Back-thrust-force-free type composite wing manned craft with turbofan thrust composite auxiliary wings

Abstract

The invention provides a back-thrust-force-free type composite wing manned craft with turbofan thrust composite auxiliary wings. The back-thrust-force-free type composite wing manned craft comprises acraft body and composite elevating force wings fixedly mounted on the two sides of the craft body. The craft body is arranged to be a deck platform. The composite elevating force wings are internallyprovided with self-sealing ducted fans, and wing hinges are designed on the outer sides of the composite elevating force wings. Turbofan thrusters are arranged at the front ends of turbofan thrust self-powered composite auxiliary wings, electricity, liquid and gas interfaces and the wing hinges are arranged on one sides or two sides of the turbofan thrust self-powered composite auxiliary wings, and the turbofan thrust self-powered composite auxiliary wings are connected with the composite elevating force wings through the wing hinges. The back-thrust-force-free type composite wing manned craft has the characteristics of being short in take-off and landing distance, high in flight speed, high in wing structure strength, capable of achieving energy storage through the wings, low in flight energy consumption, long in hovering time, high in safety and the like, the auxiliary wings adopt composite elevating force, and the adaptability of power is guaranteed.

Description

technical field [0001] The invention relates to an aircraft, in particular to a non-rear thrust compound wing manned aircraft with a turbofan thrust compound 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 disadvantages of...

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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