首页> 外国专利> Monitoring system UNIT AUTONOMOUS propulsion system runaway rocket units With Marching propulsion system REPEATED START

Monitoring system UNIT AUTONOMOUS propulsion system runaway rocket units With Marching propulsion system REPEATED START

机译:监视系统单位自主推进系统失控火箭装置带有行进推进系统REPEATED START

摘要

1.the system u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 dumping block autonomous propulsion from u0440u0430u0437u0433u043eu043du043du043eu0433u043e missile block u043cu0430u0440u0448u0435u0432u043eu0439 motor installing multiple launch, ods u0435u0440u0436u0430u0449u0430u00a0 temporary device, block u0432u043au043bu044eu0447u0435u043du0438u00a0 u043cu0430u0440u0448u0435u0432u043eu0439 propulsion repeated start, block u0432u044bu043au043bu044eu0447u0435u043du0438u00a0 autonomous propulsion, block) u044eu0447u0435u043du0438u00a0 executive elements of the system.connected to the actuating elements of the system, u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0 because it introduced u0437u0430u0434u0430u0442u0447u0438u043a time u0432u043au043bu044eu0447u0435u043du0438u00a0 u043cu0430u0440u0448u0435u0432u043eu0439 propulsion u043cu043du043eu0433u043eu043au0440 u0430u0442u043du043eu0433u043e starts and the first block u0441u0440u0430u0432u043du0435u043du0438u00a0, one input of which is connected with the u0437u0430u0434u0430u0442u0447u0438u043au043eu043c time u0432u043au043bu044eu0447u0435u043du0438u00a0 u043cu0430u0440u0448u0435u0432u043eu0439 propulsion multiple launch, second - with a temporary devicea way to block u0432u043au043bu044eu0447u0435u043du0438u00a0 u043cu0430u0440u0448u0435u0432u043eu0439 propulsion multiple launching, the sensor and the u0437u0430u0434u0430u0442u0447u0438u043a u0434u0430u0432u043bu0435u043du0438u00a0 in cell u0441u0433u043eu0440u0430u043du0438u00a0 u043cu0430u0440u0448u0435u0432u043eu0439 propulsion m u043du043eu0433u043eu043au0440u0430u0442u043du043eu0433u043e launch, which is connected with the second block u0441u0440u0430u0432u043du0435u043du0438u00a0 exits, u043fu0435u0440u0432u0430u00a0 scheme and one input of which is connected with a motor u0432u043au043bu044eu0447u0435u043du0438u00a0 u043cu0430u0440u0448u0435u0432u043eu0439 cs u0442u0430u043du043eu0432u043au0438 repeated start, and the other is connected to the second block u0441u0440u0430u0432u043du0435u043du0438u00a0,the first way is connected with the u0432u044bu043au043bu044eu0447u0435u043du0438u00a0 autonomous propulsion, and the second way is to counter the number of launches u043cu0430u0440u0448u0435u0432u043eu0439 motor u0443u0441u0442u0430u043d u043eu0432u043au0438 multiple launching, the third block u0441u0440u0430u0432u043du0435u043du0438u00a0 entrance which is connected with the meter, the first number of launches u043cu0430u0440u0448u0435u0432u043eu0439 propulsion multiple u0437u0430u043fu0443 ska,a second entrance on the number of launches u0437u0430u0434u0430u0442u0447u0438u043au043eu043c u043cu0430u0440u0448u0435u0432u043eu0439 propulsion system of multiple launch u0441u0440u0430u0432u043du0435u043du0438u00a0 fourth block, which is connected to the bottom first. u0442u0447u0438u043au043eu043c u0434u0430u0432u043bu0435u043du0438u00a0 in cell u0441u0433u043eu0440u0430u043du0438u00a0 autonomous propulsion unit, and a second entrance from a u0434u0430u0432u043bu0435u043du0438u00a0 cell autonomous manipulators u0441u0433u043eu0440u0430u043du0438u00a0 cluster whisker u0442u0430u043du043eu0432u043au0438, u0432u0442u043eu0440u0430u00a0 scheme andthe first door which is connected with the exit of the third block u0441u0440u0430u0432u043du0435u043du0438u00a0, second entry with a u0432u044bu043au043bu044eu0447u0435u043du0438u00a0 autonomous propulsion, and the third entry - exit. u0432u0435u0440u0442u043eu0433u043e u0441u0440u0430u0432u043du0435u043du0438u00a0 block, and the outlet and is connected to the second circuit block u0432u043au043bu044eu0447u0435u043du0438u00a0 executive elements of the system, which provides the signals to the executive element the system reset.
