device for sealing the aircraft when landing on the water, and final canal system regulation of air pressure in the u0433u0435u0440u043cu043eu043au0430u0431u0438u043du0435 aircraft u0430u043fu043fu0430u0440 ata

摘要

1.device for sealing the aircraft when landing on the water stop body, containing a channel for the valve system of u0440u0435u0433u0443u043bu0438u0440u043eu0432 prom aniyah, air pressure in the u0433u0435u0440u043cu043eu043au0430u0431u0438u043du0435 and clamps the stop body in open - and closed the fly, differing in thatto improve the reliability of its work by increasing over efforts to u0437u0430u043fu043eu0440u043du043eu043c body in the u043fu0440u0438u0432u043eu0434u043du0435u043du0438u0438, the locking body is in the form of a turning ships u0440u043au0438, strengthened at the lower part of the external surface of the aircraft.the front side of the handle about the direction of flight attached to the outer hull of the spacecraft through the u043fu0435u0442u043bu0435u0432u043eu0433u043e hinge with u043fu043eu043fu0435u0440u0435u0447 noah u0432u0440u0430u0449u0435u043du0438u044f.2 axis. device for p.1, different topics, with the aim of reducing the aerodynamic resistance, located in front of the wall of the channel is executed under mutually a prom working with her in the closed position of the doors as well as auxiliary equipment, which in the open position is flush with the u043eu0431u0448u0438u0432u043au043eu0439 aircraft u0430u043fu043fu0430u0440u0430u0442u0430.3. device for the ap.1 and 2, differing, however, that, in order to enable the management of the system failure of pressure regulation, the flap is provided with transmission device closure with cable p u0440u043eu0432u043eu0434u043au043eu0439.4.senior channel system to regulate air pressure in the u0433u0435u0440u043cu043eu043au0430u0431u0438u043du0435 aircraft containing duct with u043au0440u0438u0432u043eu043bu0438u043du0435u0439u043du044bu043cu0438 walls connecting the exit a separate opening in the outer hull with located ahead of him on the direction of the valve system for regulating the pressure u043fu043eu0434u043au043bu044eu0447u0435 u043du043du043eu0439 static pressure to the receiver and to the u0441u043eu043eu0431u0449u0435u043du043du043eu043cu0443 atmosphere u0448u0442u0443u0446u0435u0440u0443,with the fact that, in order to enhance its efficiency by reducing the aerodynamic resistance, an airway is monotonous u0441u0443u0436u0430u044eu0449u0438u043cu0441u044f from to u0435u043bu044cu043du043eu0433u043e valve to the outbound inlet on the distance between the front and rear walls with regard to the direction of flight, portions of which are located in front of the u044bu0445u043eu0434u043du044bu043c aperture.installed in the direction of u043au0430u0441u0430u0442u0435u043bu044cu043du044bu0445 to relevant sections of these walls, the executive u043au043bu0430u043fu0430u043du043eu043c.5. senior valve for paragraph 4, with the fact that, in order to improve the technology and service reliability of pressure regulation, the front u0441u0442u0435u043du043a and the duct mounted tangentially to the outer hull, designed as a turning u0441u0442u0432u043eu0440u043au0438.6.prom the on clause 5, a fact that a static pressure and connected with the atmosphere of a pipe installed on the rear of direction at the duct wall of the turning wing.