舰载机缩比落震动载荷预计及试验技术1)

PREDICTION AND TESTING TECHNOLOGY OF VIBRATION LOAD FOR SCALED-MODEL OF CARRIER BASED AIRCRAFT1)

  • 摘要: 舰载飞机全机落震试验是考核机体结构、起落架以及机载设备承受舰动态冲击载荷能力的整机级试验,但作为大型动态试验,其试验规模大、准备周期长,一般承制单位难以实施。本文提出了一种舰载机缩比落震动载荷预计及试验方法,该方法在保证动力学相似的前提下,将原型机按照等比原则进行缩放;同时,设计了一套全机落震试验方法,经过动力学相似理论的推导,可将缩比模型落震试验结果还原到原型机载荷。该方法以较低成本预测了原型机全机落震试验结果,经过原型机试验验证,满足试验预计精度,在一定程度上可对舰面动载荷进行提前预计与分析。

     

    Abstract: The whole aircraft drop test for a carrier based aircraft aims to examine the bearing capacity of the aircraft body structure, the landing gear and the airborne equipment. However, it is difficult to carry out the whole aircraft drop test, as a large-scale dynamic test, because of the cost and the long preparation period required. This paper proposes a test method for prediction and analysis of the dynamic load of carrier based aircraft, based on the principle of scaling the prototype aircraft on the premise of ensuring the dynamic similarity. At the same time, a set of the full aircraft drop test methods is designed, derived from the dynamic similarity theory. The drop test results of the scaled model can be restored to the prototype ones. This method can be used to predict the whole aircraft drop test results of the prototype aircraft with a low cost. The test results of the prototype aircraft show that the prediction accuracy of the test is satisfactory, and the dynamic load on the ship surface can be predicted by the test method.

     

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