Non-rear-thrust type composite wing aircraft with ducted fan composite auxiliary wings and additional wings

Abstract

The invention relates to a non-rear-thrust type composite wing aircraft with ducted fan composite auxiliary wings and additional wings. The non-rear-thrust type composite wing aircraft comprises an aircraft body, composite lift wings fixedly mounted on both sides of the aircraft body and the additional wings. The aircraft body is arranged as a deck platform. The composite lift wings are internallyprovided with self-sealing ducted fans, and wing hinges are designed on the outer sides of the composite lift wings. Ducted fan thrusters are arranged at the front ends of the ducted fan thrust self-power composite auxiliary wings, and the ducted fan thrust self-power composite auxiliary wings are internally provided with self-sealing ducted fans. Electro-hydraulic gas interfaces and the wing hinges are arranged on one or both sides of the ducted fan thrust self-power composite auxiliary wings, and the ducted fan thrust self-power composite auxiliary wings are movably connected with the composite lift wings through the wing hinges. A manned bin is mounted at the bottom of the aircraft body. The non-rear-thrust type composite wing aircraft has the characteristics of short take-off and landing distance, high wing structure strength, energy storage of the wings, low flight energy consumption, long hang time, high safety and the like, and the auxiliary wings adopt composite lift force toensure the subject range of power.

Description

technical field [0001] The invention relates to an aircraft, in particular to a thrustless composite wing aircraft with a ducted fan compound auxiliary wing and an additional wing, belonging 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 disadvantag...

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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