机译:1.系统 u0443 u043f u0440 u0430 u0432 u043b u0435 u043d u0438 u00a0自 u0440 u0430 u0437 u0433 u043e u043d u043d u043d u043e u0433 u043e导弹的自卸推进块块 u043c u0430 u0440 u0448 u0435 u0432 u043e u0439电机安装多个发射装置,ods u0435 u0440 u0436 u0430 u0449 u0430 u00a0临时设备,块 u0432 u043a u043b u044e u0447 u0435 u043d u0438 u00a0 u043c u0430 u0440 u0448 u0435 u0432 u043e u0439重复启动,阻止 u0432 u044b u043a u043b u044e u0447 u0435 u043d u0438 u0438 u044e u0447 u0435 u043d u0438 u00a0与系统的执行元件连接, u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0430 u00a0 u0441 u00a0,因为它引入了 u0437 u0430 u0434 u0430 u0442 u0447 u0438 u043a时间 u0432 u043a u043b u044e u0447 u0435 u0435 u043d u0438 u00a0 u043c u0430 u0448 u0435 u0432 u043e u0439推进 u043c u043d u043e u0433 u043e u043a u0440 u0430 u0442 u043d u043e u0433 u043e开始,第一个块 u0441 u0440 u0430 u0432 u043d u0435 u043d u0438 u00a0,其中一个输入与 u0437 u0430 u0434连接 u0430 u0442 u0447 u0438 u043a u043e u043c时间 u0432 u043a u043b u044b u044e u0447 u0435 u043d u043d u0438 u00a0 u043c u0430 u0440 u0440 u0448 u0435 u0432 u043e u043e多次发射,第二次-使用临时装置阻止 u0432 u043a u043b u044e u0447 u0435 u043d u043d u0438 u00a0 u043c u0430 u0440 u0448 u0435 u0432 u0432 u043e u0439多次发射传感器和单元格 u0441 u0433 u043d u0438 u00a0中的 u0437 u0430 u0434 u0430 u0442 u0447 u0438 u043a u0434 u0430 u0432 u043b u043b u0434 u043d u0438 u00a0 u043c u0430 u0440 u0448 u0435 u0432 u043e u043e u0439推进力m u043d u043e u0433 u043e u043e u043a u0440 u0430 u0442 u0432 u043d u043e u0433 u043e启动与第二个块连接的 u0441 u0440 u0430 u0432 u043d u0435 u043d u0438 u00a0出口, u043f u0435 u0440 u0432 u0430 u00a0 sc血红素和一个输入端与一台电机 u0432 u043a u043b u044e u0447 u0435 u043d u043d u0438 u00a0 u043c u0430 u0440 u0448 u0435 u0432 u0432 u043e u0439 cs u0442 u0430 u043d u043e u0432 u043a u0438重复启动,另一个连接到第二个块 u0441 u0440 u0430 u0432 u043d u0435 u043d u0438 u00a0,第一种方法与 u0432连接 u044b u043a u043b u044e u0447 u0435 u043d u0438 u00a0自动推进,第二种方法是计算发射次数 u043c u0430 u0440 u0448 u0435 u0432 u0432 u043e u0439电机 u0443 u0441 u0442 u0430 u043d u043e u0432 u043a u0438多次启动,第三个块 u0441 u0440 u0430 u0432 u043d u0435 u043d u0438 u00a0与仪表相连的入口,第一个发射次数 u043c u0430 u0440 u0448 u0435 u0432 u043e u0439推进倍数 u0437 u0430 u043f u0443 ska,发射次数的第二个入口 u0437 u0430 u0434 u0430 u0442 u0447 u0438 u043a u043e u043c u043c u0430 u0440 u0448 u0435 u0432 u043e u0439多重发射的推进系统 u0441 u0440 u0430 u0432 u043d u0435 u043d u0438 u00a0第四块,该块首先连接到底部。 u0442 u0447 u0438 u043a u043e u043c u0434 u0430 u0432 u043b u0435 u043d u0438 u00a0在单元格 u0441 u0433 u043e u0440 u0430 u043d u043d u0438 u00a0中,自主推进单元来自 u0434 u0430 u0432 u043b u0435 u043d u0438 u00a0单元自治操纵器 u0441 u0433 u043e u0440 u0430 u043d u0438 u00a0群集晶须 u0442 u0430 u0430 u043d u043e u0432 u043a u0438, u0432 u0442 u043e u0440 u0430 u00a0方案以及与第三个街区 u0441 u0440 u0430 u0432 u043d u043d u0435 u043d u0438的出口相连的第一扇门 u00a0,第二个条目具有 u0432 u044b u043a u043b u044e u0447 u0435 u043d u0438 u00a0自主推进,而第三个条目-退出。 u0432 u0435 u0440 u0442 u043e u0433 u043e u0441 u0440 u0430 u0432 u043d u0435 u043d u0438 u00a0块,并且插座与第二个电路块 u0432 u043a 连接u043b u044e u0447 u0435 u043d u0438 u00a0系统执行元件,该信号向执行元件重置系统。

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