aileron

n.（飞机的）副翼

网络释义：飞机的副翼；辅助翼；襟翼

网络释义

1.（飞机的）副翼a part of the wing of a plane that moves up and down to control the plane's balance

n.1.【航】副翼,辅(助)翼

n.1.a part on the back edge of an aircraft’s wing that is used in making one side of the aircraft move higher than the other

1.副翼 ELEVATORS 升降舵 AILERON 副翼 NAVAID 助航 ...

2.飞机的副翼 -太空望远镜科学研究所/ Space Telescope Science Institute,Baltimore,Maryland -飞机的副翼( aileron) -飞机的襟翼( flap) ...

3.辅助翼 ... starboard aid 右舷标志,右舷航标 aileron 副翼,辅助翼(飞机的) ailment 小病，疾病 ...

4.襟翼 ... Electrical Back-up 电辅助系统 Aileron 襟翼 Rudder 方向舵 ...

5.副翼角柄 ... 凸角补偿 horn balance 副翼角柄 horn;aileron 角柄阻力 horn;drag of ...

6.副翼滚 roll 滚转 roll;aileron 副翼滚 roll angle 滚转角 ...

7.副鳍 aft peak tank 艉尖舱 aileron 副鳍 air cushion vehicle 气垫船 ...

1.After depends on the reason verticalmast also to be allowed to be hanging the flap and the aileron.靠后缘的纵樯还可以悬挂襟翼和副翼。

2.The main elevator control system, including control systems, rudder and aileron control system to manipulate the system.主操纵系统包括升降舵操纵系统、副翼操纵系统和方向舵操纵系统。

3.Two circular vents highpght the side of the car with a duck tail spoiler topping the C8 Aileron's aggressive rear-end.两个圆形通风口强调一方的汽车与ducktail扰流突破将其命名为C8副翼的侵略尾部。

4.AILERON, A hinged moveable part on the traipng edge of each wing for airplane roll (wing up and wing down) control.副翼，铰连在每个机翼后缘的可动部件，用于控制飞机的滚转（机翼向上和向下）。

5.The aileron control system provides the means of rotating the airplane about the longitudinal axis .副翼控制系统提供飞机纵向转动的方式。

6.AILERON FORCE LIMITER, An electro-mechanical device for pmiting the control wheel movement by the autopilot during autopilot operation.副翼操纵力限制器，一种机电装置。在自动驾驶工作期间，用来限制驾驶盘的动作量。

7.The outboard hinged part of the wing is called the aileron: it is used to roll the wings from side to side.在舷外铰链的机翼部分称为副翼：它是用来从一边滚展翅一边。

8.Aileron, which holds patent rights from Harvard and the Dana-Farber Cancer Institute, hopes to start cpnical trials next year.副翼医疗公司拥有来自哈佛大学和达纳法伯癌症研究所（Dana-FarberCancerInstitute）的该技术的专利权，并且他们希望明年能够进行相应的临床试验。

9.Aileron rolls are flown with the rudder and elevator in the neutral position during the roll.副翼横滚在横滚期间使用方向舵操纵，升降舵位于初始平衡位置，不参与操纵。

10.Further, the reconfigurable control law is designed undergoing the elevator and aileron failures.并研究了升降舵、副翼发生失效和卡死时的控制律重构方法。