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1)  control surface
舵面
1.
A new design concept of flexible lamella "hinge" for unmanned aerial vehicle( UAV) control surface is presented.
针对小型无人机操纵舵面的特点,利用玻璃钢复合材料比强度高、柔韧性良好的特性,提出了“薄片”式狭长矩形玻璃钢复合材料迭层板舵面柔性铰链片的设计概念。
2.
A new concept of a flexible lamellate hinge for UAV (Unmanned Aerial Vehicle) control surfaces is presented.
针对小型无人机的特点,研究发展了一种提高无人机舵面效率的设计概念,即采用柔韧特性良好的复合材料片状结构——舵面柔性铰链片来执行舵面铰链功能,通过铰链片的柱状弯曲来实现舵面的偏转。
2)  Rudder [英]['rʌdə(r)]  [美]['rʌdɚ]
舵面
1.
Designing and modeling analysis of an aeroelastic experimental system for rudder model in transonic flows;
舵面跨声速气动弹性特性实验装置设计与分析
2.
For the characteristic of Supersonic Missile\'s low aspect-ratio of the rudder of,ignoring the mode changes in inflect direction,resonance and coupling flutter will happen when nonlinear factor with clearance is considered in rolling direction of the rudder.
针对一类超声速导弹小展弦比舵面的特点,忽略其弯曲方向的模态变化,当舵机/舵面系统旋转方向引入间隙非线性因素时,会使系统产生谐振和耦合颤振问题[1],因此,首先建立了舵机/舵面系统在模态试验和飞行状态下的单自由度非线性振动模型,通过渐近法求解这一自由度下间隙对系统的影响,以及预载和飞行速度抑制间隙的变化规律,为避免系统发生抖动和结构耦合颤振提供分析依据。
3.
The Application of Sub-Critical Technology in Wind-Tunnel Flutter Experiment for Rudder Model;
为降低模型和风洞设备的损坏率 ,用随机激励和频响函数分析法 ,测定进入颤振临界点之前舵面颤振试验模型在不同风洞气流动压下的模态频率和阻尼比 ,由阻尼外推法或稳定参数法确定颤振临界动压。
3)  fin [英][fɪn]  [美][fɪn]
舵面
1.
The combination control, an important and reasonable solution for flight control and including jet thrust and aerodynamic force and momentum by fins, have been successfully applied to aerospace vehicles.
其中最复杂情况为发动机喷流推力与舵面空气动力共同使用所形成的复合控制。
4)  retractile control surfaces
伸缩舵面
1.
In this paper,a new kind of maneuvering warhead aerodynamic configuration with the use of two retractile control surfaces is proposed,which could keep those problems away from maneuvering warhead design pro.
本文提出了一种新型伸缩舵面机动弹头气动布局设计新理念,避免了普通全动舵面布局方案中舵轴设计面临的严峻的热环境和力环境等问题,而且还可以只通过这两片舵面实现对弹头的姿态和升力大小及方向的控制,从而实现对弹道的三维控制,是一种很有前途的机动弹头布局新思路。
2.
A new kind of maneuvering warhead aerodynamic configuration with the use of two retractile control surfaces was proposed,which avoided such severely aerothermodynamic environment in reentry flying like traditional maneuvering warhead configuration.
提出了一种伸缩舵面机动弹头气动布局设计的新理念,避免了普通全动舵面布局方案中舵轴设计面临的严峻热环境和力环境等问题。
5)  Failure of rudder plane
舵面故障
6)  rudder area
舵面积
1.
Sections on rudder equipment in 《CSR for Bulk Carriers》(2006),such as rudder area,calculation model of underhung rudder with rudder trunk,prestress on conic surface of conical connector allowed stress and intensity checking of semi-balanced rudder etc.
对《散装货船共同结构规范》(2006)舵设备部分有关舵面积,有舵杆筒悬挂舵的计算模型,锥形连接器的锥面预加压力及其许用压力以及半平衡舵强度校核等提出了作者的看法,望能获得IACS和船级社的关注。
补充资料:不看金面看佛面
1.同"不看僧面看佛面"。
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
参考词条