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An aircraft, land, sea and air technology, applied in aircraft, convertible aircraft, wings and other directions, can solve the problems of low efficiency of horizontal flight and low efficiency of hovering in the air, and achieve the effect of increasing sailing speed and reducing air resistance
Inactive Publication Date: 2009-08-26
王万琼
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Problems solved by technology
It mainly solves the low efficiency of horizontal flight of existing helicopters and the low efficiency of VTOL vertical climbing and hovering in the air in the prior art
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[0020] figure 1 image 3 show (see figure 2 Figure 4 Figure 5 Figure 6 ), the present invention comprises drive system assembly, aircraft body is made up of two parts of machine head 2 fuselages, and machine head shape is quadrangular pyramid shape, fuselage front part 3 is quadrangular pyramid shape, and fuselage rear part 4 is quadrangular pyramid shape ; The nose is provided with an elevator: the air inlet 2a at the bottom of the nose is provided with an intake valve that controls the amount of air intake and is composed of two valve plates 2e, 2f hinged on the shaft 2d (see Figure 8 ), there are air outlets 2b, 2c on the left and right sides of the nose; a triangular vertical wing 5 is arranged on the top plate at the rear of the fuselage; the rear of the fuselage is provided with a fixed horizontal wing 9 and a telescopic movable horizontal wing 10; The whole aircraft body is arranged on a base plate 12, and the base plate is made up of two plates of an isoscele...
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Abstract
An aeroamphibious aircraft comprises a drive system assembly. A machine body of the aircraft is composed of two parts of a machine head and a fuselage, and a lifting rudder is arranged on the machine head; an air inlet valve which is used for controlling air inflow and composed of two valve leaves hinged on a shaft is arranged on an airflow inlet at the bottom part of the machine head, and airflow outlets are formed on the left and the right side surfaces of the machine head; a triangular vertical wing is arranged on a top plate at the back part of the fuselage; a fixed horizontal wing and a telescopic movable horizontal wing are arranged at the tail part of the fuselage; left and right wings are hinged on two waists of an isosceles trapezoid at a bottom plate, and two flaps are hinged on two waists of an isosceles triangle at the bottom plate; and four wheels are arranged on the bottom plate. The aeroamphibious aircraft solves the lift control during the flight from a plurality of aspects and solves the problem of reverse buoyancy during the land driving and the surface navigation by the unique design. The aeroamphibious aircraft can be applicable to the production of practical transportation tools or the production of toys.
Description
technical field [0001] The invention relates to a vehicle powered by an engine and capable of traveling on the ground, on the water or in the air, especially an amphibious aircraft for land, sea and air. Background technique [0002] Cars are divided into cars, buses, trucks, tractors, off-road vehicles, special vehicles (such as refrigerated trucks, passenger tank trucks, fire trucks, ambulances, etc.), and working condition dump trucks. Its basic structure is based on the engine (gasoline engine or diesel engine) as the power system, supplemented by transmission system, driving system, steering system, braking system and so on. Cars can only drive on land. Likewise, ships can only sail on water, and airplanes can only fly in the air. Existing automobiles, ships, and aircraft all have their exclusive uses, but do not have the multi-purpose or general-purpose functions of water, land and air. [0003] Chinese patent literature discloses a sea, land and air vehicle (CN1532...
Claims
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Application Information
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