Hybrid engine accessory power system
    1.
    发明申请
    Hybrid engine accessory power system 有权
    混合动力发动机附件动力系统

    公开(公告)号:US20050103931A1

    公开(公告)日:2005-05-19

    申请号:US10694645

    申请日:2003-10-27

    摘要: A system for generating accessory power from a gas turbine engine is provided by the present invention. The system includes an electronic control device for monitoring at least one parameter which provides information about an incipient change in power demand, a control valve operated by the control device for supplying bleed air from the engine during a transient state in response to the at least one monitored parameter, and a pneumatically operated device for receiving the bleed air and for generating power to operate equipment onboard an aircraft. The pneumatically operated device may be an air turbine or a pneumatically integrated generator.

    摘要翻译: 本发明提供一种用于从燃气涡轮发动机产生辅助动力的系统。 该系统包括用于监测至少一个参数的电子控制装置,所述参数提供有关电力需求的初期变化的信息;控制装置,用于在过渡状态期间响应于所述至少一个 监控参数,以及用于接收放气并用于发电以操作飞机上的设备的气动操作装置。 气动装置可以是空气涡轮或气动一体化的发电机。