推重比的英文

• thrust loading
• thrust mass ratio
• thrust weight ratio
• thrust-to-weight ratio
• thrust-weight ratio

• "比"英文翻译    2
• "推力重量比 推重比" 英文翻译 :    thrust-weightratio
• "高推重比涡轮喷气发动机" 英文翻译 :    high-thrust-to-weight ratio turbojet
• "推力负荷 推重比 重量推力比" 英文翻译 :    thrustloading
• "推重" 英文翻译 :    have a high regard for; hold in esteem: “本草纲目” 问世之后, 深受人们的推重。 the compendium of materia medica has been held in high esteem since it was first published
• "重比" 英文翻译 :    double ratio
• "多重比" 英文翻译 :    multiple ratio
• "根重比" 英文翻译 :    root weight ratio
• "果重比" 英文翻译 :    fruit weight ratio
• "强重比" 英文翻译 :    ratio of strength to weight; strength-weight ratio
• "容重比" 英文翻译 :    volume to weight ratio
• "体重比" 英文翻译 :    weight ratio
• "叶重比" 英文翻译 :    lwr leaf weight ratio
• "载重比" 英文翻译 :    bearing ratio; load ratio
• "抓重比" 英文翻译 :    anchor holding power to weight ratio; holding power to weight ratio
• "阻重比" 英文翻译 :    drag-weight ratio
• "多重比较" 英文翻译 :    multiple comparisons; multiplecomparison
• "加州重比值" 英文翻译 :    cbr value
• "举重比赛" 英文翻译 :    weight-lifting
• "三重比圆" 英文翻译 :    triplicate ratio circle
• "双重比较" 英文翻译 :    double comparative
• "有效载重比" 英文翻译 :    payload ratio
• "载重比试验" 英文翻译 :    bearing ratio test
• "载重自重比" 英文翻译 :    payload-weight ratio
• "重比重相" 英文翻译 :    heavy phase

• With the rapid development of aero science , it requires the aero engine ratio of traction to weight is higher and higher
  随着航空科技的飞速发展，要求提供推重比越来越高的航空动力。
• The results showed that the thrust - weight ratio reached 1 . 04 for the launch weight 5400kg in the condition of specific impulse near 600s
  结果表明:在发动机工作比冲接近600s的情况下,对于起飞质量为5400kg的飞行器而言,推重比为1 . 04左右。
• To optimize specific impulse to 700s or 800s , the thrust - weight ratio could be improved to 1 . 23 or 1 . 41 , it is enough to achieve the launch requirement for this vehicle
  进一步将比冲优化至700s或800s ,可以将推重比提高至1 . 23或1 . 41 ,这样就完全能够保证发射任务的完成。
• The purpose of this paper is to make extensive study on the essence of impingement / effusion film cooling , and the research results will be applied in futural study on the higher performance aeroengine
  本文旨在对冲击-发散复合冷却技术开展机理和基础性研究,研究成果可应用于更高推重比级发动机预研。
• With the development of multi - variable control technology and aero - propulsion technology , future excellent engine must have the character , which is high ratio in thrust and weight low fuel and long use life . therefore the control system of aero - engine has also been becoming more and more complicated . the precision of control system is also extra higher
  随着高推重比、低油耗、长使用寿命、高机动性航空发动机的研制，现代航空发动机需要控制的变量越来越多、精度越来越高，因此，航空发动机控制系统变得越来越复杂，传统的航空发动机控制系统是采用机械液压控制。
• Compress disk is the very important rotational component in the areoengine . when the compress disk is working , the grads of temperature and stress between the rim and the center of the disk are great . in order to raise the thrust - weight ratio of the disk and reduce oil consumption . the best prospective way is the dual alloys disk used
  压气机盘是航空发动机上一个很重要的转动部件，压气机盘工作时，轮缘和轮毂温度梯度和应力梯度较大，为了提高飞机发动机推重比、减低耗油量，要求压气机盘的工作温度、使用性能更高，双合金盘制造是最有发展前景的技术。

• 推重比的日语：推力重量比