民,陈云永,赵旭民.对转压气机转差特性试验与数值模拟[J].航空动力学报,2009,24(2):403-408. 被引量:15
  • 8杨琳,陈雷,孙海,杨明绥.对转风扇设计技术研究[J].航空学报,2014,35(5):1226-1235. 被引量:5
  • 9Brailko I A, Mileshin V I, Nyukhtikov M A, et al. Computational and Experimental Investigation of Unsteady and Acoustic Characteristic of Counter-Rotating Fans[R]. ASME HT-FED04-56435.
  • 10Knapke Robert D, Turner Mark G. Unsteady Simulations of a Counter-Rotating Aspirated Compressor[R]. ASME GT-2013-95209.

二级参考文献57

  • 1王掩刚,刘波,陈云永,姜健.双级对转压气机流场分析研究[J].西北工业大学学报,2006,24(1):97-101. 被引量:21
  • 2肖朋,王军.对旋叶栅级间内流干涉的数值研究[J].热能动力工程,2006,21(3):249-254. 被引量:3
  • 3卢新根,楚武利,朱俊强,吴艳辉,刘志伟.轴流压气机机匣处理研究进展及评述[J].力学进展,2006,36(2):222-232. 被引量:44
  • 4JI Lucheng, XIANG Lin, HUANG Bo,et al. The revelations from the research about the vaneless counter-rotating turbine[R]. ISABE-2003 1040, 2003.
  • 5Pronomariov B A. Using counter-rotating rotors for de creasing size and component number in small GTE[R]. ASME Paper , 92-GT-414, 1992.
  • 6Pempie P, Ruet L. Counter-rotating turbine designed for turbopunp rocket engine[C]// 39th AIAA/ASME/SAE/ ASEE Joint Propulsion Conference and Exhibit Huntsville. Alabama: [s. n. ], 2003.
  • 7Sharma P B, Adekoya A. A review of recent research on counter rotating axial flow compressor stage[R]. ASME 96-GT 254, 1996.
  • 8Roy B, Ravibabu K, Rao P S,et al. Flow studies in dueted twin-rotor counter-rotating axial flow fans [R]. ASME92-GT-390, 1992.
  • 9Kerrebrock J L, Epstein A H, Merchant A A. Design and test of an aspirated counter-rotating fan [R]. ASME Turbo. Expo. , GT2006-90582, 2006.
  • 10Miller D A J,Chappel M S.The co-turbo shaft-a novel gas turbine power plant for heavy equipment[R].ASME 79-GT-132,1979.

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