Analysis on Arresting Performance of Carrier-based Arresting Device

Abstract

Abstract:

To obtain the performance and design method of carrier-based arresting device, the components and the function of carrier-based arresting device were analyzed. A dynamic model of carrier-based arresting device was established and the aircraft arresting force was deduced. A set of curves about constant runout control valve area with different aircraft masses were calculated under the constant runout conditions, also the longitudinal dynamic performances of aircraft were obtained. The results show that different mass aircrafts can be stopped in the limited distance by changing the area of constant runout control valve of carrier-cased arresting device, the overload and arresting distance are satisfied with the requirements of American military standard.

Key words: carrier-based aircraft, arresting device, hydraulic, constant runout control valve

摘要：

为得到舰载型拦阻装置的性能及设计方法,分析了拦阻装置的组成及工作方式,建立了舰载型拦阻装置的动力学模型,给出了飞机航向拦阻力方程。计算得到了定长冲跑条件下,不同质量飞机拦阻时定长冲跑阀油孔面积随主液压缸行程的曲线组,同时得到了飞机航向的动力学性能。研究结果表明:通过改变定长冲跑阀的油孔面积,不同质量的飞机可在限定拦阻距离内拦停,飞机的拦阻力及拦阻距离均满足美军标取值范围。

关键词: 舰载机, 拦阻装置, 液压, 定长冲跑阀

CLC Number:

Liu Gang, Nie Hong, Ren Zhiyong, Jia Jin, Ren Guoxian. Analysis on Arresting Performance of Carrier-based Arresting Device[J]. China Mechanical Engineering, 2014, 25(9): 1244-1249,1255.

柳刚, 聂宏, 任志勇, 贾锦, 任国贤. 舰载型拦阻装置拦阻性能分析[J]. 中国机械工程, 2014, 25(9): 1244-1249,1255.

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