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helicopter
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  直升机
    Helicopter Neural Network Control and Implementation of Handling Quality Requirements
    直升机神经网络控制与飞行品质要求的实现
    Research on Vibration Signal Processing Techniques and Applications to Fault Diagnosis of Helicopter Gearbox
    振动信号处理技术在直升机齿轮箱故障诊断中的应用
    Mathematical Model of Helicopter Rotor Airfoil
    直升机旋翼型面的数学模型
    The Analysis and Control of Rotor Induced Vibration of Helicopter
    直升机全机振动分析与控制
    The Development and Tests of Y-2 Light Helicopter
    Y-2小型直升机的研制和试验
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  直升飞机
    IDS Integrated Dynamic System For Future Helicopter Derelopments
    未来直升飞机开发的综合动力系统(IDS)
    Design of a Cooling Package for Environmental Control in a Helicopter
    某型直升飞机环控系统制冷包设计
    Helicopter Surveying Supper Voltage Transmission Lines
    直升飞机巡视检测高压输电线路
    This article describes dynamic stress measurement of x-type of helicopter tail rotor tunnel test in several principal aspects.
    本文介绍x型直升飞机尾桨吹风试验动应力测量工作的几个主要方面。
    The power train engine→main transmission→main rotor of a conventional helicopter is usually realized in modular design (see Fig.1) Each individual component has its specific function which also in a geometrical sense is performed within strictly defined dimensions in line with the respective configuration.
    普通的直升飞机的动力系统通常是由一些典型的部件(图1)组成。 图1典型部件Fig.1Modulardesign各组成部件具有其专门的功能,同样在几何学方面它们应以其各自的轮廓外形实现严格的尺寸要求。
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  直升机座舱
    Inflatable System for Helicopter Cockpit
    直升机座舱气袋系统
    Investigation of human body vibration exposure in aircraft and helicopter and the permitted standard
    旅客运输机与直升机座舱中人体全身振动环境的调查及其卫生标准的探讨
    After reviewing hygienic standards of microwave radiation domestic and abroad and hygienic situation of investigation,10μW/cm 2 was proposed as the upper limit of microwave radiation in the cabins of passenger aircraft and helicopter.
    建议以<10μW/cm2作为中国旅客运输机与直升机座舱微波辐射的卫生学标准。
    This paper introduces the investigation for the technology and economic availability of manufacturing helicopter cabin subfloor from advanced thermoplastic composite and thermoforming process.
    本文介绍了采用先进的热塑性复合材料和热成形工艺制造直升机座舱地板吸能结构的技术经济可行性研究,并和热固性复合材料进行了对比分析。 研究结果表明,热塑性复合材料地板结构试件的吸能性能优于热固性材料试件,并且当生产数量达到和超过一定值时,热塑性复合材料的成本——效率高于热固性材料。
  “helicopter”译为未确定词的双语例句
    The Design of a Helicopter Rotor Flutter Model by Use of Mach Scaling Approach
    M数缩尺法旋翼颤振动力相似模型设计
    The Design of a Helicopter Rotor Flutter Model by Means of Froude Scaling Method
    F数缩尺法旋翼颤振动力相似模型设计
    STUDY AND SIMULATION OF FIRE CONTROL SYSTEM OF ADVANCED ARMED HELICOPTER
    先进武装直升机火控系统研究与仿真
    THE STUDY FOR HELICOPTER PILOT MODEL
    直升机驾驶员模型研究
    A METHOD FOR CALCULATING KINEMATIC PARAMETERS OF HELICOPTER IN LOOP AND ROLL MANEUVERS
    A METHOD FOR CALCULATING KINEMATIC PARAMETERS OF HELICOPTER IN LOOP AND ROLL MANEUVERS
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  helicopter
A model of the helicopter spatial motion was used by way of example.
      
The system embedding technology was shown to have much wider design potentialities than the current requirements on the design of the helicopter control systems.
      
The experimental results with the adaptive control on the "Helicopter" benchmark were described.
      
This will allow one to land in a prescribed range and to produce adequate conditions for the interception of the reentry spacecraft by a helicopter in order to prevent a rough landing.
      
Construction of a nonstationary nonlinear theory of helicopter rotors
      
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This article describes dynamic stress measurement of x-type of helicopter tail rotor tunnel test in several principal aspects. According to the test requirements emphases are laid on reasonably selecting specimen, measured poi its and method of instrumentation from the view point of dynamic response. A noticeable problem, the influence of support conditions in dynamic stress measureme it of tunnel test is presented.

644彩的新版网站benwenjieshaoxxingzhishengfeijiweijiangchuifengshiyandongyinglicelianggongzuodejigezhuyaofangmian。genjushiyanyaoqiuzhezhongcongzhendongdexiangyingguandianhelixuanzeshijian、celiangdianyuceshifangfa。tichulechuifengshiyandongyingliceliangzhongdeyigezhidezhuyidewenti——zhichengtiaojiandeyingxiang。

With reference to the popular theoretical contour of helicopter rotor airfoil - a form of blade, having trapezoid in plane view , with negative linear twisting and variable airfoil sections, mathematical models of the airfoil section, the whole airfoil, and the surfaces isometrie surface of the locus of cutter centers have been established by means of vector analysis here.A routine is made by using ALGOL-60 Language according to the presented method .

benwenduijuyoujiaopubianyiyideyizhongzhishengjixuanyililunwaixing——pingmianxingzhuangweitixing、youfuxianxingniuzhuan、juyoubianyixingpoumiandejiangye,yishiliangfenxiweigongju,jianlilexuanyideyixingquxian、xuanyixingmianjidaojuzhongxinguijidedengjumiandeshuxuemoxing。 genjubenwendefangfa,yibianzhichengalgol—60yuyanyuanchengxu。

The airscrew included various propellers, fans, windmills and helicopter blades, etc. In an earlier paper [2], we suggested the Mathematical model of helicopter rotor airfoil. In this paper we shall concern ourselves with the problem of describing surfaces of the propellers.Instead of subdividing a surface into parts or "patches" we shall investigate ways to treat it as a whole. This method is simple to implement and computationally efficient.After making a series of researches, the mathematics model...

The airscrew included various propellers, fans, windmills and helicopter blades, etc. In an earlier paper [2], we suggested the Mathematical model of helicopter644彩的新版网站 rotor airfoil. In this paper we shall concern ourselves with the problem of describing surfaces of the propellers.Instead of subdividing a surface into parts or "patches" we shall investigate ways to treat it as a whole. This method is simple to implement and computationally efficient.After making a series of researches, the mathematics model of airplarce propellers has been established. A routine is made by using ALGOL-60 language according to the presented method.

644彩的新版网站kongqiluoxuanbaokuoluoxuanjiang、fengche、fengshanhezhishengjiyepiandeng。zai[2]li,womentichulezhishengjixuanyijiangyedeshuxuemoxing。benwentantaoluoxuanjiangxingmiandemiaoshuwenti。zaizheili,womenbushijiangyigexingmianfenchengxuduokuaihuo“qumianpian”,ershibatadangzuoyigezhengtilaichuli。zheizhongfangfajiandanyixing,jisuanyouxiao。 jingguochubutansuo,yijingjianliqifeijiluoxuanjiangdeshuxuemoxing,erqieyongalgol-60yuyanbianxielejisuanchengxu。

 
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