一种飞机升降舵需用功率的计算方法  

A Calculation Method of Required Power for Aircraft Elevator

作　　者：杨宝钧 巩磊 YANG Baojun;GONG Lei(Flight Control System Design Institute,AVIC Xi’an Aircraft Design Institute,Xi’an,710089,China)

机构地区：[1]航空工业西安飞机设计研究所飞控系统设计研究所,西安710089

出　　处：《南京航空航天大学学报》2018年第6期802-806,共5页Journal of Nanjing University of Aeronautics & Astronautics

摘　　要：为提供舵面需用功率的计算依据,对工程作动器的设计提供理论支撑,提出了一种飞机升降舵需用功率的计算方法,通过不同类型飞机实例进行计算。首先,针对不同种类的工况进行阐释,并详述速率计算所用的评价准则;然后,提出带载荷平均速率计算方法步骤,分析铰链力矩特性;最后,通过计算空载速率,分析舵面需用功率,并进行计算分析。计算结果表明,该方法计算出的需用功率不仅保证稳定裕度,且与舵面载荷具有理论相关性,设计结果安全合理,对工程设计具有实用指导意义。In order to provide the calculation basis of the required power of the rudder surface,theoretical support is provided for the design of the engineering actuator,and a calculation method for the power required by the aircraft elevator is proposed,which is calculated by different types of aircraft examples.First,we explain the different kinds of working conditions,and elaborate the evaluation criteria used for rate calculation.Then,the calculation method of the average rate of load is proposed to analyze the characteristics of the hinge torque.Finally,the calculation of the no-load rate is used to analyze the rudder surface.The calculation results show that the required power calculated by this method not only guarantees the stability margin,but also has theoretical correlation with the rudder surface load.The design results are safe and reasonable,and have practical guiding significance for engineering design.

关 键 词：升降舵需用功率 工况 平均速率 铰链力矩 舵面载荷 

分 类 号：V249[航空宇航科学与技术—飞行器设计]