您当前的位置:
首页 >
文章列表页 >
TLD simulation analysis with multiple faults for FADEC system ,under full repair policy
更新时间:2026-07-07
    • TLD simulation analysis with multiple faults for FADEC system ,under full repair policy

    • Vol. 35, Issue 4, Pages: 823-831(2020)
    • DOI:10.13224/j.cnki.jasp.2020.04.016    

      CLC:
    • Published:2020

    移动端阅览

  • doi: 10.13224/j.cnki.jasp.2020.04.016 DOI:

  •  
  •  
icon
试读结束,您可以激活您的VIP账号继续阅读。
去激活 >
icon
试读结束,您可以通过登录账户,到个人中心,购买VIP会员阅读全文。
已是VIP会员?
去登录 >

0

Views

414

下载量

0

CSCD

Alert me when the article has been cited
提交
Tools
Download
Export Citation
Share
Add to favorites
Add to my album

Related Articles

Life cycle probabilistic modeling and simulation of aero⁃engine maintenance
Algorithm of “turning square into circle” for valve hole
Aero-engine power control based on life consumption of ligh pressure turbine blade
Identification of multiple faults of the aircraft engine digital control system
基于自适应MOMEDA滚动轴承故障特征提取方法

Related Author

Jianzhong SUN
Yang YI
Hong WEN
Peng WANG
Chuanjin SHAO
SU Zhishan
LI Huacong
LIU Bao-hua

Related Institution

College of Civil Aviation,Nanjing University of Aeronautics and Astronautics
Training Center, China Eastern Airlines Jiangsu Limited
Commercial Aircraft Engine Company Limited,Aero Engine Corporation of China
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
Aviation Motor Control System Institute, Aviation Industry Corporation of China
0