CN103407576B - 触发发动机备份控制模式的方法及发动机备份控制系统 - Google Patents
触发发动机备份控制模式的方法及发动机备份控制系统 Download PDFInfo
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- CN103407576B CN103407576B CN201310213737.7A CN201310213737A CN103407576B CN 103407576 B CN103407576 B CN 103407576B CN 201310213737 A CN201310213737 A CN 201310213737A CN 103407576 B CN103407576 B CN 103407576B
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CN201310213737.7A CN103407576B (zh) | 2013-05-31 | 2013-05-31 | 触发发动机备份控制模式的方法及发动机备份控制系统 |
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CN201310213737.7A CN103407576B (zh) | 2013-05-31 | 2013-05-31 | 触发发动机备份控制模式的方法及发动机备份控制系统 |
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CN103407576A CN103407576A (zh) | 2013-11-27 |
CN103407576B true CN103407576B (zh) | 2015-07-08 |
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Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
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FR3076387B1 (fr) * | 2018-01-04 | 2020-01-24 | Airbus Operations | Procede et systeme d'aide a la gestion de listes de commandes sur un aeronef. |
US11188075B2 (en) * | 2018-08-02 | 2021-11-30 | Qualcomm Incorporated | Controlling a robotic vehicle following flight controller signal loss |
GB2615072A (en) * | 2022-01-24 | 2023-08-02 | Airbus Operations Ltd | An aircraft control system |
CN114687865B (zh) * | 2022-02-25 | 2023-10-31 | 中国航发控制系统研究所 | 一种fadec控制软件的状态机跟随方法 |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
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US5893040A (en) * | 1996-05-15 | 1999-04-06 | The Boeing Company | Method and apparatus for automatically providing jet engine thrust ratings to avionic systems |
US6224021B1 (en) * | 1998-03-10 | 2001-05-01 | Toyota Jidosha Kabushiki Kaisha | Thrust control apparatus and method for an airplane |
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FR2934065B1 (fr) * | 2008-07-17 | 2010-08-27 | Airbus France | Dispositif pour la determination de la position d'une manette des gaz dans un aeronef |
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Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
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US5893040A (en) * | 1996-05-15 | 1999-04-06 | The Boeing Company | Method and apparatus for automatically providing jet engine thrust ratings to avionic systems |
US6224021B1 (en) * | 1998-03-10 | 2001-05-01 | Toyota Jidosha Kabushiki Kaisha | Thrust control apparatus and method for an airplane |
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CP02 | Change in the address of a patent holder |
Address after: No.25, Zhangyang Road, China (Shanghai) pilot Free Trade Zone, Pudong New Area, Shanghai, 201210 Patentee after: COMMERCIAL AIRCRAFT CORPORATION OF CHINA, Ltd. Patentee after: COMMERCIAL AIRCRAFT CORPORATION OF CHINA, LTD SHANGHAI AIRCRAFT DESIGN AND Research Institute Address before: No.25 Zhangyang Road, Pudong New Area, Shanghai 201210 Patentee before: COMMERCIAL AIRCRAFT CORPORATION OF CHINA, Ltd. Patentee before: COMMERCIAL AIRCRAFT CORPORATION OF CHINA, LTD SHANGHAI AIRCRAFT DESIGN AND Research Institute |
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Effective date of registration: 20220923 Address after: No.25, Zhangyang Road, China (Shanghai) pilot Free Trade Zone, Pudong New Area, Shanghai, 201210 Patentee after: COMMERCIAL AIRCRAFT CORPORATION OF CHINA, Ltd. Patentee after: Shanghai Aircraft Design Research Institute Co.,Ltd. Address before: No.25, Zhangyang Road, China (Shanghai) pilot Free Trade Zone, Pudong New Area, Shanghai, 201210 Patentee before: COMMERCIAL AIRCRAFT CORPORATION OF CHINA, Ltd. Patentee before: COMMERCIAL AIRCRAFT CORPORATION OF CHINA, LTD SHANGHAI AIRCRAFT DESIGN AND Research Institute |
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TR01 | Transfer of patent right |