首页>
外国专利>
FAR search and rescue amphibious floatplane tri-pattern layout 'frigate'
FAR search and rescue amphibious floatplane tri-pattern layout 'frigate'
展开▼
机译:FAR搜索和救援两栖水上飞机三模式布局“护卫舰”
展开▼
页面导航
摘要
著录项
相似文献
摘要
the search and rescue u043fu043eu043fu043bu0430u0432u043au043eu0432u044bu0439 seaplane - u0430u043cu0444u0438u0431u0438u00a0 u0442u0440u0438u043cu0430u0440u0430u043du043du043eu0439 layout scheme designed u0434u043bu00a0 u0441u043fu0430u0441u0435u043du0438u00a0 people u0442u0435u0440u043fu00a0u0449u0438u0445 disaster at sea at the roughness of the water surface to 4 points, containing u0444u044eu0437u0435u043bu00a0u0436, wing with mechanization as u043fu0440u0435u0434u043au0440u044bu043bu043au043eu0432, flap setting, u0438u043du0442u0435u0440u0446u0435u043fu0442u043eu0440u043eu0432, primed u0432u0438u043du0442u043eu0432u0435u043du0442u0438u043bu00a0u0442u043eu0440u043du044bu0435 no u0430u0442u0435u043bu0438, tail feathers, wheeled chassis, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 orderthe u0433u0438u0434u0440u043eu0441u0430u043cu043eu043bu0435u0442u0435 u0443u0441u0442u0430u043du0430u0432u043bu0438u0432u0430u044eu0442u0441u00a0: u0434u0435u043bu044cu0442u0430u0441u0442u0440u0435u043bu043eu0432u0438u0434u043du043eu0435 wing with missing console apps u043fu043eu0434u043au0440u044bu043bu044cu043du044bu043cu0438 scenarios with a positive angle of a v, centro the plan which distributed on the whole length of u0444u044eu0437u0435u043bu00a0u0436u0430 limited ribs u043au0438u043bu0435u0439, u00a0u0432u043bu00a0u0435u0442u0441u00a0 main bearing design element of the plane, u0441u0432u00a0u0437u044bu0432u0430u044eu0449u0438u043c in ed design: a u0444u044eu0437u0435u043bu00a0u0436, floats,u0431u0435u0437u043au043eu043du0441u043eu043bu044cu043du044bu0439 stabilizer and u0434u0432u0443u0445u043au0438u043bu0435u0432u043eu0435 reverse sweep tail feathers, which are installed on the u043au0438u043bu00a0u0445 two extendable u0432u0438u043du0442u043eu0432u0435u043du0442u0438u043bu00a0u0442u043eu0440u043du044bu0445 u0434u0432u0438u0433u0430u0442u0435u043bu00a0,;three long float u043au0438u043bu0435u0432u0430u0442u043du043eu0439 form, established under the u0446u0435u043du0442u0440u043eu043fu043bu0430u043du043eu043c on u0442u0440u0438u043cu0430u0440u0430u043du043du043eu0439 pattern design, not u0432u044bu0445u043eu0434u00a0u0449u0438u0435 for front edge wing, equipped with u0434u0435u043cu043f u0444u0438u0440u0443u044eu0449u0438u043cu0438 u0441u043au043eu043bu044cu0437u00a0u0449u0438u043cu0438 u0433u0438u0434u0440u043eu043bu044bu0436u0430u043cu0438 issued during takeoff, landing and u0443u0431u0438u0440u0430u0435u043cu044bu043cu0438 in flight;u043fu043eu043bu0443u0446u0438u043bu0438u043du0434u0440u0438u0447u0435u0441u043au0438u0439 fully hermetic u0444u044eu0437u0435u043bu00a0u0436 with u043au043eu043du0443u0441u043eu043eu0431u0440u0430u0437u043du043eu0439 front part, in which the u0440u0430u0437u043cu0435u0449u0430u044eu0442u0441u00a0 radar technical compartment with u0434u0432u0443u043cu00a0 u0434u0432u0438u0433u0430u0442u0435u043bu00a0u043cu0438 u043fu043eu0434u0434u0443u0432u0430 and ka bean crew bearing in front of the two additional u0440u0443u043bu00a0 height, its u043fu043eu043bu0443u0441u0444u0435u0440u043eu0439 u043du0430u043au043bu0430u0434u044bu0432u0430u0435u0442u0441u00a0 on top of u0446u0435u043du0442u0440u043eu043fu043bu0430u043d wing;u0448u0435u0441u0442u0438u0442u043eu0447u0435u0447u043du043eu0435 wheeled chassis, carts, which are stored in the compartments on each side floats, u0432u044bu043fu0443u0441u043au0430u044eu0442u0441u00a0 while landing on the airport surface u0431u0430u0437u0438u0440u043eu0432u0430u043du0438u00a0 and u0443u0431u0438u0440u0430 u044eu0442u0441u00a0 in flight;two internal catflap u0446u0435u043du0442u0440u043eu043fu043bu0430u043du0430 set in the aft part of the channel forming the air cushion by u0434u0432u0438u0433u0430u0442u0435u043bu00a0u043cu0438 u043fu043eu0434u0434u0443u0432u0430.
展开▼