| 单词 | 喷气发动机 |
| 释义 | 〔turbofan〕A turbojet engine in which a fan supplements the total thrust by forcing air directly into the hot turbine exhaust.涡轮风扇喷气发动机：一种涡轮喷气发动机带有一个风扇，通过将空气直接压入热的涡轮排气管而补充总推力〔turboramjet〕An aircraft in which a turboramjet is used.冲压式涡轮喷气飞机：装有冲压式涡轮喷气发动机的飞行器〔scramjet〕A ramjet airplane engine designed for hypersonic flight that burns fuel in the supersonic airstream produced by the plane.超音速冲压喷气发动机：一种喷气式飞机发动机，设计用于极超音速飞行，燃料在由飞机产生的超音速气流中燃烧〔turbojet〕A jet engine having a turbine-driven compressor and developing thrust from the exhaust of hot gases.涡轮喷气发动机：一种喷气式发动机，有一个涡轮推动的压气机，通过排出热气而产生推力〔thrust〕The forward-directed force developed in a jet or rocket engine as a reaction to the high-velocity rearward ejection of exhaust gases.推力，侧面压力：喷气发动机或火箭发动机产生的作为高速向后排出的气体的反作用力而向前推动的力量〔turboramjet〕A turbojet engine that can be operated as a ramjet.冲压式涡轮喷气发动机：一种可当作冲压式喷气发动机操作的涡轮喷气发动机〔fanjet〕A jet engine that provides extra thrust by means of a ducted fan in its forward end that draws in extra air.涡轮风扇发动机：一种喷气发动机，前有一管道风扇吸入额外量的空气，这部分空气经压缩后提供额外推力〔combustor〕A combustion chamber and its igniters, injectors, and other related apparatus in a jet engine or gas turbine.燃烧室：喷气发动机或气轮机内的燃烧室及其点火器、喷头和其他相关的装置〔hydrazine〕A colorless, fuming, corrosive hygroscopic liquid, H2NNH 2, used in jet and rocket fuels. 肼：一种无色发烟的、具有腐蚀性和强还原性的液体化合物，H2NNH 2，用于喷气发动机和火箭的燃料 〔afterburner〕A device for augmenting the thrust of a jet engine by burning additional fuel with the uncombined oxygen in the hot exhaust gases.加力燃烧室：通过燃烧热废气中所含的分离氧和附加燃料以增加喷气发动机推力的设备〔twinjet〕An aircraft powered by two jet engines.双喷气发动机的飞机〔ramjet〕A jet engine that propels aircraft by igniting fuel mixed with air taken and compressed by the engine in a fashion that produces greater exhaust than intake velocity.冲压式喷气发动机：一种喷气发动机，靠燃烧发动机吸入和压缩的空气与燃料的混合物推进飞机，其排出空气的速度比吸入快〔athodyd〕A simple, essentially tubular jet engine, such as a ramjet.压式喷气发动机：一种简单的，主要为管道式的喷气发动机，如喷压式发动机 |
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