民机起落架系统研制适航工作分析
作者:
作者单位:

作者简介:

通讯作者:

中图分类号:

基金项目:


Author:
Affiliation:

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    在梳理国家适航法规要求、适航管理机制、民机研制过程、适航审定过程的基础上,对民机起落架系统研制过程相关适航工作要求开展分析,明确了民机起落架系统随航空器型号合格审定、生产许可审定和适航合格审定一起批准(随机适航)过程中的适航工作目标和主要适航工作内容,并对起落架系统持续适航工作进行了简要论述。民机起落架系统研制随机适航工作虽然属于航空器适航取证工作的组成部分,但起落架系统研制单位仍承担其产品适航性的“第一责任”,研究内容对民机起落架系统研制单位开展项目策划和研制体系建设具有指导作用。

    Abstract:

    Based on the requirements of national airworthiness regulations, airworthiness management, civil aircraft development process, and airworthiness certification process, this paper analyzes the airworthiness requirements related to the development of civil aircraft landing gear system to define the airworthiness objectives and main tasks of civil aircraft landing gear system in the process of approval (random airworthiness) together with aircraft type certification, production certification and airworthiness certification, and also briefly discusses the continuing airworthiness work of the landing gear system. Although the airworthiness work of the landing gear system is a part of aircraft airworthiness certification, the research and development unit of the landing gear system still bears the “first responsibility” for the airworthiness of its products. The research content has a guiding role in the project planning and development system construction for the civil aircraft landing gear system development unit.

    参考文献
    相似文献
    引证文献
引用本文

冯全磊,冯广,周笛.民机起落架系统研制适航工作分析[J].民用飞机设计与研 究,2020(3):115-120FENG Quanlei, FENG Guang, ZHOU Di.[J]. Civil Aircraft Design and Research,2020,(3):115-120. ( in Chinese)

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2020-10-15
  • 出版日期:

微信公众号二维码

手机版网站二维码

我要投稿 投稿指南 联系我们 二维码
TOP