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空中加油过程受油装置载荷测量方法及地面试验验证

文敏 张霞妹 牛宏伟 张强波

文敏,张霞妹,牛宏伟, 等. 空中加油过程受油装置载荷测量方法及地面试验验证[J]. 机械科学与技术,2020,39(8):1307-1312 doi: 10.13433/j.cnki.1003-8728.20190210
引用本文: 文敏,张霞妹,牛宏伟, 等. 空中加油过程受油装置载荷测量方法及地面试验验证[J]. 机械科学与技术,2020,39(8):1307-1312 doi: 10.13433/j.cnki.1003-8728.20190210
Wen Min, Zhang Xiamei, Niu Hongwei, Zhang Qiangbo. Load Measurement Scheme of Refueling Receptacles in Aerial Refueling Process and Ground Test Verification[J]. Mechanical Science and Technology for Aerospace Engineering, 2020, 39(8): 1307-1312. doi: 10.13433/j.cnki.1003-8728.20190210
Citation: Wen Min, Zhang Xiamei, Niu Hongwei, Zhang Qiangbo. Load Measurement Scheme of Refueling Receptacles in Aerial Refueling Process and Ground Test Verification[J]. Mechanical Science and Technology for Aerospace Engineering, 2020, 39(8): 1307-1312. doi: 10.13433/j.cnki.1003-8728.20190210

空中加油过程受油装置载荷测量方法及地面试验验证

doi: 10.13433/j.cnki.1003-8728.20190210
详细信息
    作者简介:

    文敏(1990−),工程师,硕士,研究方向为航空发动机强度振动飞行试验技术,wenmin0504205@163.com

  • 中图分类号: V228.1

Load Measurement Scheme of Refueling Receptacles in Aerial Refueling Process and Ground Test Verification

  • 摘要: 受油装置作为受油机的重要机构与加油设备建立输油通道,与加油设备对接过程中的载荷大小对于受油装置结构强度设计具有重要意义。本文根据受油装置结构形式,提出基于应变电测原理的受油装置对接载荷测量方法。在空中加油吊舱地面调试试验期间搭建可移动式测试系统,验证对接载荷测量思路及方法,获取了锥套与受油插头对接过程中受油管上的应变数据,分析了对接过程中的载荷变化规律,并结合受油管几何模型估算给出了对接过程中的轴向载荷大小,为后续空中加油过程对接载荷测量进行了原理及可行性验证。
  • 图  1  F-105D轰炸机的收放式受油装置

    图  2  拉/弯/扭组合作用时布片及组桥原理

    图  3  应变电桥

    图  4  受油管应变计改装位置

    图  5  测试系统示意

    图  6  试验测试现场

    图  7  典型对接过程应变测试结果

    图  8  受油插头结构示意图

    图  9  不同对接速度下应变变化曲线

    表  1  不同对接速度下对接载荷计算结果

    对接速度/(m·s−1)0.30.60.91.2
    对接载荷/N3 1863 2593 2874 011
    下载: 导出CSV
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出版历程
  • 收稿日期:  2019-05-09
  • 刊出日期:  2020-08-05

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