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全尺寸结构
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  “全尺寸结构”译为未确定词的双语例句
     CATAS ( Computer Aided Test and Analysis System ) is used for combining large scale static structural test and analysis. One of its aims is ensuring the consistency and reliability between structural analysis results ( FEM or engineering method ) and test measuring data.
     CATAS系统是用于全尺寸结构静力试验与分析的大型综合系统,目的之一就是为保证有限元分析和工程细节分析结果和试验测量结果的一致性和可靠性。
短句来源
     The precondition of solving life prediction and life extension for airplane structures is to work out a typical load time history, i.e. load spectrum, which can simulate airplane's real service situation. This is the basis of theory analysis and whole size structure fatigue test.
     解决飞机结构定寿、延寿的先决条件是 ,编制出能模拟飞机真实情况具有代表性的典型载荷 时间历程 ,即载荷谱 ,以此作为理论分析和全尺寸结构疲劳试验的基础 .
短句来源
     This paper describes all engineering key techniques used to evaluate life of dynamic components for the Z8 helicopter and puts emphasis on the method of determining S - N curve of full-scall construction and technology of drawing up measuring load-spectrum .
     本文全面叙述直8型机动部件定寿中采用的所有工程技术关键,重点介绍了全尺寸结构的S-N曲线确定方法和实测载荷谱的编制技术。
短句来源
     According to the principle of the equivalent damage, we use the simplified loading spectrum and damage accumulation to derive the constant amplitude loading for full scale blade fatigue testing.
     对于叶片全尺寸结构疲劳试验用的等幅试验谱,可由简化载荷谱及线性损伤累积理论,按损伤等效原则求出。
  相似匹配句对
     Compared the actuality of the structure of th
     *; 结构;
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     Structure of perfect Artin Rings
     Artin环的结构
短句来源
     The Similarity of Structure and Dimensions of the Wheel Loaders
     装载机的结构尺寸相似性
短句来源
     Using AFS algebra and AFS structure, any human ordinary fuzzy concept can be represented.
     结构
短句来源
     Digital Simulation of Full Scale Static Test of Aircraft
     尺寸飞机结构静力试验数字仿真(英文)
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CATAS ( Computer Aided Test and Analysis System ) is used for combining large scale static structural test and analysis. One of its aims is ensuring the consistency and reliability between structural analysis results ( FEM or engineering method ) and test measuring data. How to modify test based FEM models from the one used for designing is demonstrated.

CATAS系统是用于全尺寸结构静力试验与分析的大型综合系统,目的之一就是为保证有限元分析和工程细节分析结果和试验测量结果的一致性和可靠性。对设计厂、所提供的强度校核的有限元模型如何修改后建立用于试验分析的有限元模型进行了论述。

The precondition of solving life prediction and life extension for airplane structures is to work out a typical load time history, i.e. load spectrum, which can simulate airplane's real service situation. This is the basis of theory analysis and whole size structure fatigue test. In view of this, the data treatment and the compilation procedure of median stochastic load spectrum are discussed. The data treatment expert system for median stochastic load spectrum is created. It includes system framework design,...

The precondition of solving life prediction and life extension for airplane structures is to work out a typical load time history, i.e. load spectrum, which can simulate airplane's real service situation. This is the basis of theory analysis and whole size structure fatigue test. In view of this, the data treatment and the compilation procedure of median stochastic load spectrum are discussed. The data treatment expert system for median stochastic load spectrum is created. It includes system framework design, data description and parameter configuration, implementation process and database design, etc. The research achievement has been used for load spectrum data treatment and compilation for airplane, aeroengine, airplane landing gear and main fighting tank, etc.

解决飞机结构定寿、延寿的先决条件是 ,编制出能模拟飞机真实情况具有代表性的典型载荷 时间历程 ,即载荷谱 ,以此作为理论分析和全尺寸结构疲劳试验的基础 .对此 ,在探讨中值随机载荷谱数据处理与编制过程的基础上 ,建立了中值随机载荷谱数据处理专家系统 .内容包括系统结构设计、数据描述与参数设置、实现过程和数据库设计等 .本项研究成果已用于飞机、航空发动机、飞机起落架和主战坦克等载荷谱的实测数据处理与编制之中

The Z8 helicopter has special constrution of dynamic components and many key positions. These dynamic components major bear high-frequency and low-amplitude high-cycle vibration fatigue load and they are high-cycle fatigue construction. They are main elements of evaluating fatigue life of the helicopter, which differs from evaluating fatigue life of fixed-wing aircraft. This paper describes all engineering key techniques used to evaluate life of dynamic components for the Z8 helicopter and puts emphasis on the...

The Z8 helicopter has special constrution of dynamic components and many key positions. These dynamic components major bear high-frequency and low-amplitude high-cycle vibration fatigue load and they are high-cycle fatigue construction. They are main elements of evaluating fatigue life of the helicopter, which differs from evaluating fatigue life of fixed-wing aircraft. This paper describes all engineering key techniques used to evaluate life of dynamic components for the Z8 helicopter and puts emphasis on the method of determining S - N curve of full-scall construction and technology of drawing up measuring load-spectrum .

直8型机动部部件结构形式特殊,关键部位众多,主要承受高频率、低幅值的高周振动疲劳载荷,属高周疲劳结构,是直升机疲劳定寿的主体,与定翼机的疲劳定寿有很大差别。本文全面叙述直8型机动部件定寿中采用的所有工程技术关键,重点介绍了全尺寸结构的S-N曲线确定方法和实测载荷谱的编制技术。

 
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