Rear single-propeller type composite wing manned aircraft with thrust-free composite ailerons

Abstract

The invention relates to a composite lift aircraft with an expanding platform. A rear single-propeller type composite wing aircraft comprises an aircraft body, composite lift ailerons which are fixedly arranged on two sides of the aircraft body and propeller thrusts, wherein the aircraft body is arranged as a deck platform; self-closed duct fans are arranged inside the composite lift ailerons; aileron hinges are arranged on the outer sides of the composite lift ailerons; self-closed duct fans are arranged inside thrust-free self-energy supplied composite ailerons; electro-hydraulic and pneumatic interfaces and aileron hinges are arranged on one side or two sides of the thrust-free self-energy supplied composite ailerons; the thrust-free self-energy supplied composite ailerons are movably connected with the corresponding composite lift ailerons by the corresponding aileron hinges; a manned capsule is arranged below the aircraft body. The composite lift aircraft disclosed by the invention has the characteristics of short take-off and landing distance, high flight speed, high structural strength of the ailerons, capability of storing energy by the ailerons, low flight energy consumption, long hang time and the like; the large-area composite lift ailerons can be used as a glider under the emergency condition, so that the safety of the aircraft is greatly improved and the safety ofmaterials is ensured.

Description

technical field [0001] The invention relates to an aircraft, in particular to a rear single propeller composite wing manned aircraft with a non-thrusting composite auxiliary wing, which belongs to the technical field of aircraft equipment. Background technique [0002] Existing aircraft are mainly divided into two categories: fixed-wing and vertical take-off and landing aircraft (such as helicopters and multi-rotors). Of course, there is also a vertical take-off and landing fixed-wing product. The traditional fixed wing has the advantages of fast flight speed, low energy consumption, etc., but it has the disadvantages that the main wing and the horizontal tail are not connected front and rear, the wing structure is not strong, easy to be damaged, the take-off and landing requirements are high, and the take-off and landing distance is long; the traditional vertical The take-off and landing aircraft has the advantages of convenient take-off and landing, but has the disadvanta...

AI Technical Summary

Problems solved by technology

The traditional fixed wing has the advantages of fast flight speed, low energy consumption, etc., but it has the disadvantages that the main wing and the horizontal tail are not connected front and rear, the wing structure is not strong, easy to be damaged, the take-off and landing requirements are high, and the take-off and landing distance is long; the traditional vertical The take-off and landing aircraft has the advantages of convenient take-off and landing, but has the disadvantages of high energy consumption, low safety factor, poor load capacity, slow horizontal flight speed, and easy crash; although the current vertical take-off and landing fixed wing has the characteristics of convenient take-off and landing , but the controllability is not ideal when flying horizontally, and there are disadvantages such as large flight resistance, high energy consumption, and low safety factor.

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