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Way to speed horizontal flight helicopter vibration reduction, increased efficiency and parries ROLLOVER AND DEVICE FOR ITS IMPLEMENTATION
Way to speed horizontal flight helicopter vibration reduction, increased efficiency and parries ROLLOVER AND DEVICE FOR ITS IMPLEMENTATION
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机译：加快水平飞行直升机减振，提高效率并招架的方法实施的过渡和装置
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摘要
1.method u043fu043eu0432u044bu0448u0435u043du0438u00a0 speed horizontal flight of the helicopter, u0441u043du0438u0436u0435u043du0438u00a0 vibrations u043fu043eu0432u044bu0448u0435u043du0438u00a0 economy and u043fu0430u0440u0438u0440u0443u044eu0449u0438u0439 u043eu043fu0440u043eu043au0438u0434u044bu0432u0430u043du0438u00a0, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, mode e horizontal flight at the helicopter include u0442u00a0u043du0443u0449u0438u0439,the thrust screw u0441u043du0438u043cu0430u00a0 function u0434u0432u0438u0436u0438u0442u0435u043bu00a0 with the rotor together with the swashplate u043fu0435u0440u0435u0432u043eu0434u00a0u0442 in high-speed flight mode in which the pen u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 general sha gaume u043fu0435u0440u0435u0432u043eu0434u00a0u0442 in situation of equal or below the u0432u0438u0441u0435u043du0438u00a0 with switch fuse switch speed.a common step in lowering u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 u043eu043fu0443u0441u043au0430u0435u0442u0441u00a0 and clip to u043eu0433u0440u0430u043du0438u0447u0438u0442u0435u043bu00a0 u043eu043fu0443u0441u043au0430u043du0438u00a0 located on the side of the advancing blades in u0430u0437u0438u043cu0443u0442u0435 0 - 180 and limiting u0430u044eu0449u0438u0439 decline angle attack the oncoming blades below the limit u043eu0431u0435u0441u043fu0435u0447u0435u043du0438u00a0 u0441u043eu0437u0434u0430u043du0438u00a0 lifting force, while further lowering the pens u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 general stepu0441u043au043eu043bu044cu0437u00a0u0449u0435u0433u043e rings and clips the leash u0442u00a0u043du0435u0442 u043eu0442u0441u0442u0443u043fu0430u044eu0449u0443u044e - u043fu0440u0438u0432u043eu0434u00a0 in negative angle along the u0432u0440u0430u0449u0435u043du0438u00a0 in between u0430u0437u0438u043cu0443u0442u0430 180 to 360 and the positive angle at aki to u043du0430u0431u0435u0433u0430u044eu0449u0435u043cu0443 air flow u0441u043eu0437u0434u0430u0432u0430u00a0 producing at u043eu0442u0441u0442u0443u043fu0430u044eu0449u0435u0439 blades, however, depending on the mode and speed of horizontal flight u0432u0435u0440u0442u043eu043b this reduces the speed of the rotor and the rotor u0432u0440u0430u0449u0435u043du0438u00a0 powerin this u0444u0443u043du043au0446u0438u00a0 u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 passes u0441u0442u0430u0431u0438u043bu0438u0437u0430u0442u043eu0440u0430u043c - u0440u0443u043bu00a0u043c height and rotation and to u0445u0432u043eu0441u0442u043eu0432u043eu043cu0443 wintu language, to further increase the speed of horizontal flight, with c spruce u0441u043eu0437u0434u0430u043du0438u00a0 lifting force to the rotor speed, rotor systems, and the blades u0441u0442u0430u0432u00a0u0442 under positive angle of attack u043du0430u0431u0435u0433u0430u044eu0449u0435u0433u043e air flow as well.;2. the device is the swashplate on p.1, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u0441u043au043eu043bu044cu0437u00a0u0449u0435u0435 ring u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 common step has a large amplitude u0445u043eu0436u0434u0435u043du0438u00a0 with lower reference limit the possibility of u0441u043eu0437u0434u0430u043du0438u00a0 autry the attack on the u0446u0430u0442u0435u043bu044cu043du043eu0433u043e u043bu043eu043fu0430u0441u0442u00a0u0445 rotor and brake u043eu043fu0443u0441u043au0430u043du0438u00a0 clips located on the side of the advancing blades in u0430u0437u0438u043cu0443u0442u0435 0 - 180and the speed switch located at the hands u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 common step.
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