system for pumping fuel, mainly in order to change the position of the center of gravity of a supersonic aircraft

摘要

a fuel pumping system mainly u0434u043bu00a0 u0438u0437u043cu0435u043du0435u043du0438u00a0 u043fu043eu043bu043eu0436u0435u043du0438u00a0 centre u0442u00a0u0436u0435u0441u0442u0438 supersonic aircraft u0441u043eu0434u0435u0440u0436u0430u0449u0430u00a0 u0446u0435u043du0442u0440u043eu0432u043eu0447u043du044bu0435 fuel tanks sensors u0443u0440u043eu0432u043du00a0, u0441u0432u00a0u0437u0430u043du043du044bu0435 between a pumping line, connected with the u0441u0442u0440u0443u0439u043du044bu043cu0438 pumps installed in the tanks and operating at high u0434u0430u0432u043b fuel u0435u043du0438u00a0 released from the motor pump and the discharge tank.u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0 so that, with a view to u0441u043du0438u0436u0435u043du0438u00a0 hours u0432u044bu043fu043eu043bu043du0435u043du0438u00a0 system u0443u043cu0435u043du044cu0448u0435u043du0438u00a0 her weight and u043fu043eu0432u044bu0448u0435u043du0438u00a0 reliability, on the main line pumping a tre u0445u043fu043eu0437u0438u0446u0438u043eu043du043du044bu0439 faucet that funnels u043fu0435u0440u0435u043au0430u0447u0438u0432u0430u0435u043cu043eu0435 fuel tank with an increase in u0440u0430u0441u0445u043eu0434u0443u0435u043cu044bu0439 allowable u0443u0440u043eu0432u043du00a0 in u0437u0430u043fu043eu043bu043du00a0u0435u043cu043eu043c u0446u0435u043du0442u0440u043eu0432u043eu0447u043du043eu043c tank, and u0441u043bu0438u0432u043du043eu043c pipeline e is a limit flow u0441u043bu0438u0432u0430u0435u043cu043eu0433u043e fuelu0443u043fu0440u0430u0432u043bu00a0u0435u043cu044bu0439 sensor u0443u0440u043eu0432u043du00a0.