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- An aircraft in which a turbojet is used. 渦輪噴氣式飛機一種帶渦輪發(fā)動(dòng)機的飛行器
- A turbojet engine used todrive an external propeller. 渦輪螺旋槳發(fā)動(dòng)機一種用于推動(dòng)外部螺旋槳的渦輪噴氣式發(fā)動(dòng)機。
- The turboprop engine is very much like the turbojet. 渦輪螺槳發(fā)動(dòng)機與渦輪發(fā)動(dòng)機十分相似。
- The turboprop engine is very much like the turbojet . 渦輪螺槳發(fā)動(dòng)機與渦輪發(fā)動(dòng)機十分相似。
- A turbojet engine used to drive an external propeller. 渦輪螺旋槳發(fā)動(dòng)機一種用于推動(dòng)外部螺旋槳的渦輪噴氣式發(fā)動(dòng)機
- In 1939 the turbojet brought an entirely new method of propulsion. 1939年，渦噴發(fā)動(dòng)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(fā)動(dòng)機和渦輪螺槳發(fā)動(dòng)機更適用于飛機。
- The validation of method is demonstrated by one-spool turbojet engine. 單軸渦噴發(fā)動(dòng)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(shí)，改變尾緣射流速度，可以改變它的有效堵塞比，實(shí)現加力比的 無(wú)級調節，是一種可變流阻系數(*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(fēng)扇噴氣發(fā)動(dòng)機一種渦輪噴氣發(fā)動(dòng)機帶有一個(gè)風(fēng)扇，通過(guò)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采用了一個(gè)可調節機腹進(jìn)氣口為一臺留里卡-土星設計局的AL-31FN加力燃燒渦輪風(fēng)扇發(fā)動(dòng)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(yè)航母添油加力！
- First came the turbojet, now obsolete, then the turboprop, which is still found onboard small planes. 最開(kāi)始的引擎是渦輪噴射式，目前已淘汰；然后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于巡航導彈。
- 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(cháng)度對摻混流場(chǎng)和二次燃燒效率的影響。
- The experimental result has practical significance for correctly using the twin-rotor turbojet. 實(shí)驗結果對于正確使用該類(lèi)型雙轉子渦噴發(fā)動(dòng)機具有重要的現實(shí)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于研究其他結構類(lèi)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(wú)忌，“超小型燃油氣渦輪噴射引擎”中華民國第136677號專(zhuān)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(dòng)熱力參數對發(fā)動(dòng)機故障進(jìn)行診斷與定位的實(shí)用方法;”北京航空航天大學(xué)碩士論文第二章;1989年.
