| 飞机起落架缓冲性能分析、试验、设计一体化技术 |
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| 引用本文： | 齐丕骞,牟让科.飞机起落架缓冲性能分析、试验、设计一体化技术[J].航空学报,1998,19(3):332-334. |
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| 作者姓名： | 齐丕骞 牟让科 |
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| 作者单位： | 飞机强度研究所,西安,710065 |
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| 摘 要： | 提出了一种飞机起落架缓冲性能分析、试验、设计一体化的工程方法。利用起落架落震试验结果，自动识别缓冲器空气压缩多变指数和油孔流量系数等不可测参数，以便建立准确的起落架数学模型；并在此基础上对缓冲器充填参数和油孔尺寸进行优化设计，使得起落架着陆最大冲击载荷达到最小。试验验证结果表明，该方法是成功且有效的。
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| 关 键 词： | 起落架 缓冲器 参数识别 优化设计 |
INTEGRATION OF SHOCK\|ABSORBER PERFORMANCE ANALYSIS, TEST AND DESIGN OF AIRCRAFT LANDING GEARS |
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| Qi Piqian,Mu Rangke.INTEGRATION OF SHOCK\|ABSORBER PERFORMANCE ANALYSIS, TEST AND DESIGN OF AIRCRAFT LANDING GEARS[J].Acta Aeronautica et Astronautica Sinica,1998,19(3):332-334. |
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| Authors: | Qi Piqian Mu Rangke |
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| Institution: | Aircraft Strength Research Institute, Xi′an, 710065 |
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| Abstract: | An integration method of shock absorber performance analysis, test and design of aircraft landing gears is presented. By this method, the air polytropic exponent and the orifice discharge coefficient of shock strut can be automatically identified by using drop test results of the landing gear, and the maximum impact load of the landing gear on the runway can be minimized by adjusting the filling parameters and the variable orifice size of the shock absorber. The test results show that the presented algorithm is successful and effective. |
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| Keywords: | landing gear shock absorber parameter identification optimization |
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