thrust vt. (thrust) 1.猛推,冲;猛揿,冲入,插入,推入(出),突出,伸出,塞,刺,戳,戳穿。 2.逼迫,把[将]…强加于… (into)。 3.突然提出,不恰当地插进(插嘴等)。 vi. 1.推,冲;强行推入,冲入;强行推进,突进;冲过去。 2.挺伸,延伸。 thrust one's hand into one's pocket 将手插进口袋里。 thrust one's way through a crowd 冲过人群。 It's not time for you to thrust in a question now. 现在轮不到你插嘴提问题。 It was John who thrust a person aside. 是约翰把一个人猛推在一旁的。 Unexpected events thrust themselves continually athwart our path. 在我们工作的进程中,出乎意料的事层出不穷。 After he invented the new drilling machine, honours were thrust upon him. 他发明了新的钻机之后,许多荣耀都加在他的身上了。 He showed great reluctance to accept the responsibility thrust upon him. 对强加给他的责任,他不乐于承担。 thrust at sb. with a dagger 以匕首戳人。 thrust on one's gloves 急忙带上手套。 thrust through 挤过。 be thrust into fame 突然出名。 thrust a hand in 插手,干预。 thrust aside 推开。 thrust home 把(短刀等)深深刺入。 thrust (sth.) (up)on (sb.) (将东西)推给(某人);强卖给(某人)。 thrust oneself forward = thrust oneself in=thrust one's nose in 探听;插嘴;出头,干涉。 thrust one's way 向前推进,勉强挤过。 thrust out 推出;逐出,赶出;挤出,排出;发射。 n. 1.推,冲;刺。 2.攻击;苛评,讥刺。 3.【军事】突入,突击,冲锋;【机械工程】推力,侧向压力;【地质学;地理学】逆断层;冲断层;【矿物】煤柱压裂。 a reactive thrust 反冲力。 make a thrust with a dagger 用匕首冲刺。 the thrust and parry of A and B 甲乙两人间唇枪舌剑的激烈辩论[攻击]。
maximum n. (pl. maximums, -ma ) 极点,最大,最高,最高额,最大值;最高点;最大限度;【数学】极大(值)(opp. minimum)。 The excitement was at its maximum. 兴奋到极点。 adj. 最大的,最高的,顶点的,最多的。 maximum draught [draft] 【航海】最大吃水深度。 maximum obscuration 【天文学】蚀甚。 a maximum range 最大射程。 a maximum thermometer 最高温度计。
10 maximum thrust force of top drive power head 30 kn 10动力头最大给进力30 kn
10 maximum thrust force of top drive power head 15 kn 10动力头最大给进力15 kn
Maximum thrust force of top drive power head 15 kn 9动力头最大给进力kn 15
Stand by . we ' re going to maximum thrust 准备,我们要加速了
Hardware - in - loop simulating system of ifpc is built to research the digital simulations , which are conducted with two optimization modes : maximum thrust mode and minimum fuel consumption mode 构建了实物在回路的飞推综合控制仿真试验系统,进行了最大推力模式和最小油耗模式的优化仿真试验。
The conclusion that the optimal secondary nozzle exit area generating the maximum thrust agrees well with the numerical simulation , indicating that the exit area of secondary nozzle should be optimized according to structure and flow parameters during design 表明在引射火箭设计时,应结合引射火箭的结构和流动参数对二次喷管出口面积进行优化设计,以达到最佳推力性能。
Simulation results presented here demonstrate that during accelerating flight at constant altitude thrust increases up to approximately 12 percent in the maximum thrust mode , and at subsonic cruise specific fuel consumption decreases up to 2 percent in the minimum fuel consumption mode 试验结果表明两种优化模式下,飞推综合控制的优化算法可以显著提高发动机性能,也验证了该优化计算机设计方案是可行的。
The results indicate that with decrease of exit area of secondary nozzle , the bypass ratio is decreasing , and the static pressure in integrated ejector combustor is increasing , and mixing condition becomes better . there exists an optimal exit area of secondary nozzle to get maximum thrust of rocket ejector 结果表明:引射能力随着二次喷管出口面积的减小而减小;整体式引射燃烧室压强随着二次喷管出口面积的减小而上升,混合随之更为充分;存在一个最优的二次喷管出口面积,使发动机推力最大。