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加油时间
相关语句
  refueling time
     Study on Method of Flow Mstching design Based on the Least Refueling Time
     基于加油时间最短的流量平衡设计方法研究
短句来源
     Based on the pipeline model of airplane pressure refueling system,we establish the mathematical model of the least refueling time.
     基于飞机地面压力加油系统管路模型 ,运用运筹学方法 ,建立了求取加油时间最短的数学模型 ,求觖得出只有在流量平衡的条件下 ,加油时间最短。
短句来源
     With optimal research,throught adding variable throttle apparatus to every branch pipe,the purpose was attained for the least refueling time regardless of the quantity of refueling fuel on a big aircraft ground pressure refueling system.
     针对飞机地面压力加油系统 ,为保证在任意加油量下 ,都能得到最短的加油时间 ,本文对加油系统进行优化研究 ,得出通过在各支路加装可变节流装置能实现这个目标。
短句来源
     Aiming at the problem of long refueling time of normal refueling quantity for one aircraft ground pressure refueling system,a new system optimal design method was proposed.
     针对某型飞机地面压力加油系统存在的常用加油量加油时间过长的问题,提出了一种新的系统优化设计方案。
短句来源
  “加油时间”译为未确定词的双语例句
     Sealing rings have run for 2650 hours, oil saving may be 20kg per year in a decelerator, and environment is improved.
     密封圈已运转2650h,使用寿命将远大于此值。 每年每台可节油20kg多,还改善了环境和维修加油时间等。
短句来源
     Based on the pipe model of ground pressure - refueling system for aircratt,the optimizing target is obtained for refueling control. By using the integrated method of fuzzy conlrol and PID control. the desirab1e responsecurve is emulaied with the help of MATLAB software.
     本文针对给出的飞机地面压力加油系统管路模型 ,分析得出加油控制优化目标 ,利用模糊控制理论及PID控制相结合的方法 ,得到理想的离线仿真计算结果 ,应用于地面模拟试验 ,加油时间达到了预定要求
短句来源
     Firstly the number of assistant aircraft was supposed to be special value,like 1,2,3,4.Then a table of experimental data with more values and some figure were resulted,from which a general rule was lastly concluded.
     整个思路由浅入深,通过考虑辅机数目n分别为1,2,3,4的特殊情况进而探讨一般的规律,包括辅机在基地无加油时间和有加油时间以及主机在空中盘旋等不同假设条件下的复杂情况,并将统计出的数据列表对比,获得了更直观的认识.
短句来源
  相似匹配句对
     Time
     时间
短句来源
     Time is...
     时间
短句来源
     Study on Method of Flow Mstching design Based on the Least Refueling Time
     基于加油时间最短的流量平衡设计方法研究
短句来源
查询“加油时间”译词为用户自定义的双语例句

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  refueling time
For metal hydrides, weight, system volume and refueling time are the primary issues.
      
Refueling time must be minimized and propellant transfer rate maximized.
      


Five dynamic seals are designed to selve oil leakage in decelerator, and their optimum selections are double gland packing and labyrinth gland packing. Tests show that ideal structure is the combination of many types of seals and sealing material had best to take filling PTFE. Sealing rings have run for 2650 hours, oil saving may be 20kg per year in a decelerator, and environment is improved.

为解决减速器漏油设计了5种动密封装置,优选出双填料密封和迷宫填料密封,试验表明,以多种密封类型组合的结构较为理想;密封材料以填充聚四氟乙烯最好。密封圈已运转2650h,使用寿命将远大于此值。每年每台可节油20kg多,还改善了环境和维修加油时间等。

Based on the pipe model of ground pressure - refueling system for aircratt,the optimizing target is obtained for refueling control. By using the integrated method of fuzzy conlrol and PID control. the desirab1e responsecurve is emulaied with the help of MATLAB software. And through simulation test, the satisfied fefueling time is at-tained.\;

本文针对给出的飞机地面压力加油系统管路模型 ,分析得出加油控制优化目标 ,利用模糊控制理论及PID控制相结合的方法 ,得到理想的离线仿真计算结果 ,应用于地面模拟试验 ,加油时间达到了预定要求

Based on the pipeline model of airplane pressure refueling system,we establish the mathematical model of the least refueling time.On the maximum refueling pressure,we draw the conclusion that on condition that flow matches,refueling time can be least And through simulated test,the results show that the conclusion mentioned above is valid and feasible.

基于飞机地面压力加油系统管路模型 ,运用运筹学方法 ,建立了求取加油时间最短的数学模型 ,求觖得出只有在流量平衡的条件下 ,加油时间最短。系统研究的结果验证了该结论的正确性。

 
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