您要查找的是不是:
- An aircraft in which a turbojet is used. 渦輪噴氣式飛機一種帶渦輪發動機的飛行器
- A turbojet engine used todrive an external propeller. 渦輪螺旋槳發動機一種用於推動外部螺旋槳的渦輪噴氣式發動機。
- The turboprop engine is very much like the turbojet. 渦輪螺槳發動機與渦輪發動機十分相似。
- The turboprop engine is very much like the turbojet . 渦輪螺槳發動機與渦輪發動機十分相似。
- A turbojet engine used to drive an external propeller. 渦輪螺旋槳發動機一種用於推動外部螺旋槳的渦輪噴氣式發動機
- In 1939 the turbojet brought an entirely new method of propulsion. 1939年,渦噴發動機引入了一種全新的推力方法。
- The turbojet and the turboprop are much more satisfactory for airplanes. 渦輪噴氣發動機和渦輪螺槳發動機更適用于飛機。
- The validation of method is demonstrated by one-spool turbojet engine. 單軸渦噴發動機的算例證明了方法的有效性。
- In the case of afterburning, the effective blockage of the EBMC flameholder , i.e. 加 力時,改變尾緣射流速度,可以改變它的有效堵塞比,實現加力比的 無級調節,是一種可變流阻係數(*的穩定器。
- A turbojet engine in which a fan supplements the total thrust by forcing air directly into the hot turbine exhaust. 渦輪風扇噴氣發動機一種渦輪噴氣發動機帶有一個風扇,通過將空氣直接壓入熱的渦輪排氣管而補充總推力
- The J-10 adopts an adjustable, chin-mounted air intake that supplies air to the single Lyulka-Saturn AL-31FN afterburning turbofan jet engine. J-10採用了一個可調節機腹進氣口為一台留里卡-土星設計局的AL-31FN加力燃燒渦輪風扇發動機提供空氣。
- Dispersity of gas flow can be enhanced and afterburning efficiency can be improved by increasing primary nozzle numbers and nozzle expansion ratio. 增加一次噴嘴的數目和加大噴嘴的擴張比增加了燃氣的分散性,提高了補燃效率。
- At this point, we very much look forward to working with you in good faith met together for your business carrier oil Afterburning Tim! 在此,我們非常期望與您真誠相識,共同為您的企業航母添油加力!
- First came the turbojet, now obsolete, then the turboprop, which is still found onboard small planes. 最開始的引擎是渦輪噴射式,目前已淘汰;然後是渦輪螺旋槳式引擎,現在仍可在小飛機上看到。
- Breathing can be divided into jet engine turbojet engine, turbo-fan jet engine and combustion ramjet engine. 如果按照這一定義,除遠程巡航導彈外,各種飛航式反艦導彈和空地、空艦飛航式導彈也屬於巡航導彈。
- The influence of afterburning chamber length on secondary combustion efficiency and flow field were analyzed based on direct-connected ground simulation test. 結合直連式地面模擬試驗,分析了補燃室長度對摻混流場和二次燃燒效率的影響。
- The experimental result has practical significance for correctly using the twin-rotor turbojet. 實驗結果對於正確使用該類型雙轉子渦噴發動機具有重要的現實意義。
- The proposed modeling methods can be extended to study other gas turbines with different types.For example, a twin-spool or with afterburning gas turbine system. 該文提出的建模方法可擴展應用於研究其他結構類型的燃機,如雙軸的或帶有回熱器的燃氣輪機系統。
- Chiang, H. D., and W. C. Ho, 「Miniature Liquid Fueled Turbojet Engine」, U. S. Patent #5782079. 蔣小偉,何無忌,「超小型燃油氣渦輪噴射引擎」中華民國第136677號專利。
- Smetana, F. O.,「Turbojet Engine Gas Path Analysis A Review,」AGARD Conference Proceedings, No. 165, 4-5 April, 1974. 陳大光;張赫然;「用氣動熱力參數對發動機故障進行診斷與定位的實用方法;」北京航空航天大學碩士論文第二章;1989年.