METHOD OF CREATING AIRCRAFT LIFT (VERSIONS), METHOD OF FLIGHT, NON-AERODYNAMIC ALL-WEATHER VTOL AIRCRAFT MAXINIO (VERSIONS), METHODS OF TAKE-OFF AND LANDING, AICRAFT CONTROL METHOD AND SYSTEM, FUSELAGE, WING (VERSIONS), THRUST REVERSE AND METHOD OF ITS OPERATION, LANDING GEAR SYSTEM, GAS SEPARATION AND DISTRIBUTION SYSTEM

摘要

FIELD: aeronautical engineering. ^ SUBSTANCE: set of invention relates to aeronautical engineering. The methods of creating lift, taking off, flying and landing feature separation of air flow designed to produce opposite parts of jet thrust of blowing over the carrier surfaces. The aircraft comprises fuselage, power plant, air flow intake assembly and wing leading-edge air flow distributor. Fuselage includes the system of lines feeding air flow from the turbojet engine compressor to the aforesaid wing leading-edge air flow distributor. The wing comprises leading-edge air flow distributor. In compliance with the other version the wing outer surface has slots communicating, via appropriate ducts, with the air intake slows. The methods of flight control, taking off, flying and landing comprise using the system of control of aerostatic lift. The aircraft control system comprises a subsystem designed to control aerodynamic lift and that to control aerostatic lift. Thrust reverse incorporates the system controlling flaps and grids intended for separation the jet thrust into parts. The thrust reverse operating technique features using the aforesaid system of controlling flaps and grids. Three-leg landing gear comprises low-pressure tires. Gas separation and distribution system comprises pipelines communicating with the air intake receiver. ^ EFFECT: reduced dependence of flight upon weather conditions. ^ 43 cl, 27 dwg