飞机尾部的水平稳定器和升降舵。
The horizontal stabilizer and elevator in the tail assembly of an aircraft.
飞机的升降舵可以使它升降自如。
速度快的飞机很少采用平衡升降舵。
平尾上的升降舵控制俯仰。
这架直升飞机失事的主要原因是升降舵失灵。
The main reason that caused the accident of this plane was a malfunction of the elevator.
升降舵稍微向前倾斜，增加了机尾向下的载荷。
The elevator, tilted upward-slightly, increases the down-load, in the tail.
我们遭到雷击，后机身被打坏，失去右升降舵。
We have been struck by lightning, the rear fuselage damaged, right elevator lost.
如果扳动机尾处的升降舵，就会减速，但能保持住高度。
To move what he calls the elevators in the tail. You'll lose speed, but keep altitude.
最后，针对某型飞机升降舵操纵机构进行了应用研究。
At last, the software scheme of the mechanism reliability simulation is defined, and a case of an elevator control mechanism is presented.
它生产的电梯和功能既是一种俯仰升降舵和方向舵偏转。
It produces lift and functions as both a pitch elevator and yaw rudder.
升降舵的根梢比通常较小，因而两个值之间的差别一般不大。
The taper of elevators is usually slight, and the difference between the two values is generally small.
升降舵操纵系统故障，轻微抖动，我们在五边保持稍大进场速度。
We have trouble with elevator control, it is fluttering (sharking) slightly, we 're to keep higher approach speed on final.
升降舵操纵系统故障，轻微抖动，我们在五边保持稍大进场速度。
We have trouble with elevator control , it is fluttering ( sharking ) slightly , we ' re to keep higher approach speed on final.
随动补偿片，铰接在操纵面后缘(副翼，方向舵，升降舵)的可动部。
BALANCE TAB, a small hinged moveable part on the trailing edge of a control surface (aileron, elevator, rudder).
升降舵一个可动控制台，通常安装在飞机的尾翼上，用来操纵飞机。
A movable control surface, usually attached to the horizontal stabilizer of an aircraft, that is used to produce motion up or down.
移动升降舵离开它们的流线型位置，使得飞机改变水平轴上的俯仰姿态。
Moving the elevators out of their faired position causes the airplane to change the pitch attitude about the lateral axis.
水平和垂直安定面、驾驶舱门、方向舵以及升降舵组件目前正在组装和安装。
The assembly and installation of the vertical and horizontal stabilizers, cabin door, rudder and elevator assemblies are being concluded.
分析潜艇空间运动典型的操纵方式和运动特性及尾升降舵卡故障和挽回方式。
This paper analyzes the typical control styles and the motion characters of submarine′s space motion.
管理与A350升降舵相关的文件，包括图纸，工艺，切割原材料工艺以及质量报告。
Manage documentation related with A350 Elevator, included composite drawings, composite process, cutting raw material process and quality reports.
对于任意一个重心位置，平衡速度由它的初始值变化到较大的值时要求升降舵向下偏转。
For any C. G. position, an increase in trim speed from any initial value to a larger one requires a downward deflection of the elevator.
辅助操纵系统由升降舵调整片、副翼调整片、副翼随动补偿调整片和方向舵补偿调整片组成。
Assisted by the elevator control system to adjust on-chip, chip aileron adjustment, moving with the aileron and rudder-chip compensation adjustment compensation adjustment film composition.
升降舵，铰连在水平安定面后缘上的可动部件。用以操纵飞机的俯仰运动(机头朝上及朝下)。
ELEVATOR, a hinged moveable part on the trailing edge of the horizontal stabilizer for airplane pitch (nose up and nose down) control.
飞行器以发泡聚丙烯为主体，在其背部与两个升降舵补助翼（可以操控的界面）上有一个电动机。
The flying robots were built out of expanded polypropylene with a single motor at the rear and two elevons (control surfaces that enable steering).
针对此翼面上有升降舵的多舵面布局，建立了俯仰运动下不同于翼面上只有副翼的动力学模型。
About multi - control surface configuration with elevators, its dynamic model was established under pitch movement, differing from wing with ailerons alone.
对于前轮转弯系统，脚踏板传感器组件通过升降舵副翼计算机向刹车和转弯控制组件发送信号。
The pedal transducer units send data to the BSCU via the ELACs for the nosewheel steering system.
并且，局部搜索引入序列二次规划策略（SQP），分步求解出升降舵偏角，油门设置与迎角初始值。
Furthermore, sequential quadratic programming (SQP) is introduced so as to accelerate the local optimum. Attacking angle, elevator deflection and throttle setting are obtained by steps.
在适配值集合内，随着弹射能量的增加，升降舵预置偏角的适配范围增大，前起落架突伸力的影响减小。
Within the boundary of the match value set, as the catapult energy increases, the match range of the presetting elevator angle enlarges and the influence of the nose gear fast-extension weakens.
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。)
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。)
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).
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