记作业>英语词典>ejection seat翻译和用法

ejection seat

英 [i(ː)ˈdʒɛkʃən siːt]

美 [ɪˈdʒɛkʃən siːt]

弹射椅;弹射座椅

英英释义

noun

  • a pilot's seat in an airplane that can be forcibly ejected in the case of an emergency
      Synonym:ejector seatcapsule

    双语例句

    • This paper analyses the ejecting rescue of К-36 ДМ ejection seat of a certain fighter plane. It builds up the kinematic mathematical model of man-seat system, and gives the kinematic features before parachute being opened.
      对某型飞机К-36ДМ弹射座椅的弹射救生进行了分析,建立了人椅系统的运动数学模型,给出了其在开伞前的运动特性。
    • A brief history and development for ejection seat is introduced.
      本文回顾了弹射座椅的发展历程。
    • According to the problems of the lapping technology of a driven toothed bar pair of rise and fall system of aircraft ejection seat, the abrasive tool, abrasive material and lapping amount are discussed. The lapping technology is perfected and the required results are obtained through tests.
      针对飞机弹射座椅升降系统从动齿杆副的研磨技术问题,讨论了研具、研磨剂和研磨用量,通过试验完善了研磨技术,获得了预期的效果。
    • The research of ejection seat test
      弹射座椅试验研究
    • Calculation and Establishment of Interior Ballistics Model for Ejection Gun of Rocket Ejection Seat
      火箭弹射座椅弹射动力系统内弹道模型建立与计算
    • As a kind of safety devices of aircraft, the ejection seat is regarded as the most reliable life-saving tool and the most widely used equipment in the air rescue.
      航空救生中的弹射座椅是飞机的重要安全装置,也是当前救生系统中最为广泛、最为可靠的救生工具。
    • Lapping Technology of a Driven Toothed Bar Pair of Rise and Fall System of Aircraft Ejection Seat
      飞机弹射座椅升降系统从动齿杆副的研磨技术
    • Deceleration performance is an important performance of ejection seat, whose evaluation is coarse till now and can be estimated, only according to the ground ejection experiment or experience.
      减速性能是火箭弹射座椅的一个重要性能指标,而且一直不能得到很好的评估预测,只能根据地面弹射试验和经验粗略估计座椅的减速性能。
    • Your stop is like an ejection seat on an aircraft.
      止损就想是飞机上的弹射椅。
    • In order to test the dynamic characteristics of the stabilizing parachute of the ejection seat in high speed flow, dynamic force tests for the stabilizing parachute have been conducted in 1.2m × 1.2m high speed wind tunnel of CARDC.
      为了测试弹射座椅稳定伞在高速气流中的动态特性,在1.2m×1.2m跨、超声速风洞(FL24)进行了稳定伞高速风洞动态测力试验。