伞舱系统,parachute-cabin system
1)parachute-cabin system伞舱系统
1.The model of theparachute-cabin system was built with the riser being of rigidity or elasticity,which was applied for simulating the system of Soyuz.建立了伞舱系统刚性连接和弹性连接时的数学模型,针对联盟号飞船回收系统进行了动力学仿真。
英文短句/例句
1.Influence of Character of Parachute on Stability of Parachute-cabin System降落伞特性对伞舱系统运动稳定性的影响
2.crude oil washing原油洗舱原油洗舱系统
3.Testing System and Course Simulation of Parachute Opening and Landing Shock;伞兵伞开伞、着陆过载测试系统及过程仿真
4.gas smothering system in cargo hold货舱惰气灭火系统货舱气体灭火系统
5.cargo oil thermal oil heating system货油舱热油加热系统
6.active roll tank system主动式减摇水舱系统
7.electronic tank level indication system油舱电子液位指示系统
8.cockpit temperature regulating system驾驶舱温度调节系统
9.cockpit pressure regulating system驾驶舱压力调节系统
10.bilge pumping and draining system舱底污水泵及排水系统
11.bilge and ballast piping system舱底水和压载水系统
12.ballast water treatment system压舱油污水处理系统
13.life support system in the closed cabin密闭舱生命保证系统
14.gas smothering system in cargo space货舱气体窒息灭火系统
15.automatic control system for unattended engineroom无人机舱自动控制系统
16.cargo oil steam heating system货油舱蒸汽加热系统
17.dedicated clean ballast tank system专用清洁压载舱系统
18.towed bird AEM systems吊舱式航空电磁系统
相关短句/例句
parachute-mass system伞物系统
1.Concerning that the characteristics change of movingparachute-mass system exerts an influence on the heavy items air-dropa,model of the heavy cargo air-drop system was established,the parachutes’ movement characteristics were analyzed,and the efficiency formula of theparachute-mass system was given.针对重物空投时伞物系统运动特征变化影响空投质量,建立了重物空投着陆系统模型,对降落伞的运动特性进行了分析,给出了伞物系统的效率计算公式,并进行了仿真。
3)aircraft-parachute system机伞系统
1.This paper discusses the position and gesture of the recovery motion for a small UAV,analyzes the dynamic relation between the aircraft and the parachute,and establishes a mathematical model of theaircraft-parachute system during the parachute landing program.通过分析机伞间的力学关系,建立了机伞系统运动模型,并进行了仿真分析,给出了无风情况下回收运动的仿真结果。
4)parachute-bomb伞弹系统
1.In order to find a suitable analysis method for the aerodynamic properties ofparachute-bomb system,the external flow field of the terminal guidance submunition decelerated by the parachute system is simulated in this paper.为了探寻一种适用于降落伞减速的灵巧子弹伞弹系统的气动特性数值仿真方法,本文针对某子弹及伞采用有限体积法求解不可压流的N-S方程,K-ERNG湍流模型,对其外流场特性进行了数值仿真分析计算,仿真结果与理论分析及试验结果基本一致,表明该方法对具有伞弹系统的子弹外流场的数值仿真是有效可行的,可以近似模拟风洞试验。
5)body-parachute system物伞系统
1.For the air-separation process of air-launch vehicle from the carrier aircraft,this paper gives out the unified model that is the rigid body-mass point model of thebody-parachute system.对运载器与载机分离过程的几个阶段采用统一模型进行研究,建立了分离过程物伞系统的刚体-质点模型。
6)man parachute system人伞系统
1.This paper built up a kinematic mathematical model for aman parachute system Theman parachute system was analyzed and calculated Security measures duing ejecting rescue on high altitude plateau areas were pointed ou建立了人伞系统的运动数学模型 ,对某型飞机К - 36 ДМ弹射座椅的人伞系统运动进行了分析计算 ,指出了在大海拔高原地区弹射救生中的安全性措施。
延伸阅读
吡啶烷基衍生物蒸馏残余物氯化苄季铵化物CAS：97375-31-0中文名称：吡啶烷基衍生物蒸馏残余物氯化苄季铵化物英文名称：Pyridine, alkyl derivs., distn. residues, benzyl chloride-quaternized
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