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某降落伞伞绳断裂仿真分析 被引量:1

Emulation Analysis for a Parachute’s Suspension Line Fracturing
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摘要 分析了在降落伞充气过程伞衣织物的传力路线 ,得出当连接伞衣的某根伞绳断裂之后其上的力将由与其邻的伞绳承担。并且采用动力学仿真软件ADAMS进行建模 ,针对 During the parachute’s inflation, the stress passing pipelines in the canopy fabric are analyzed. We conclude that: when one suspension line is fractured, the stress in it will be assumed the suspension lines next to it. By means of the software ADAMS, we analyze five situations, and conclude that the most dangerous suspension lines endure larger stress when suspension lines are distantly fractured than when they continuously.
出处 《航天返回与遥感》 2004年第4期15-19,共5页 Spacecraft Recovery & Remote Sensing
关键词 降落伞 伞绳断裂 ADAMS仿真 Parachute Suspension lines fracturing ADAMS
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参考文献5

  • 1降落伞技术编委会.环帆伞设计[J].降落伞技术特刊,1977,.
  • 2Swing E.G,Knacke T.W.,Bixby H.W.著,吴建平等译.回收系统指南.北京:航空工业出版社,1988.
  • 3Lindh K.G., McEwan A.J. Analysis of Tension Impact Tests on the Nylon Webbing Structure of an Apollo Pilot Chute Riser.NASA CR - 101772, . May 1969.
  • 4Groom J.J. A Characterization of Nylon Parachute Webbing With Hysteresis Effects in a Simple Dynamic System. AIAA Paper, No.75 - 1361.
  • 5McCarty R.E.. A Computer Subroutine for the Load- Klongation Characteristics of Parachute Suspension Lines AIAA 75 - 1362.

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