aileron

英 [ˈeɪlərɒn] 美 [ˈeɪlərɑːn]

n.  (飞机的)副翼

复数:ailerons

机械

BNC.29585 / COCA.33779



牛津词典

noun

  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

    柯林斯词典

    1. (飞机的)副翼
      An aileron is a section on the back edge of the wing of an aircraft that can be raised or lowered in order to control the aircraft's movement.

      双语例句

      1. I knocked my head on the doorpost and hurt it.
        我的头撞在门柱上,碰破了。
      2. Airframe and powerplant Aileron control and reconfiguration of flying wing aircraft
        飞行器构架和动力装置飞翼布局飞行器副翼性能及重构分析
      3. Strut-and-tie model reinforcement of the external prestressed box-beam anchor block Aileron servo pull rod should be vertical to the shaft of aileron basically.
        体外预应力箱梁锚固块拉压杆模型法配筋副翼舵机拉杆应基本上垂直于副翼转动轴线。
      4. Aileron control actuator leaked fluid.
        副翼操纵作动筒漏油。
      5. Lift is lost on the wing where the aileron is raised, but it increases on the side where the lowered aileron increases the camber of the wing.
        副翼扬起的时候机翼的胜利就会减小,但是副翼降下的一边会增加机翼的弯曲度。
      6. Aileron control and reconfiguration of flying wing aircraft A Kind of Composite Rotor Structural Optimization Design Model
        飞翼布局飞行器副翼性能及重构分析一种复合材料旋翼结构优化设计模型
      7. It has plenty of aileron deflection and will rotate quite quickly in both directions while hovering.
        飞机的副翼有很大的行程,所以飞机在悬停时,向左向右的滚转都很容易。
      8. When one row on one side blows air at a higher pressure than the other it causes the airflow over the trailing edge on that side to bend up or down, in exactly the way that an aileron would, and the plane rolls accordingly.
        当一侧机翼上的一排狭槽喷出的空气压力大于另一排,就导致了掠过机翼后缘的气流偏向上方或偏向下方,与副翼的作用完全相同,飞机随之上升或下降。
      9. Modeling analysis of friction stimulating vibration for rudderpost and bearing framework of shipping Aileron servo pull rod should be vertical to the shaft of aileron basically.
        船舶舵轴及轴承结构摩擦激振建模研究副翼舵机拉杆应基本上垂直于副翼转动轴线。
      10. Positive aileron deflection produces an anti-clockwise moment about the X axis. Aileron servo pull rod should be vertical to the shaft of aileron basically.
        正的副翼偏转角产生绕X轴的负方向力矩。副翼舵机拉杆应基本上垂直于副翼转动轴线。
      11. Analysis on Dutch Roll Modal of Unmanned Aerial Vehicle with the Limited Deadlocking of Single Aileron
        无人机单副翼有限卡死时荷兰滚运动分析
      12. Alignment of rudder blade and rudder stock on Aileron servo pull rod should be vertical to the shaft of aileron basically.
        舵叶与舵杆平台找正副翼舵机拉杆应基本上垂直于副翼转动轴线。
      13. Note: If the flight crew inadvertently activates aileron trim while an autopilot is engaged, the repositioning of the aileron neutral point is not apparent to the crew.
        注:在自动驾驶接通的情况下,如果飞行机组无意中触动了副翼配平,新调定的副翼中立点对机组来说并没有明显的反映。
      14. Finally the negative feedback effect of the aileron operation on the control parameters in the stable region is studied.
        最后研究了副翼操纵反馈设计对操纵参数稳定域的影响。
      15. This paper aims at the research of aerodynamic characteristic of two dimensional aileron by solving N-S equation, based on the structured grid and Baldwin-Lomax turbulent model.
        为开展三维舵面绕流的NS方程数值模拟和铰链力矩数值计算研究奠定了基础。
      16. You still have control over elevator and aileron but it can't be over controlled.
        你还可以控制电梯和副翼但不能超过控制。
      17. Aileron servo pull rod should be vertical to the shaft of aileron basically. In the pilot house, Dwyer was already fighting the wheel.
        副翼舵机拉杆应基本上垂直于副翼转动轴线。在驾驶室里,德怀尔已经跟舵轮较上劲了。
      18. Usually only a small amount of rudder is needed, especially if a large amount of differential ( more up aileron motion than down motion) is present.
        通常只需要少量的方向舵,尤其是出现大量差速时(上副翼动作多于下副翼动作)。
      19. I've also carved one aileron and the fin fairing
        我也刻一个副翼和鳍整流罩
      20. I read him checklists, learning words like "aileron,"" magnetos," and" pitot "that no one else in my first-grade class knew.
        我给他念设备清单,学会了很多其他一年级学生都不认识的词,像“副翼”、“磁发电机”和“空速管”。
      21. Due to the influence of the elastic deformation of flexible structures, the efficiency drops constantly with the increase of the dynamic pressure, which even causes aileron reversal.
        受到结构弹性变形的影响,随着飞行动压的增加,舵面的操纵效率不断下降,副翼甚至会出现操纵反效现象;
      22. The paper also describes a ground demonstration of a one channel primary flight control system and a flight demonstration of an aileron trim control system.
        同时还介绍了一单通道主飞控系统的地面演示和一副翼配平控制系统的飞行演示。
      23. The method may be applied to differential aileron as well as plain aileron.
        方法适用于简单副翼和差动副翼。
      24. As a result of applying this method, simple and optimal control laws have successfully been developed for the active suppression of wing bending-torsion flutter and under-ballanced aileron flutter using a single trailing-edge active control tab.
        运用这种方法获得用单独后缘主控调整片抑颤的优化控制律,实现了对质量不平衡舵面颤振和翼面弯扭颤振的有效抑制。
      25. Effect of external stores and aileron control stiffness on flutter characteristics of wing
        外挂物、副翼操纵刚度对机翼颤振特性的影响
      26. The simulation study of the static test of composite aileron is carried out.
        对复合材料副翼静力试验进行仿真研究。
      27. A non-contact calibration method for angular displacement sensor of aileron, flap, rudder and elevator for vehicle based on computer monocular vision is proposed.
        提出一种基于计算机单目视觉的飞行器副翼、襟翼、方向舵和升降舵角位移传感器的非接触标定方法。
      28. Numerical simulations are included to verify its control performance. Secondly, considering the main and aileron rotor flapping dynamics, an adaptive attitude and altitude controller is designed using the backstepping method.
        仿真结果也表明该分层控制器具有良好的控制性能。第二,在考虑了主旋翼和副翼挥舞动态模型的基础上,应用反步法设计了自适应姿态与高度控制器。
      29. The aileron case analysis shows that the model can meet the resource access control requirements. ( 2) For the problem of evaluating the collaborative design progress in the workflow process, an evaluation method of design maturity is presented.
        经副翼的案例分析表明,该模型能较好的实现对资源的访问控制要求。(2)针对工作流运行过程中需要评估协同设计工作进度的问题,给出了一种设计成熟度的评估方法。
      30. When the rudder is the uncontrollable surface, a method which designs the aileron channel control law only is proposed to make the UAV step out the spiral motion.
        当方向舵面为不可控舵面时,提出了仅通过设计副翼通道的控制律使无人机步出螺旋运动的方法。

      英英释义

      noun

      1. an airfoil that controls lateral motion