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 |