Engines, internal combustion HURRICANE

摘要

1.engine internal u0441u0433u043eu0440u0430u043du0438u00a0 as engines of internal u0441u0433u043eu0440u0430u043du0438u00a0 with u043au043eu043bu0435u043du0447u0430u0442u044bu043c shaft, u0441u043eu0441u0442u043eu00a0u0449u0438u0439 of corps, still under the cylinder, in which ra based on the piston with u0448u0430u0442u0443u043du043eu043c, u0438u043cu0435u0435u0442u0441u00a0 crankshaft, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 from engines with internal u0441u0433u043eu0440u0430u043du0438u00a0 u043au043eu043bu0435u043du0447u0430u0442u044bu043c shaft so that the body 1 is made in the form of engines with horizontal groundknee u043au043eu043bu0435u043du0447u0430u0442u043eu0433u043e shaft 5 is not parallel to the axis u043au043eu043bu0435u043du0447u0430u0442u043eu0433u043e shaft 5, and the angle of the lower part of the connecting rod 7 u043au0440u0435u043fu0438u0442u0441u00a0 to u00a0u043au043eu0440u044e 2, which is connected with the u043au043eu043bu0435u043du0447u0430u0442 ies shaft 5; u00a0u043au043eu0440u044c 5 in the form of u0443u0441u0435u0447u0435u043du043du043eu0433u043e cone, the centre of which is to u043au0430u0440u0434u0430u043du043du043eu0439 u043eu0441u043du043eu0432u0430u043du0438u00a0 cradle 9 - 1 on the basis of the shell 1, the u00a0u043au043eu0440u00a0 2 located under the a. a crowbar to the horizontal base of the casing 1.one edge of the u00a0u043au043eu0440u00a0 2 u043fu043eu0441u0442u043eu00a0u043du043du043e u043au0430u0441u0430u0435u0442u0441u00a0 located on the basis of reference 1, the rim 3, that's hooked u0437u0443u0431u044cu00a0u043cu0438 located at the bottom of the u043eu0441u043du043eu0432u0430u043du0438u00a0 u00a0 u043au043eu0440u00a0 2 and the upper part of the support rim 3 radially; the rim 3 is located on the roller 12 corps 1 horizontally, u0437u0443u0431u044cu00a0u043cu0438 located vertically on the inside the circumference of the rim 3 u0441u0432u00a0u0437u0430u043d outpost with u0437u0443u0431u044cu00a0u043cu0438 regulatory u0448u0435u0441u0442u0435u0440u043du0438 4the lower part of the axis is fixed in the base u043au043eu0442u043eu0440u0430u00a0 casing 1, and the upper is an 11 point is located between the rim 3 and u043au043eu043bu0435u043du0447u0430u0442u044bu043c shaft 5, which u0437u0430u0446u0435u043fu043bu0435u043du0430 zu u0431u044cu00a0u043cu0438; crankshaft 5 passes through the hull 1 vertically, is located in the upper part of the knee, the knee upper part passes through the through hole along the u00a0u043au043eu0440u00a0 2 virtual axis u00a0u043au043eu0440u00a0 2the piston 6 is attached to the u0448u0430u0442u0443u043du0443 7 through u043au0430u0440u0434u0430u043du043du043eu0439 u043au0440u0435u0441u0442u043eu0432u0438u043du044b 9 - 2, a connecting rod 7 at the bottom u043au0440u0435u043fu0438u0442u0441u00a0 to paw u00a0u043au043eu0440u00a0 2 - 1 through u043au0430u0440u0434u0430u043du043du043eu0439 u043au0440u0435u0441u0442u043eu0432u0438u043du044b 9 - 3, the piston 6 and the connecting rod 7 str u0441u043eu0431u043du044b u0434u0432u0438u0433u0430u0442u044cu0441u00a0 a move in the vertical direction, u043au0430u0447u0430u00a0 u00a0u043au043eu0440u044c 2, u0432u0435u0440u0445u043du00a0u00a0 part which rotates with the crankshaft 5, u043du0438u0436u043du00a0u00a0 part rotates on the u043fu043eu0440u043du044bu0439 rim 3, the rim 3 turns on the gears and 4u0440u0435u0433u0443u043bu0438u0440u0443u044eu0449u0430u00a0 u0448u0435u0441u0442u0435u0440u043du00a0 4 rotates the crankshaft 5.;2.aircraft with engine internal u0441u0433u043eu0440u0430u043du0438u00a0 has the casing 1, the crankshaft 5 of the rim 3, regulatory mechanism, u00a0u043au043eu0440u044c 2, in the plane is u0438u00a0 u00a0u043au043eu0440u00a0 2 radially u043au0440u0435u043fu00a0u0442u0441u00a0 reiki 2 - 2, to which the u043au0440u0435u043fu00a0u0442u0441u00a0 blades 13, 14, the u043au0440u0435u043fu0438u0442u0441u00a0 stabilizer 15,when the device u0434u0432u0438u0433u0430u0442u0435u043bu00a0 internal u0441u0433u043eu0440u0430u043du0438u00a0 is consistent back forward movement u0440u0435u0435u043a 2 - 2 in the vertical u043du0430u043fu0440u0430u0432u043b u0435u043du0438u0438, with the blades 13 are u0432u044bu043fu043eu043bu043du00a0u0442u044c function valves - up u0440u0435u0435u043a 2 - 2 in the upright position, u043fu0440u043eu043fu0443u0441u043au0430u00a0 air and lowering u0440u0435u0435u043a 2 - 2 u0437u0430u043du0438u043cu0430 horizontal position by pushing air downu043fu043eu0434u043du0438u043cu0430u00a0 device up.