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DEVICE FOR DISPLACING MODEL OF CABIN OF PILOTAGE BED

机译:排水床舱位模型的装置

摘要

the invention u043eu0442u043du043eu0441u0438u0442u0441u00a0 to aviation technology, in particular to u043fu0438u043bu043eu0442u0430u0436u043du044bu043c stand and u0442u0440u0435u043du0430u0436u0435u0440u0430u043c u0434u043bu00a0 training flight personnel. the approximation conditions u0432u043eu0441u043fu0440u043eu0438u0437u0432u0435u0434u0435u043du0438u00a0 the overload to the u043du0430u0442u0443u0440u043du044bu043c by u0443u0432u0435u043bu0438u0447u0435u043du0438u00a0 range of displacements of a cabin.the device provides a linear u043fu0435u0440u0435u043cu0435u0449u0435u043du0438u00a0 cabin layout 1 u043fu0438u043bu043eu0442u0430u0436u043du043eu0433u043e stand in u043du0430u043fu0440u0430u0432u043bu0435u043du0438u00a0u0445 vertical axis y and the horizontal axis z, and the angular u043fu0435u0440u0435u043cu0435u0449 by around a horizontal axis x 1. the cabin is connected with the upper u0448u0435u0441u0442u0438u0433u0440u0430u043du043du043eu0439 hard edge 2 side, and the line 3 is installed on the lower u0448u0435u0441u0442u0438u0433u0440u0430u043du043du043eu0439 prisms of the 4 u043fu0438u043bu043eu0442u0430u0436u043du043eu0433u043e stand.u0432u0435u0440u0445u043du00a0u00a0 and u043du0438u0436u043du00a0u00a0 prisms have a common line 5. all the side edges 6 of both prisms, as well as the verge 2, 3 and 5 u0441u0432u00a0u0437u0430u043du044b between a planetary u0448u0430u0440u043du0438u0440u0430u043cu0438 7, the axis of which are mutually parallel and u00a0u0432u043bu00a0u044eu0442u0441u00a0 ribs both prize m. the ribs of each prism in pairs in one u0441u0432u00a0u0437u0430u043du044b u0448u0430u0440u043du0438u0440u0430u043cu0438 8 with u0433u0438u0434u0440u043eu0446u0438u043bu0438u043du0434u0440u0430u043cu0438 9 of their movements.the layout of the cabin 1 is surrounded by a screen 10 provided at the edge of the prism 2 and is equipped with additional devices 11 moves in the u043fu0438u043bu043eu0442u0430u0436u043du043eu0433u043e are u0432u0445u043eu0434u00a0u0449u0438u043cu0438 yeah. 2). (l, c
机译:u043e u0442 u043d u043e u0441 u0438 u0442 u0441 u00a0尤其是航空技术,尤其是 u043f u0438 u043b u043e u0442 u0430 u0436 u043d u043d u044b u043c u0442 u0440 u0435 u043d u0430 u0436 u0435 u0440 u0430 u043c u0434 u043b u00a0训练飞行人员。近似条件 u0432 u043e u0441 u043f u0440 u043e u0438 u0437 u0432 u0435 u0434 u0435 u043d u043d u0438 u00a0对 u043d u0430 u0442 u0443 u0440 u043d 的重载 u0443 u0432 u0435 u043b u0438 u0447 u0435 u043d u0438 u00a0的位移范围。设备提供了线性 u043f u0435 u0440 u0435 u043c u043c u0435 u0449 u0435 u043d u0438 u00a0机舱布局1 u043f u0438 u043b u043e u044e u0442 u0430 u0436 u043d u043e u043e u0433 u043e站在 u043d u0430 u043f u0440 u0430 u0432 u043b u0435 u043d u0438 u00a0 u0445垂直轴y和水平轴z,以及角度 u043f u0435 u0440 u0435 u043c u0435 u0449通过围绕水平轴x 1进行连接。 u0448 u0435 u0441 u0442 u0438 u0433 u0440 u0430 u043d u043d u043e u0439硬边2侧,并且第3行安装在下部 u0448 u0435 u0441 u0442 u0442 u0438 u0433 u0440 u0430 u043d u043d u043e u0439 4个棱镜 u043f u0438 u043b u043e u0442 u0430 u0436 u043d u043e u043 3 u043e支架。 u0432 u0435 u0440 u0445 u043d u00a0 u00a0和 u043d u0438 u0436 u043d u00a0 u00a0棱镜都有一条共同的线5。两个棱镜的所有侧边6也作为行星 u0448 u0430 u0440 u043d u0438 u0440 u0430 u043c u0438 7之间的边缘2、3和5 u0441 u0432 u00a0 u0437 u0430 u043d u044b相互平行且 u00a0 u0432 u043b u00a0 u044e u0442 u0441 u00a0的肋骨都奖励m。每个棱镜的肋骨成对 u0441 u0432 u00a0 u0437 u0430 u043d u044b u0448 u0430 u0440 u043d u0438 u0440 u0430 u043c u0438 8和 u0433 u0438 u0434 机舱1的布局被位于棱镜2边缘的屏幕10围绕着,并且它们的机芯9的运动。配备了其他设备的 u043f u0438 u043b u043e u0442 u0430 u0436 u043d u043e u0433 u043e中的11个移动是 u0432 u0445 u043e u0434 u00a0 u0449 u0438 u043c u0438是。 2)。 (l,c

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