发明名称 METHOD AND SYSTEM FOR INTEGRATING ENGINE CONTROL AND FLIGHT CONTROL SYSTEM
摘要 <p>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.</p>
申请公布号 CA2787579(A1) 申请公布日期 2013.02.28
申请号 CA20122787579 申请日期 2012.08.23
申请人 GENERAL ELECTRIC COMPANY 发明人 MATHEWS, HARRY KIRK, JR;ADIBHATLA, SRIDHAR;BULT, JEFFREY RUSSELL
分类号 B64C19/00;B64C19/02 主分类号 B64C19/00
代理机构 代理人
主权项
地址