| 飞行载荷发展综述 |
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| 引用本文： | 闫中午,宗宁,任文广,李志.飞行载荷发展综述[J].航空工程进展,2020,11(6):873-886. |
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| 作者姓名： | 闫中午 宗宁 任文广 李志 |
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| 作者单位： | 中国商用飞机有限责任公司上海飞机设计研究院,上海201210,沈阳飞机设计研究所扬州协同创新研究院有限公司,扬州225000,中国商用飞机有限责任公司上海飞机设计研究院,上海201210,中国航空工业集团有限公司沈阳飞机设计研究所,沈阳110035 |
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| 摘 要： | 飞行载荷设计是飞行器设计的一个重要组成部分,是连接总体气动设计和结构强度设计的桥梁。本 文从飞行载荷设计所需要遵循的规范、飞行载荷的设计方法、严重载荷选取、飞行载荷的验证等方面对飞行器 飞行载荷设计的发展历程进行了回顾,并对未来飞行载荷的发展方向进行了展望。
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| 关 键 词： | 飞行载荷 结构强度规范 适航条例 机动载荷 分布载荷 试飞 |
| 收稿时间： | 2020/10/10 0:00:00 |
| 修稿时间： | 2020/12/12 0:00:00 |
Overview of Flight Loads Development |
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| YAN ZHONGWU,ZONG NING,REN WENGUANG,Li zhi.Overview of Flight Loads Development[J].Advances in Aeronautical Science and Engineering,2020,11(6):873-886. |
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| Authors: | YAN ZHONGWU ZONG NING REN WENGUANG Li zhi |
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| Institution: | SADRI;Yangzhou Collaborative Innovation Research Institute of Shenyang Aircraft Design and Research Institute Co. Ltd |
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| Abstract: | Flight load design is an important part of aircraft design. It is a bridge connecting the General&Aerodynamic and Structure&Stress. In this paper, the development of flight load design is reviewed in terms of the specifications to be followed, the design methods, and the verification of flight load, especially focuses on the design methods, the selection of severe case and the verification method, and summarizes the advantages and disadvantages of existing design verification methods, and The development direction in the future are carried on. |
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| Keywords: | Flight Loads Specification of structure Stress Airworth Regulation Maneuver Loads Load Distribution Flight Test |
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