TANDEM flapping wings DEVICE WITH AUTOMATIC CYCLIC twist and roll control

摘要

1.the device u043cu0430u0448u0443u0449u0438u0445 towards each other u0442u0430u043du0434u0435u043cu043du043e - located wings aircraft drive containing soft in torsion u043au0440u044bu043bu044cu00a0 and united in u043fu0440u043eu0442u0438u0432u043eu0444u0430u0437u0435 oscillating u0448u0430u0442u0443u043du043du043e - u043au043eu0440u043eu043cu044bu0441u043bu043eu0432u044bu0435 mechanisms u0434u0432u0443u043fu043bu0435u0447u0438u043cu0438 levers - u043au043eu0440u043eu043cu044bu0441u043bu0430u043cu0438 which u00a0u0432u043bu00a0u044eu0442u0441u00a0 u043bu043eu043du0436u0435u0440u043eu043du044b or the edges of the wings, which u0442u0440u0435u0445u0448u0430 u0440u043du0438u0440u043du044bu0435 mechanisms as the connecting rods are, in fact u043cu0430u0445u043eu0432u043eu0435 movementand the automatic of the twist of the u043cu0430u0445u0430u043du0438u00a0 u0434u043bu00a0 u043eu0431u0435u0441u043fu0435u0447u0435u043du0438u00a0 optimal angles of attack on the scale sections, with the possibility of the progressive movement vig wings "back and forth" along the axis u043cu0430u0445u0430u043du0438u00a0, causing a u0441u0432u00a0u0437u0430u043du043du044bu0445 with them u0442u0440u0435u0445u0448u0430u0440u043du0438u0440u043du044bu0445 u0448u0430u0442u0443u043du043eu0432 around the fingers u043au0440u0438u0432u043eu0448u0438u043fu043eu0432 and, respectively.additional, independent of the treatment u043cu0430u0445u0430u043du0438u00a0 or u043fu043bu0430u043du0438u0440u043eu0432u0430u043du0438u00a0 skewed wings around the axle u043du0430u043au043bu043eu043du00a0u044eu0449u0438u0445u0441u00a0 upper hinges u0448u0430u0442u0443u043du043eu0432.;2. device for u043eu0442u043bu0438u0447u0430u044eu0449u0435u0435u0441u00a0 1, so that the u043au0440u0435u043du0443 u0434u043eu0441u0442u0438u0433u0430u0435u0442u0441u00a0 progressively - u0432u0440u0430u0449u0430u0442u0435u043bu044cu043du044bu043cu0438 u043fu0435u0440u0435u043cu0435u0449u0435u043du0438u00a0u043cu0438 wings in a vertical u043fu043bu043eu0441u043a secant at symmetry of the guests through a beam components of suspension wings, causing a u0441u0432u00a0u0437u0430u043du043du044bu0445 with triangular u0448u0430u0442u0443u043du043eu0432 around the fingers u043au0440u0438u0432u043eu0448u0438u043fu043eu0432 and equipped u0442u0432u0435u043du043du043e wings around the u043du0430u043au043bu043eu043du00a0u044eu0449u0438u0445u0441u00a0 axes, skewed upper hinges u0448u0430u0442u0443u043du043eu0432.