Aircraft engine control system

更新时间:2023-05-18 06:47:18 阅读: 评论:0

倒走专利名称:Aircraft engine control system
质保承诺书发明人:ZACCARIA, PATRICK,OSTERMANN, PATRICE 申请号:EP99400017.2
申请日:19990106
公开号:EP0933294B1
公开日:
葡萄牙人
台风命名20030730
专利内容由知识产权出版社提供
古城荆州
摘要:The system us engine power laws for application to subquent similar aircraft. The system (2,22) provides control of the engine of a first aircraft (1) which forms part of a family of aircraft, the first aircraft having the greatest maximum mass of the aircraft in question. For each engine of the first aircraft a power law is determined which is specific to this engine and aircraft during the takeoff pha (T). A cond power law is determined for the subquent pha of flight (R) after takeoff. A detection signal is produced when the aircraft moves from the takeoff pha to the subquent flight pha and the appropriate power law is applied. The signals may be processing either by a computer processing technique, or by an electronic circuit processor.
申请人:AIRBUS FRANCE,AIRBUS FRANCE,AIRBUS FRANCE生蚝做法
地址:FR
面具图片绘画国籍:FR
代理机构:Bonnetat, Christian
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