起飞重量

  • 网络flying weight;Weight;MTOW;TOW;flight weight
起飞重量起飞重量
  1. 为了满足部队提高该机起飞重量和跨海作战的使用要求,急需提高直九武装直升机主减速器的传递功率和战场生存能力。

    To meet the urgent needs of heightening own flying weight and battle across the sea , the transmission power of the Z-9 military helicopter main gearbox and battlefield viability have to be increased as soon as possible .

  2. a380的最大起飞重量为560吨,是天空中的巨人,但在起飞时,噪音只有波音747-400的一半。

    With a maximum take-off weight of 560 tonnes , the A380 is the giant of the skies but , at take-off , it has half the noise of the Boeing 747-400 .

  3. 战斗机单机寿命监控中起飞重量的影响

    Effect of Take-off Weight in Fighter Fatigue Life Monitoring

  4. 各型航空器所使用的最大起飞重量和最大着陆重;

    The maximum takeoff and landing weight to be used for each type of aircraft ;

  5. AG600由四台国产涡桨-6涡轮螺旋桨发动机提供动力,最大起飞重量达53.5吨。

    Powered by four domestically designed WJ-6 turboprop engines , it has a maximum takeoff weight of 53.5 metric tons .

  6. AG600机长37米,翼展38.8米,最大起飞重量53.5吨。

    The 37-meter AG600 , with a wingspan of 38.8 meters , has a maximum take-off weight of 53.5 tons .

  7. 其它性能改进有:持续回转率被提升了14%,增加了最大起飞重量、翼内的储油量以及额外的一百○一公里的作战半径。

    Other improvements include increased sustained turn rate by14 % , increased in-wing fuel capacity , increased MTOW and increased combat radius by101 km .

  8. AG600最大起飞重量53.5吨,水上应急救援可以一次性救护50名人员。

    The plane has a maximum takeoff weight of 53.5 tons , and is able to carry 50 people during a maritime search and rescue mission .

  9. 由结果可知,该机的实际起飞重量与优化结果十分相似,证明了优化计算的可行性和高精度。

    Simulation result shows that the result of the optimization is resemble to the practice , and the algorithm is feasible , reasonable and of high precision .

  10. 通过现有地效飞行器数据和资料的整理,研究其起飞重量与空机重量以及其他各项参数的统计关系。

    By searching and sorting out the data of existing WIG , the statistic relationship of takeoff weight and empty weight as well as other parameters are studied .

  11. 通过数据分析计算起飞重量和空机重量估算中的线性回归值,形成适用于各类地效飞行器的重量估算方法及其推荐经验系数。

    Through data analysis and linear regression value calculation , the weight estimation methods and recommended experience factors which can be applied to every type of WIG are determined .

  12. 为了实现飞行器最小净起飞重量的要求,复合材料在航空航天领域应用越来越广泛,特别是碳纤维增强树脂基复合材料。

    To achieve the requirements of the aircraft minimum take-off weight , composite materials are used in the aerospace field more and more widely , especially carbon fiber reinforced resin matrix composites .

  13. 通过地毯图,设计人员可以选取在满足飞机各个设计性能要求约束下使得飞机起飞重量最小的推重比和翼载的组合。

    By using this carpet plot , a designer can conveniently select the values of the wing loading and the thrust-to-weight ratio to minimize the takeoff weight , while still meeting the performance requirements .

  14. “嫦娥五号”探测器起飞重量8.2吨,包括轨道器、返回器、着陆器、上升器四个部分,将在月球轨道实施无人交会对接。

    Chang'e-5 , comprising an orbiter , a returner , a lander , and an ascender , with a total takeoff mass of 8.2 tonnes , is expected to accomplish unmanned rendezvous and docking in lunar orbit .

  15. 在地毯图中,描述了飞机推重比和翼载与客机最大起飞重量之间的相互关系。同时依据界限线的绘制方法,也将客机各个设计性能要求绘制在同一张图上。

    In the carpet plot module , the relation of the aircraft takeoff weight with the wing loading and thrust-to-weight ratio are displayed on the carpet plot , and various requirement boundaries are also plotted on the same plot .

  16. 主要通过飞行参数记录仪(FPR)记录的数据研究战斗机起飞外挂重量对飞机结构疲劳寿命的影响。

    How the variation of take-off suspension weights affects the structural fatigue life is investigated through surveying actual flight parameter recorder ( FPR ) data .

  17. 其任务是找到能满足飞机性能要求的飞机主要参数。这些参数包括:起飞翼载、推重比、起飞重量、机翼面积、机翼翼载、机翼后掠角、机翼相对厚度和机翼梯形比等。

    The task of the initial sizing is to find the primary parameters of aircraft , including the takeoff wing loading , thrust-to-weight ratio , takeoff weight , wing area , aspect ratio of wing , wing sweep , thickness and taper ratio to match the mission requirements .

  18. 中断起飞过程中,取决于刹车吸收预定能量之能力的最大起飞重量。

    The maximum takeoff weight based on the ability of the brakes to absorb a predetermined amount of energy during a rejected takeoff .