用于控制起飞推力的系统和方法
用于控制起飞推力的系统和方法
本披露提供了用于控制飞行器(100)的至少一个发动机(114，116)在起飞时所产生的推力的系统和方法。接收(202)至少一个输入信号，所述至少一个输入信号包括指示所述飞行器的速度的输入数据。将所述飞行器的速度与第一预定阈值进行对比。响应于确定所述速度低于所述第一阈值，根据所述输入数据确定(204)所述至少一个发动机的推力极限，并向所述至少一个发动机输出推力限制信号，以用于根据所述推力极限来限制(210)所述推力。
The present disclosure provides systems and methods for controlling thrust produced at takeoff by at least one engine (114, 116) of an aircraft (100). At least one input signal comprising input data indicative of a speed of the aircraft is received (202). The speed of the aircraft is compared to a first pre-determined threshold. Responsive to determining that the speed is below the first threshold, a thrust limit for the at least one engine is determined (204) from the input data and output to the at least one engine a thrust limitation signal for causing the thrust to be limited according to the thrust limit (210).
Dokumentinformationen
用于控制起飞推力的系统和方法
2023-07-21
Patent
Elektronische Ressource
Chinesisch