舰载飞机拦阻钩载荷实测方法研究

doi:10.7527/S1000-6893.2014.0334

固体力学与飞行器总体设计

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舰载飞机拦阻钩载荷实测方法研究

杨全伟

中国飞行试验研究院, 西安 710089

收稿日期:2014-05-05 修回日期:2014-12-03 出版日期:2015-04-15 发布日期:2014-12-15
通讯作者: 杨全伟Tel.: 029-86837951 E-mail: yyangqw@163.com E-mail:yyangqw@163.com
作者简介:杨全伟男, 硕士, 高级工程师。主要研究方向: 飞行器结构强度飞行试验。Tel: 029-86837951 E-mail: yyangqw@163.com
基金资助:
省部级项目

Research on flight measurement method of a carrier-based aircraft arresting hook loads

YANG Quanwei

Chinese Flight Test Establishment, Xi'an 710089, China

Received:2014-05-05 Revised:2014-12-03 Online:2015-04-15 Published:2014-12-15
Supported by:
Ministry Level Project

摘要/Abstract

摘要：

为完成某舰载飞机飞行试验任务,采用应变法实测了其拦阻着舰时的拦阻钩载荷。在分析着舰拦阻过程中拦阻钩受载状态的基础上,建立了拦阻钩纵向、侧向和垂向这3个方向上的载荷模型;对拦阻钩钩臂进行内力分析,设计了载荷测量应变电桥,并进行了载荷校准,建立了载荷方程。给出并详细分析了典型拦阻过程中的拦阻钩载荷,计算了拦阻功量及拦阻系统的效率。最后,通过与常规单向载荷模型的对比,探讨了采用三向载荷模型的意义。分析表明,建立的模型和采用的方法正确,结果合理可信,可供相关工程参考。

关键词: 飞行试验, 载荷实测, 舰载飞机, 拦阻钩, 拦阻着舰, 应变电桥

Abstract:

For the purpose of complete flight test mission of a carrier-based aircraft, its arresting hook loads are measured using strain gage. A three-direction (longitudinal, lateral and vertical directions) load model of arresting hook is built through analyzing the loads in the arrest deck-landing process. Strain gages are designed and installed on the arresting hook. Ground calibration tests are implemented and load equations are constructed. Some typical loads of arresting hook in the process of carrier-based aircraft arrest deck-landing are also presented in detail, and the arresting energy and efficiency of arresting gear equipment are studied. Moreover, compared with the loads obtained by an ordinary single-direction load model, the three-direction load model is discussed. The results show that the load model and measurement methods are correct and credible, which can provide some references for the engineering practice.

Key words: flight test, flight measurement of load, carrier-based aircraft, arresting hook, arrest deck-landing, strain-gage bridge

中图分类号:

V217⁺.32

杨全伟. 舰载飞机拦阻钩载荷实测方法研究[J]. 航空学报, 2015, 36(4): 1162-1168.

YANG Quanwei. Research on flight measurement method of a carrier-based aircraft arresting hook loads[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(4): 1162-1168.

参考文献

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E-mail：hkxb@buaa.edu.cn

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

舰载飞机拦阻钩载荷实测方法研究

Research on flight measurement method of a carrier-based aircraft arresting hook loads

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