发明名称 Method of creation of airplane type aircraft forces system and aircraft - ground-air amphibian for its implementation
摘要 The invention relates to vehicles of airplane's type designated for short-haul and mean-haul operation routes for passenger and freight traffic transportation. More precisely, it relates to methods of enhancing of the aerodynamic and transport characteristics of aircrafts of airplane's type, which are obtained by the use of new constructional elements. The invention's essence is that lift, thrust and control forces of aeroplane type aircraft are created in order to provide it with take-off, landing, motion and maneuvring. Gas dynamic power transfer is performed from gas generators to lift propulsors-fans, cruise propulsor (3) and to a device designed to create a gas jet curtain. Additional freight and passenger modules (5) are disposed on the wing (4) tips. These modules and fuselage are made in the form of aerodynamic airfoils. A static air cushion is created under the bottom carrying surface of the vehicle. The lift propulsors-fans are disposed near the bottom of the vehicle. A jet is created and directed to a supporting surface and intensive suction of boundary layer from the upper airfoil section is also performed. An action of created system of forces is rationally distributed in the vehicle construction and strains structure variation is realized in the construction members. The aircraft of aeroplane type is made as the ground-air amphibian type. The aircraft comprises the fuselage with passenger cabin and/or additional compartments, the lift wing with end plates (6) mounted on its tips and powerplant with gas generators providing with the cruise propulsor and lift propulsors-fans, which form start and landing multi-chamber air cushion that is retained by means of gas jet curtains. The gas generators are connected to actuators by means of gas conduits, and the fans are made carrying and disposed at the fuselage and wing junction. Movable suspended passenger and freight modular sections (5) are secured to the end plates of the wing.
申请公布号 AU3542799(A) 申请公布日期 1999.11.08
申请号 AU19990035427 申请日期 1999.04.12
申请人 VALENTIN VASILIEVICH NAZAROV 发明人 VALENTIN VASILIEVICH NAZAROV
分类号 B60V1/08;B60F5/02;B60V3/08 主分类号 B60V1/08
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