Heavy transport amphibious floatplane catamaran layout drawing

摘要

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de u043bu044cu0442u0430u0441u0442u0440u0435u043bu043eu0432u0438u0434u043du044bu043c wing, u0446u0435u043du0442u0440u043eu043fu043bu0430u043d whichdistributed in the whole length of the u0444u044eu0437u0435u043bu00a0u0436u0430, u00a0u0432u043bu00a0u0435u0442u0441u00a0 with constructive element in a single plane, u0441u0432u00a0u0437u044bu0432u0430u044eu0449u0438u043c design u0444u044eu0437u0435u043bu00a0u0436, u0434u0432u0443u0445u043au0438u043bu0435u0432u043eu0435 u0445u0432u043eu0441 u0442u043eu0432u043eu0435 empennage and nacelle floats, possessing high strength and color of primed engines from u0431u0440u044bu0437u0433u043eu0432u043eu0433u043e flow; u043fu043eu0434u0434u0443u0432u043eu043c under u0446u0435u043du0442u0440u043eu043fu043bu0430u043d u0434u0432u0438u0433u0430u0442u0435u043bu00a0 mi u043fu043eu0434u0434u0443u0432u0430 located in the foredeck. currently, the company develops in maintenancethat under the u0446u0435u043du0442u0440u043eu043fu043bu0430u043du043eu043c air cushion and u0441u0434u0443u0432u0430u044eu0449u0438u043c u043du0430u0431u0435u0433u0430u044eu0449u0443u044e wave; u0434u0432u0443u0445u043au0438u043bu0435u0432u044bu043c your tail feathers with u0441u0440u0435u0434u043du0435u0440u0430u0441u043fu043eu043bu043eu0436u0435u043du043du044bu043c form with stabilizer u0446u0435u043du0442u0440u043eu043fu043bu0430u043du043eu043c and u0444u044eu0437u0435u043bu00a0u0436u0435u043c solid design for the effective management of course; placing the extendable u0442u0443u0440u0431u043eu0440u0435u0430u043au0442u0438u0432u043du044bu0445 engines for stabilizer e the tail u043eu043fu0435u0440u0435u043du0438u00a0,what u0434u043eu0441u0442u0438u0433u0430u0435u0442u0441u00a0 protecting them from u0431u0440u044bu0437u0433u043eu0432u043eu0433u043e flux; the front part of the u0444u044eu0437u0435u043bu00a0u0436u0430 additional controls the height that currently, the company develops u0443u043fu0440u0430u0432u043bu00a0u0435u043cu043eu0441u0442u044c; u0430u043cu0444u0438u0431u0438 u0439u043du043eu0441u0442u044cu044e, u043au043eu0442u043eu0440u0430u00a0 u0434u043eu0441u0442u0438u0433u0430u0435u0442u0441u00a0 installation u0442u0440u0435u0445u0442u043eu0447u0435u0447u043du043eu0433u043e wheeled chassis, the chassis design of aircraft u0431u0430u0437u0438u0440u043eu0432u0430u043du0438u00a0 equal u0433u0440u0443u0437u043eu043fu043eu0434u044a shore u0435u043cu043du043eu0441u0442u0438; u043eu0442u043au0438u0434u044bu0432u0430u044eu0449u0435u0439u0441u00a0 toward a part of the u0444u044eu0437u0435u043bu00a0u0436u0430 aircraftcurrently, the company develops u043fu043eu0437u0432u043eu043bu00a0u044eu0449u0435u0439 to loading, unloading, with the front of the u0444u044eu0437u0435u043bu00a0u0436u0430; broad hemispheric u0444u044eu0437u0435u043bu00a0u0436u0435u043c, which u043du0430u043au043bu0430u0434u044bu0432u0430u0435u0442u0441u00a0 on top of u0446u0435u043du0442u0440u043eu043fu043bu0430 mr. wing, currently, the company develops u0443u0441u0438u043bu0438u0432u0430u00a0 structural strength.