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   飞机结构 的翻译结果: 查询用时:1.511秒
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飞机结构     
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  aircraft structure
     FA-CAD/CAPP/CAM SYSTEM FOR THE COMPLICATED AIRCRAFT STRUCTURE PARTS
     复杂飞机结构零件FA-CAD/CAPP/CAM系统
短句来源
     A STUDY ON EIFS DISTRIBUTION OF AIRCRAFT STRUCTURE DETAILS
     飞机结构细节EIFS分布的研究
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     Some technological problems of142 0 Al- L i alloy aircraft structure with use of welding,such as welding methods,welding wire,welding parameters and its influence on me- chanical properties of structure,are reviewed.
     评述了 142 0 Al- L i合金飞机结构的若干焊接工艺问题 ,如焊接方法、焊丝、焊接工艺参数及其对力学性能的影响。
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     Structure and Performance of Formed Forgings of Titanium Alloy TC11 for Aircraft Structure
     飞机结构用TC11钛合金异型锻件的组织与性能
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     DFR METHOD IN CORROTIVE FATIGUE ANALYSIS OF AIRCRAFT STRUCTURE
     飞机结构腐蚀疲劳分析中的DFR法
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更多       
  aircraft structures
     Research on Information Model in Virtual Assembly of Aircraft Structures Based on CATIA/CAA
     基于CATIA/CAA的飞机结构虚拟装配信息模型研究
短句来源
     DAMAGE TOLERANCE AND DURABILITY DESIGN OF COMPOSITE AIRCRAFT STRUCTURES
     复合材料飞机结构损伤容限和耐久性设计初探
短句来源
     The experimental studies of "detail fatigue ratings cutoff (DFRcutoff)" of LY12CZ,LC4CS aluminum alloy and 30CrMnSiA steel commonly used in aircraft structures were conducted in different environment and aircraft structure durability design were provided with important experimental data.
     对LY12CZ、LC4CS铝合金和30CrMnSiA钢进行了不同环境介质下的“细节疲劳额定强度截止值(DFR_(cutoff))”的试验研究,提供了飞机结构耐久性设计的重要数据。
短句来源
     EDDY CURRENT INSPECTION OF FASTENERS IN AIRCRAFT STRUCTURES
     飞机结构紧固件涡流探伤简介
短句来源
     In the present dissertation the focus is on the investigation of fatigue and corrosion cumulative damage rule, for it is the primary element of the approach for the prediction of calendar life and the design of aircraft structures against fatigue and corrosion.
     飞机结构日历寿命的确定与腐蚀环境对飞机结构寿命的影响紧密相连,材料抗疲劳性能随日历年限的变化规律和腐蚀环境作用后的疲劳累积损伤理论是科学地确定飞机结构日历寿命的基础。
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  airplane structure
     Design and Analysis Expert System of Airplane Structure Durability
     飞机结构耐久性设计与分析专家系统
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     The Development of Design for Modern Airplane Structure
     现代飞机结构设计的发展
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     The Applied Technique for Active Vibration Control of Airplane Structure
     飞机结构振动主动控制应用技术
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     APPLICATION OF ACCELERATED FATIGUE TESTS TO STUDY CALENDAR LIFE ON AIRPLANE STRUCTURE
     加速疲劳寿命试验在飞机结构日历寿命研究中的应用
短句来源
     The Actualities and Development of Impact Damage Forecastfor Airplane Structure
     飞机结构撞击损伤预测的现状及发展
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  aircraft structural
     Under windows operation system, a system for test data tracking, analyzing and p rocessing of aircraft structural strength (TestDTAS) is developed on MSC/PATRAN platform. The work is performed with adding special commands and windows by usin g the PCL language provided by MSC/PATRAN and C++ language.
     在Windows环境下,以MSC/PATRAN为平台,利用平台提供的二次开发语言PCL(Patran Command Language),并结合C++语言,通过客户化、增设特定的命令和窗体等技术开发了飞机结构强度静力试验数据实时跟踪与处理系统TestDTAS(Test Data Tracking,Analyzing and Processing System)。
短句来源
     Establishment of Aircraft Structural Life Envelope
     飞机结构寿命包线的建立
短句来源
     On the Comprehensive Design of Aircraft Structural Effectiveness
     飞机结构效能的综合设计
短句来源
     Stress Field Intensity Method Analysis on Fatigue Life of Aircraft Structural Detail
     飞机结构细节疲劳寿命的应力场强法探析
短句来源
     Combined Analysis Model on Aircraft Structural Durability and Damage Tolerance
     飞机结构耐久性/损伤容限综合分析模型
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  aircraft structure
For example, the patterns might be interfered with multi-path signals, which will cause errors in the angle estimation, when installed in an aircraft structure.
      
It is very important for the aircraft structure with MSD to estimate the load carrying capacity of such damaged structures.
      
This paper introduces a methodology for simultaneously designing a minimum weight structure and robust active controls to reduce vibrations in an aircraft structure due to external disturbances.
      
Instead, a multi-antenna system is required with antennas widely distributed over the aircraft structure.
      
This paper derives simple formulas to predict the reduction of the residual strength due to rivet holes in stiffened and unstiffened panels of aircraft structure.
      
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  aircraft structures
Data on microdischarges from both metal elements and the composite elements now widely used in aircraft structures are obtained.
      
Active Thermal Detection of Water in Cellular Aircraft Structures
      
Microprocessor AE System for Strength Tests of Aircraft Structures
      
This paper presents an overview of the damage growth suppression effects in CFRP laminates using embedded SMA foils, and was conducted to technically verify the application to aircraft structures.
      
In this study, recent efforts into the research and development of composite repairs bonded to defective aircraft structures are discussed.
      
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  aircraft structural
Experimental study of repair efficiency for single-sided composite patches bonded to aircraft structural panels
      
Aircraft structural-health monitoring using optical fiber distributed BOTDR sensors
      
We conducted theoretical and practical studies for applying the Brillouin optical timedomain reflectometer (BOTDR) to an aircraft structural-health-monitoring system.
      
Reproducing aircraft structural components using laser scanning
      
In this study, the re-engineering and re-manufacturing capabilities of laser scanning systems in aircraft structural components manufacturing are evaluated.
      
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