试验结果表明，机翼结构的设计满足了设计要求。
The results of the experiment show that the design of the wing structure satisfies the design requirements.
应用该结构模型可以很好的模拟机翼结构的实际情况。
With use of this structure model, we can simulate the real performance of aerofoil very well.
本玩具直升飞机机翼结构较好的解决了玩具 直升飞机平稳飞行问题。
The wing structure of the toy helicopter better solves the problem of stable flying of the toy helicopter.
每个主起落架支柱具有一部双机轮组件，主起落架支柱安装在机翼结构中。
The MLG legs, each with a twin-wheel assembly, are installed in the wings.
为机翼结构的可靠性分析和损伤容限设计提供了比较有价值的力学分析手段。
A good mechanics analysis approach was presented for reliability analysis and damage tolerance design of aerofoil structure.
如果该载荷重心在机翼结构弹性轴之后，则引起主机翼表面前端向下的扭转。
If this load centroid is behind the elastic axis of the wing structure, then a nose-down twist of the main wing surface results.
翼盒为机翼主要承力部件，优化潜力较大，是机翼结构优化设计的重点对象。
As the main load-bearing structure, wing box is one of the main optimization objects which has great potential of weight reduction.
整体油箱，由机翼结构件梁、肋、蒙皮组成，用来在飞机上储存燃油的金属容器。
INTEGRAL TANK, a metal container formed by the wing structure (spars, ribs, skin) for storage of fuel on the airplane.
这种细长梁由质轻但坚韧的碳纤维复合材料制成，负责承载引擎、起落架和机翼结构。
The long, slender beams that carry engines, landing gear and wing structure are made from light but tough carbon-fibre composites.
研究表明，开发知识驱动的设计工具，是解决机翼结构布局设计问题的一条可行途径。
The study shows that developing knowledge-driven design tools should be a feasible approach to the wing structural layout problem.
将等效板模型推广应用到典型机翼结构的静力学、动力学以及静、动气动弹性分析中。
Some typical numerical results are presented from application of the model to static analysis, dynamic analysis, static aeroelasticity and flutter analysis of a wing-box and a wing.
将等效板模型推广应用到典型机翼结构的静力学、动力学以及静、动气动弹性分析中。
Some typical numerical results are presented from application of the model to the static analysis, dynamic analysis, static aeroelasticity and flutter analysis of a wing-box and a wing.
飞机机翼挂装翼尖导弹对机翼结构设计和结构分析提出了诸多全新课题，如结构的振动响应和气动弹性动响应。
Missile carrying on the wing tip causes the wing structure design and analysis to face many challenges, such as structural vibration response and aeroelastic response.
GE也提供GEnx引擎、固定和移动的机翼结构，作为起落架促进作用和通用中心系统直接提供给波音公司的787项目。
Ge also supplies the GEnx engine, fixed and moveable wing structures as well, as landing gear actuation and the common core system direct to Boeing for the 787 program.
正像翼间支柱是机翼结构中不可缺少的一部分一样，Strut也可能成为您下一个Web项目的不可缺少的一部分。
Just as struts are essential to the structure of a wing, struts might become an indispensable part of your next Web project.
传统机身设计要求使用重型结构材料，以便把机身横向重量转移到机翼下方的起落架和机轮上。
Conventional airframes require heavy structural material to transfer the fuselage's weight laterally to landing gear and wheels under the wings.
但是在2008年，公司发现内部机身结构与机翼结合处的787的碳素纤维“翼盒”，强度不够并且需要金属翼梁的加固。
But in 2008, the firm found that the 787's carbon-fibre "wingbox", the internal fuselage structure the wings attach to, was not strong enough and needed stiffening with metal spars.
由于机翼和尾部边缘的蜂窝状非金属结构不反射雷达波，所以飞机的雷达反射波就减少了很多。
The radar cross-section was further reduced because the wings' leading and trailing edges were composed of nonmetallic honeycomb structures that do not reflect radar rays.
麻省学院的D型“两个泡泡”系列设计概念基于改进过的“管状机身和一对后倾机翼”结构，机身更加宽大，可以提供额外的升力。
MIT’s D “double bubble” series design concept is based on a modified “tube-and-wing” structure that has a very wide fuselage to provide extra lift.
就在上周，机身结构的其他应力测试显示，就在机翼连接的面之上的机身每侧需要强化18个点。
Then last week, other stress tests on an airframe showed that the plane needs strengthening at 18 points on either side of the fuselage just above the area where the wing attaches.
波音公司又一次推迟了波音787梦想飞机的首次试飞。这次是因为机翼与机身的连接区域的结构性缺陷。
Boeing yet again postponed the maiden test flight of its 787 Dreamliner, this time because of structural weakness in the area where the wing attaches to the body of the aeroplane.
壁板式隔框，机身或机翼内一种结构隔板。
MK2型的机身和尾部结构将进行延寿和重新组装，包括采用重新设计的新型机翼和BR 710涡扇发动机。
MK2 fuselage and empennage structure would be re-lifed and reassembled, with redesigned wings and BR710 turbofan engines.
另外，机翼和机翼下具有较为精细的结构的外挂物之间的耦合效应也是不容忽视的。
Another coupling effect between the airfoil and the suspenders containing more exquisite structures is also can not be neglected.
以飞机机翼等大型结构为例，探讨了大型结构部件载荷标定试验的力学模型。
As an example of large sized structural component, the mechanical model of load calibration test of an airplane wing was analysed.
该自适应机翼的重要组成部分是集成到结构中的传感器和致动器。
Important constituents of an adaptive wing are sensors and actuators integrated into the structure.
飞机机翼是一个连续的结构体，通过机身隔框36和42之间。
The aircraft wing is a continuous structure which goes through the fuselage between Frames 36 and 42.
由于中心体与机翼的紧密集成，BWB还提供了结构性优势。
The BWB also offers structural gains due to the close integration of the centerbody with the wing.
简要介绍了自适应机翼的概述和智能材料与结构的功能特点。
This paper introduces in brief the summary of adaptive wing and the function character of smart material and structure.
简要介绍了自适应机翼的概述和智能材料与结构的功能特点。
This paper introduces in brief the summary of adaptive wing and the function character of smart material and structure.
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