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支柱柔性对起落架缓冲器摩擦力的影响 被引量:9

Effect of Shock Strut Flexibility on Landing Gear Shock Absorber Friction Force
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摘要 旨在通过缓冲支柱柔性对起落架缓冲器摩擦力的影响研究,为起落架缓冲器摩擦力建模方法和柔性起落架防卡滞设计提供技术指导。伴随着超高强度钢的逐步应用,刚度问题成为起落架设计中日益突出的矛盾问题,传统的缓冲支柱刚性假设可能并不适用于一些新类型起落架的分析。本文结合某无人机飞行试验中出现的主起落架缓冲器卡滞问题,首次建立了考虑支柱柔性影响的起落架缓冲器摩擦力模型,计算了最严重工况下的摩擦力值,并与缓冲支柱刚性假设计算得到的摩擦力值进行了对比分析。分析表明在考虑支柱柔性和理想平面滑动轴承约束的情况下,摩擦力大小为原来的6倍,缓冲器发生卡滞。分析了平面滑动轴承的实际约束情况,提出了轴承支承变形协调系数的概念,并分析了其与摩擦力和卡滞的关系,进而研究了支柱外筒和活塞杆刚度对于缓冲器摩擦力的影响。研究表明在变形协调系数不小于0.53时,缓冲器发生卡滞;适当改变活塞杆和外筒的刚度使其相匹配可以降低缓冲器的摩擦力。 In order to provide a new modeling method of the landing gear shock absorber friction force and offer technical advice about shock absorber binding, influence of the shock strut flexibility on landing gear shock absorber friction force is researched. With the use of high-strength steel, stiffness becomes an ever more serious issue. Traditional rigid shock strut presupposition may not be suitable for analysis of new types of aircraft landing gear. To address the binding occurring to an unmanned aircraft, a landing gear shock absorber friction force model is established with the shock strut flexibility taken into consideration. The friction force under the most serious case is calculated, and is compared with the force calculated without taking shock strut flexibility into account. The study shows that in the case when the shock strut flexibility is considered and under the ideal planar slide constraint, the friction force is 6 times that of the rigid model. The friction force thus can lead to shock absorber binding. Furthermore, the actual constraint forms are analyzed, and the coefficient of bearing deformation consistency is presented. The relationships of this coefficient with the friction force and shock absorber binding are analyzed. The influence is studied of the flexibility of the shock strut inner cylinder and outer cylinder on the value of the friction force. The study shows that the shock absorber will get stuck as the coefficient of bearing deformation consistency becomes no less than 0.53. Decreasing the inner cylinder's flexibility or increasing the outer cylinder's flexibility can decrease the shock absorber friction force.
出处 《航空学报》 EI CAS CSCD 北大核心 2014年第6期1604-1611,共8页 Acta Aeronautica et Astronautica Sinica
基金 国家自然科学基金(51105197 11372129 51305198) 江苏高校优势学科建设工程资助项目~~
关键词 起落架 缓冲器 支柱柔性 摩擦力 卡滞 anding gear shock absorber shock strut flexibility friction force binding
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参考文献22

  • 1聂宏.起落架的缓冲性能分析与设计及其寿命计算方法[D].南京:南京航空航天大学航空宇航学院,1990.
  • 2Chester D H. Aircraft landing impact parametric study with emphasis on nose gear landing conditions[J]. Journal of Aircraft, 2002, 39(3): 394-403.
  • 3Evans P, Perhinschi M G, Mullins S. Modeling and simulation of a tricycle landing gear at normal and abnormal conditions, AIAA-2010-7618. Reston: AIAA, 2010.
  • 4Batterbee D C, Sims N D, Stanway R, et al. Design and performance optimization of magneto rheological oleo pneumatic landing gear//Proceedings of SPIE Vol. 5760. Bellingham: WA, 2005.
  • 5Gerardi A G. Digital simulation of flexible aircraft response to symmetrical and asymmetrical runway roughness, AFFDL-TR-77-37. Dayton, OH: Wright-Patterson AFB, 1977.
  • 6顾宏斌.飞机地面运行的动力学模型[J].航空学报,2001,22(2):163-167. 被引量:53
  • 7袁东.飞机起落架仿真数学模型建立方法[J].飞行力学,2002,20(4):44-47. 被引量:35
  • 8Ro K. A descriptive modeling and simulation of aircraft-runway dynamics, AIAA-2003-1895. Reston: AIAA, 2003.
  • 9贾玉红,何庆芝,杨国柱.主动控制起落架滑行性能分析[J].航空学报,1999,20(6):545-548. 被引量:17
  • 10牟让科,罗俊杰.飞机结构弹性对起落架缓冲性能的影响[J].航空学报,1995,16(2):205-208. 被引量:21

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