旋翼機 的英文怎麼說

中文拼音 [xuányìjī]
旋翼機 英文
[航空] rotaplane; autogiro; autogyro; rotorcraft; rotary-wing aircraft
  • 旋 : 旋Ⅰ動詞1 （旋轉） whirl 2 （用車床切削或用刀子轉著圈地削） turn sth on a lathe; lathe; pare Ⅱ名詞...
  • 翼 : Ⅰ名詞1 （翅膀） the wing of a bird 2 （像翅膀的東西） the wing of an aeroplane etc : 鼻翼 wing of...
  • 機 : machineengine
  • 旋翼 : helicopter rotor
  1. Standard practice for continued airworthiness system for light sport gyroplane aircraft

    輕型運動自轉旋翼機的持續適航系統的標準實施規程
  2. The stability of the tiltrotor in the heli copter mode is analyzed aiming t a semi span soft - inplane tiltrotor model with an elastic wing

    集成了非定常動態人流方程與傾轉過渡狀態的多體動力學力程，建立了傾轉旋翼機時域非定常氣彈耦合分析模型。
  3. Breakthroughs in modern gyroplane technology - an introduction to the advances in gyroplane technology and the emerging market opportunities for a new generation of gyroplanes ranging from small vtol & ustol gyroplanes to large vtol gyrodyne airliners or freighters with 20 ton payload capacity

    現代旋翼機科技的突破-介紹旋科技的進步，以及新一代旋翼機的市場機會，從小型超短距離升降和垂直升降的旋翼機到可垂直升降，載重20噸以上的大型直升旋翼客機和貨運機
  4. Standard specification for design and performance of light sport gyroplane aircraft

    輕型運動自轉旋翼機的設計和性能的標準規范
  5. Standard specification for manufacturer quality assurance program for light sport gyroplane aircraft

    輕型運動旋翼機用製造者質量保證程序的標準規范
  6. The hawk 4 gyroplane is supported in the air by a horizontally mounted airfoil similar to that of a helicopter but unpowered

    鷹4旋翼機利用類似直升機的旋翼提供升力，但機頂的水平旋翼無需動力推動。
  7. The pilot held a current airline transport pilot s licence ( helicopters and gyroplanes ) and a valid class one medical certificate. he had 3, 900 hours of operating experience

    肇事直升機的飛行員具備有效的航空運輸飛行員執照（直升機和自轉旋翼機）和一級體檢合格證明書，並擁有3 ， 900小時的飛行經驗。
  8. Handling loads suspended from rotorcraft

    裝卸旋翼機上懸吊的貨物
  9. This paper is a review of rotorcraft cfd in light of major unsolved problems, and some prospects and solution philosophy for solving them

    本報告是依據未解決的重大問題、解決這些問題的若干前景和指導思想對旋翼機計算空氣動力學（ cfd ）所作的評述。
  10. The rotor / wing aerodynamic interactions of the tilt rotor vehicle in hover is described in this dissertation

    本文主要研究的是傾轉旋翼飛行器懸停狀態時，旋翼機翼之間的氣動干擾問題。
  11. When the tilt rotor vehicle is in hover, the aerodynamic download of the rotor flowfield imposes on the wing. in this time, the rotor / wing interaction is severe

    傾轉旋翼飛行器懸停時，旋翼的下洗流剛好作用在機翼上，此時，旋翼機翼間的氣動干擾非常劇烈。
  12. Variable diameter rotor is an effective method to improve the aerodynamic performance of tilt - rotor in both hover and cruise state. on the basis the research before, the variable diameter tilt rotor structure design has been finish, and in virtue of the technology of virtual prototyping to simulate and analyze the kinetic, dynamic and intensity property of it

    變直徑傾轉旋翼能有效的改善傾轉旋翼機懸停和巡航狀態下的氣動效率，本文提出了變直徑傾轉旋翼試驗模型設計方案，完成了可變直徑傾轉旋翼的結構設計，並利用虛擬樣機技術對變直徑傾轉旋翼的運動特性、結構動力學特性以及結構強度進行了分析、研究。
  13. On the basis of axial vortex theory, the aerodynamic performance of tilt - rotor model has been built, and using it to analyze the aerodynamic performance of xv - 15, comparing to the actual data to prove the model ’ s validity, finally studied the variety of aerodynamic performance relative to the variable rotor diameter

    以軸向渦流理論為基礎，建立了適合於傾轉旋翼機氣動分析模型，以xv - 15傾轉旋翼機作為算例，通過結果的對比，表明本文的氣動模型能較好的分析傾轉旋翼機的氣動性能，並在氣動性能的基礎上分析了直徑變化對傾轉旋翼機氣動性能的影響。
  14. Mathematical model and formulations of a new tilt - rotor aircraft for aeroelastic stability analysis

    新型傾轉旋翼機氣動彈性穩定性分析模型
  15. The multi - body analysis of the aeroelastic stability of the tiltrotor aircraft is presented

    摘要通過多體動力學方法建立了傾轉旋翼機動力學分析模型。
  16. As one of the basic problem of helicopter dynamics, the aeromechanical stability of the coupled rotor - body system has been paid a lot of attention

    直升機旋翼/機體耦合系統的氣動機械動穩定性問題是直升機動力學的基本問題之一，長期以來一直受到人們的普遍關注。
  17. In order to analyze this model, a modified multi - blade coordinate transformation was proposed. at last, the aeromechanical stability problem was analyzed with the two

    最後用上述兩種分析方法對帶葉間減擺器的旋翼/機體耦合系統的氣動機械穩定性問題進行了分析研究。
  18. To study the influence of this damper configuration to aeromechanical stability, some work has been done in this thesis. first, dynamic equation of the rotor - hub system was modeled with the generalized hamilton principle, which can be used to analyze the stability problem in different conditions like on - ground, hovering and flight. when fastening the fuselage, the model can also be used to analyze the stability problem of isolated rotor system

    為了研究這種新型布置減擺器對直升機穩定性的影響，本文所作研究工作如下:首先，本文利用廣義的hamilton原理建立了適用於不同狀態（地面、懸停和前飛）的旋翼/機體耦合系統的動力學模型，該模型中將機體固定可以用來分析孤立旋翼的穩定性問題。
  19. In chapter 5, a new dynamic wake model is developed by employing the rotor free - wake method in chapter 2, and is used to investigate the curve distortion during the conversion of tiltrotor aircraft between helicopter flight conditions and airplane flight conditions

    在第二章方法的基礎上，第五章建立一個傾轉旋翼動態尾跡模型，使用該模型對傾轉旋翼機傾轉過渡狀態的尾跡彎曲變形進行了研究，得出了一些結論。
  20. Within this analytical model, the factors as unsteady aerodynamic and blade flap / lead - lag coupled motion are both considered

    旋翼機體耦合動力學模型考慮了非定常空氣動力和槳葉揮舞擺振運動耦合。
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