助手标题  
全文文献 工具书 数字 学术定义 翻译助手 学术趋势 更多
查询帮助
意见反馈
   扭力臂 的翻译结果: 查询用时:0.665秒
图标索引 在分类学科中查询
所有学科
航空航天科学与工程
更多类别查询

图标索引 历史查询
 

扭力臂     
相关语句
  “扭力臂”译为未确定词的双语例句
     THE TECHNOLOGY RESEARCH AND PRACTICE OF THE FATIGUE TEST FOR THE TWISTING FORCE ARM OF THE LANDING GEAR
     飞机起落架扭力臂变行程疲劳试验技术研究与实施
短句来源
  相似匹配句对
     The torsion balance
     谈
短句来源
     TORSION CLASSES OF S-SYSTEMS
     S-系的
短句来源
     An Experimental Study on the Length and Arm of Quadriceps Femoris
     股四头肌长度和力臂的实验性研究
短句来源
     Measuring arm of force in all directions directly
     直接测量任意方向力的力臂
短句来源
     Moment arms of the wrist motor tendons and its implication
     人腕关节动力肌腱的力臂值及意义探讨
短句来源
查询“扭力臂”译词为用户自定义的双语例句

    我想查看译文中含有:的双语例句
例句
为了更好的帮助您理解掌握查询词或其译词在地道英语中的实际用法,我们为您准备了出自英文原文的大量英语例句,供您参考。
  scissor link
These computations yielded the link length, final base size, and the final scissor link angle.
      
  torque arm
These examples include the size optimization of a 40 member frame, the configuration design of a 25-bar space truss and the shape design of a torque arm and a plate with a hole.
      
Apparatus including a torque arm pivoted about a fulcrum to reposition the tool face with respect to the support or holder.
      
A torque arm was connected between the front bellcrank pivots and a load was applied at the outboard end.
      
As shown, a loop of wire with a torque arm R is free to rotate about the z-axis.
      
By shortening the torque arm, the length of stroke is shortened and less water is lifted per revolution of the turbine.
      
更多          


Applying the general linear theory of shimmy, this paper analyzes the main wheel shimmy problem of a special type of the main landing gear equipped with an additional shimmy damper between the upper part and lower part of torque arms. The influence of various structural and operational parameters on shimmy is discussed, and the results show that the additional damper is necessary and effective for preventing shimmy. Meanwhile, a new version of this type of airceraft with four wheel bogie main landing gear is...

Applying the general linear theory of shimmy, this paper analyzes the main wheel shimmy problem of a special type of the main landing gear equipped with an additional shimmy damper between the upper part and lower part of torque arms. The influence of various structural and operational parameters on shimmy is discussed, and the results show that the additional damper is necessary and effective for preventing shimmy. Meanwhile, a new version of this type of airceraft with four wheel bogie main landing gear is also investigated. It is concluded that in this case the additional damper can be omitted, since this landing gear itself is inherently stable as for shimmy. This approach aims to explain the practical advice adopted in an existing design. The results may also be referred for other aircraft design.

针对××型飞机主起落架上、下扭力臂之间装有附加阻尼器的特殊方案,分析了主起落架机轮摆振问题,讨论了各种参数的变化对防止摆振的作用,结果表明附加阻尼器对防止摆振的必要性和有效性。同时,又对该型飞机采用4轮小车式主起落架的改型方案,验证了去掉原来附加阻尼器的合理性。

This paper describes a method of fatique test of the twisting force arm of landing gear and discusses the necessity of variable stroke test of landing gear. It takes into account the effects of variable stroke test of landing gear on the crack growth. This paper provides the information for determining the service life and the overhaul periods with high reliability of structure of landing gear. The result of the test indicates that the fatique crack situation and its propagation rate are in accordance with the...

This paper describes a method of fatique test of the twisting force arm of landing gear and discusses the necessity of variable stroke test of landing gear. It takes into account the effects of variable stroke test of landing gear on the crack growth. This paper provides the information for determining the service life and the overhaul periods with high reliability of structure of landing gear. The result of the test indicates that the fatique crack situation and its propagation rate are in accordance with the field-failure data.

阐述了起落架扭力臂变行程疲劳试验的必要性,提出了扭力臂变行程疲劳试验的实施方法,设计了加载装置。通过某型飞机起落架扭力臂变行程疲劳试验的实施,使外场故障再现,证明了该试验实施方法合理可行。

 
图标索引 相关查询

 


 
CNKI小工具
在英文学术搜索中查有关扭力臂的内容
在知识搜索中查有关扭力臂的内容
在数字搜索中查有关扭力臂的内容
在概念知识元中查有关扭力臂的内容
在学术趋势中查有关扭力臂的内容
 
 

CNKI主页设CNKI翻译助手为主页 | 收藏CNKI翻译助手 | 广告服务 | 英文学术搜索
版权图标  2008 CNKI-中国知网
京ICP证040431号 互联网出版许可证 新出网证(京)字008号
北京市公安局海淀分局 备案号:110 1081725
版权图标 2008中国知网(cnki) 中国学术期刊(光盘版)电子杂志社