某型飞机,aircraft
1)aircraft[英]["e?krɑ:ft][美]["?r"kr?ft]某型飞机
1.Development of Aircraft Battle Damage Assessment and Repair Forecasting Spare Part System某型飞机战伤抢修备件保障预测系统开发
2.The corrosion characteristics ofaircraft structures were briefed.在某典型机场地面停放环境谱的基础上,综合考虑关键部位的结构形式、密封性等因素,以某型飞机机翼Ⅳ梁接头为例,对飞机结构局部环境谱编制的工程方法进行了探索。
英文短句/例句
1.Flight Test Technique for Certain Model Airplane"s Stall/Spin Motion某型飞机模型失速/尾旋飞行试验技术
2.Analysis of Fatigue Characteristics of a Certain Type Nose Landing Gear;某型飞机前起落架结构疲劳特性分析
3.Study of Oil Measure Instrument for Some Areoplane Feul System;某型飞机燃油系统油量测量仪的研制
4.Design of IETM for some Aircraft Based on PDA;基于PDA的某型飞机IETM的设计
5.Research on the Landing Dynamic Performance for a Certain Type of Aircraft Landing Gear某型飞机起落架的着陆动态性能研究
6.Control System Design of Aircraft High Pressure Hydraulic Power Carts某型飞机高压油泵车控制系统的设计
7.Thermal Simulation of One Aircraft Hydraulic System Based on AMESim基于AMESim的某型飞机液压系统温度仿真
8.Simulink Simulation of Landing Gear Movement of an Aircraft某型飞机起落架运动的SIMULINK仿真
9.Design of Simulative Training System For HUD某型飞机平显火控模拟训练系统设计
10.Performance Analysis of Micro-ejector Anti-icing Tunnel;某型飞机防冰系统机翼防冰腔性能研究
11.Fault Diagnosis Expert System for One Type Aero-engine in Our Army;我军某型飞机发动机故障诊断专家系统
12.A Study of Fatigue Properties of Newly- formed and Served Canopy PMMA in Certain Airplane某型飞机新旧座舱盖有机玻璃的疲劳性能研究
13.Development of Intelligence Test Bed of Certain Type GCU某型飞机发电机控制器智能测试台的研制
putation of Moving Track for Buoy Dropped From Aircraf浮标在某型飞机上投放离机时的运动轨迹计算
15.Developed of Testing System for Certain Aero-engine Temperature Controller某型飞机发动机温度控制盒检测系统设计
16.Bifurcation Analysis of a Nonlinear Dynamics Aircraft Model某型飞机非线性动力学特性的分叉分析
17.Structural Strength Analysis and Design Optimization for a Certain Type of Canopy;某型飞机座舱罩结构强度分析与设计优化
18.Parallel Computing of Dynamic Character of a Plane Wing;某型号飞机机翼动力特性的并行计算
相关短句/例句
Light aircraft轻型飞机
1.Influence of climate conditions on the safe light aircraft operations against forest pest insects and its countermeasures;气候条件对轻型飞机防治森林害虫的影响与对策研究
2.Linkages are extensively adopted in the design of light aircraft.轻型飞机上有大量的杆系结构，传统的杆料毛坯长度只靠试验得出。
3.In particular, the importance of fuzzy optimization in the preliminary design phase of light aircraft is discussed.本文介绍了工程设计中的不确定性信息，着重讨论了轻型飞机在总体设计阶段中，对总体性能进行模糊优化设计的必要性。
3)large aircraft大型飞机
1.This paper aims at thelarge aircraft and its structure characteristics,and by comparing the man assembly system with the machine assembly system and analyzing relation curves of automatic assembly and assembly cost,points out the meaning of automatic assembly technology which ensures long life,high efficiency and low cost oflarge aircraft structure,both in research and in manufacture.简述了大型飞机及其结构特点,通过比较人与机器两种装配系统的特性,及分析装配自动化水平与装配成本等诸因素的关系曲线,指出了自动化装配技术在保证大型飞机结构长寿命、高效率、低成本研制和生产等方面的意义;对国外大型飞机的装配自动化发展状况进行了综述,简要分析了国外发展的几种主要自动化装配系统,总结了国外大型飞机的自动化装配水平;对西方国家在大型飞机自动化装配中采用的先进的装配理念和方法,如决定性装配方法等进行了概述。
2.The present development and tendency of new materials used inlarge aircraft are introduced.介绍了用于大型飞机的新材料的发展现状和趋势。
3.It is argued that while developing airborne equipment for China slarge aircraft should mainly rely on our own research and development(R&D),attention should also be paid to possible international cooperation of various forms for win-win purposes.阐述了大型飞机工程中飞机、发动机、机载设备协调发展的必要性;提出了中国大型飞机机载设备的研发必须把立足点放在自主研发上,同时也要注意不同形式的国际合作,争取双赢;建议重视大型飞机共用技术和共用研发平台的开发,以利于提高资金的有效利用率;特别强调找准市场定位发展有特色的机载设备以提高国产大型飞机的市场竞争力;最后建议了11项需提前启动的项目。
4)aircraft model飞机模型
1.To measure theaircraft model attitude in the spin time,a method based on stereo vision is presented.最后,分别给出旋转天平实验和风洞实验的实测数据,实测结果表明该方法测量准确,鲁棒性好,在立式风洞飞机模型尾旋运动测量的应用中十分有效。
5)plane model飞机模型
1.Using simulink toolbox of matlab to establish aplane model.使用Matlab的Simulink工具箱建立了飞机模型,利用代码生成工具箱将其转换为C代码,再利用嵌入式操作系统VxWorks的集成开发环境Tor nado把该代码下载到嵌入式主机,从而和一些其它外围设备快速完成飞控测试系统的开发。
6)airplane model飞机模型
1.Focused on the uncertainty ofairplane model,a kind of fuzzy control in which the fuzzy rules are optimized and the field of fuzzy variable can be adjusted adaptively was adopted in this paper.针对飞机模型的不确定性,文中采用模糊规则寻优调整和模糊变量论域自适应调整的模糊控制方法,对飞机姿态角自动控制系统进行设计,分别在6个不同的飞行状态,向系统引入相同的俯仰角偏差,数字仿真结果表明,这种模糊控制方法取得了良好的控制效果。
延伸阅读
变后掠翼飞机(见后掠翼飞机)变后掠翼飞机(见后掠翼飞机)swing-wing aircraftbianhoul位eyi feiii变后掠翼飞机(swing一wing aircran)见后掠翼飞机。
