发明名称 SYSTEM AND METHOD FOR IMPROVED LOW AIRSPEED WARNING
摘要 A method and system are provided for generating a low airspeed warning in an aircraft. This method creates a scale factor that is a factor of engine thrust and aircraft altitude. A low airspeed threshold is determined that varies according to the aircraft altitude with respect to a predetermined altitude band and the engine thrust with respect to a predetermined engine thrust band. A low airspeed alert is generated in response to the determination of the low airspeed threshold. This method provides a pilot with earlier knowledge of low airspeed conditions when the aircraft is in a target altitude band, increasing the pilot's response time and thereby enhancing overall aircraft safety.
申请公布号 US2015314884(A1) 申请公布日期 2015.11.05
申请号 US201414265723 申请日期 2014.04.30
申请人 HONEYWELL INTERNATIONAL INC. 发明人 Johnson Steve;Ishihara Yasuo;Bateman Charles Donald
分类号 B64D45/00 主分类号 B64D45/00
代理机构 代理人
主权项 1. A method for generating a low airspeed warning in an aircraft, the method comprising: receiving engine thrust data; receiving altitude data; determining, in a processor, a low airspeed threshold that is a function of engine thrust when the aircraft altitude is within a predetermined altitude band; and generating a low airspeed alert in response to the step of determining.
地址 Morristown NJ US