Test and analysis on load bearing capability of hinge lug of aircraft horizontal stabilizer elevator 飞机平尾升降舵接头耳片承载能力分析与试验
Horizontal or lateral axis, passes through the airplane from one side to the other-nose up and nose down control is by elevators ( and stabilizer for trim). 从飞机一侧通向另一侧的水平轴或横轴。升降舵控制机头绕此轴作上下的运动。(水平安定面则用以配平。)
A short, winglike control surface projecting from the fuselage of an aircraft, such as a space shuttle, mounted forward of the main wing and serving as a horizontal stabilizer. 鸭式飞机的水平安定面和升降舵:从一架飞行器伸出的一个短的翼状控制平面,如航天飞船的机身,被安在飞机翼前方,作为水平稳定器。
Taking a certain model of the helicopter as an example, a method for selecting the aerodynamic shape of a fuselage, the parameters and locations of a horizontal stabilizer and a tail rotor in the preliminary design is presented. 通过对某型号直升机气动布局设计,介绍了在直升机总体设计中选择直升机气动外形、平尾和尾桨的参数及位置的一些基本方法。
The method is used in a hinge wear inspection example of Horizontal stabilizer to testify its efficiency. 以水平安定面铰链磨损检查的转化和简化工作为例,说明了方法的有效性。
This peper is based on the wind tunnel experiment data and studies the air dynamic performance of fuselage, horizontal stabilizer and fin under level wind in any direction. 本文以风洞试验数据为依据,对在任意方向水平作用下的机身、垂尾和尾桨气动特性进行了研究。
The Optimum Transfer Function Method in the Design Tanker's Horizontal Stabilizer 设计坦克水平向稳定器的最优传递函数法
This paper introduces such contents as the design of horizontal stabilizer, engine inlet and the medthod of solving tail shake for a helicopter. 本文介绍了直升机平尾设计、发动机进气道设计以及解决尾部抖动的方法等问题。
Sliding mode variable structure control is applied to design horizontal stabilizer for tanks. 介绍了用滑动模态变结构控制对坦克水平稳定器进行设计的方法。
LQG/ LTR is used to design tank horizontal stabilizer, to solve the unstable phenomenon of LQG controller under random disturbance. System simulation shows, that LQG/ LTR controller has good robustness. 应用LQG/LTR控制方法设计坦克水平向稳定器,以解决在随机干扰作用下坦克稳定器LQG控制器可能出现的不稳定现象,系统仿真表明,应用了LTR过程的LQG控制器具有很好的鲁棒性。
The horizontal stabilizer actuator is one of the key components of an aircraft, whose fatigue failure directly affects the security in aviation, so it has important practical significance to carry out the research about improving structural fatigue life and reliability. 大型飞机水平安定面作动器是飞机的关键部件之一,其疲劳失效直接影响到飞机的安全飞行,因此开展长寿命、高可靠性设计技术的研究具有重要的现实意义。
We established rear suspension system, steering system, tire system, horizontal stabilizer bar and body system to be assembled to get the vehicle dynamics model of the car. 建立了后悬架系统、转向系统、轮胎系统、横向稳定杆、车身系统等子系统进行装配得到该车的整车动力学模型。