发明授权
US08634972B2 Method and system for integrating engine control and flight control system
有权
整合发动机控制和飞行控制系统的方法和系统
- 专利标题: Method and system for integrating engine control and flight control system
- 专利标题(中): 整合发动机控制和飞行控制系统的方法和系统
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申请号: US13221102申请日: 2011-08-30
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公开(公告)号: US08634972B2公开(公告)日: 2014-01-21
- 发明人: Harry Kirk Mathews, Jr. , Sridhar Adibhatla , Jeffrey Russell Bult
- 申请人: Harry Kirk Mathews, Jr. , Sridhar Adibhatla , Jeffrey Russell Bult
- 申请人地址: US NY Niskayuna
- 专利权人: General Electric Company
- 当前专利权人: General Electric Company
- 当前专利权人地址: US NY Niskayuna
- 代理商 John P. Darling
- 主分类号: G01C23/00
- IPC分类号: G01C23/00
摘要:
A method and system of operating an aircraft system are provided. The aircraft system includes an integrated aircraft flight control system that includes an engine control system configured to generate engine performance and health information. The integrated aircraft flight control system also includes a flight control system configured to generate flight information and trajectory intent information. The integrated aircraft flight control system further includes a communications channel communicatively coupled between the engine control system and the flight control system, where the engine control system is configured to transmit the generated engine performance and health information to the flight control system using the communications channel and the flight control system is configured to transmit the generated flight information and trajectory intent information to the engine control system using the communications channel.
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