Non-rear-thrust type composite wing aircraft with ducted fan composite auxiliary wing and additional wing
A ducted fan and composite wing technology, used in aircraft, rotorcraft, current collectors, etc., can solve the problems of low wing structure, slow horizontal flight speed, and unsatisfactory controllability, etc., to expand the wing. The effect of area, fast flight speed and convenient cluster flight
Inactive Publication Date: 2018-11-20
JIANGSU CHANGTAN ROBOT CO LTD
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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.
Method used
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[0031] The present invention will be further described below in conjunction with the accompanying drawings.
[0032] Such as figure 1 As shown, the non-rear-thrust type compound-wing aircraft with ducted fan compound auxiliary wing and additional wing is characterized in that the thrust self-powered by the non-rear-thrust type compound-wing aircraft and the ducted fan thrust assembled on both sides of its wing Composite ailerons and additional wings 114; wherein, the non-rear thrust compound wing aircraft includes a body 101, fixedly installed on both sides of the body 101 composite lift wings 102; wherein, wherein, the body 101 is set as a deck platform; the self-enclosed ducted fan 104 is built in the composite lift wing 102, and a wing hinge 1028 is designed on the outside of the composite lift wing 102; 1063, a self-enclosed ducted fan 104 is provided inside the ducted fan thrust self-powered composite aileron, and an electro-hydraulic interface 1036 and a wing hinge 1028...
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The invention relates to a non-rear-thrust type composite wing aircraft with a ducted fan composite auxiliary wing and an additional wing. A self-sealing ducted fan is arranged in a ducted fan thrustself-energized composite wing; an electrohydraulic gas interface and a wing hinge are arranged on one side or two sides of the ducted fan thrust self-energized composite wing; the ducted fan thrust self-energized composite wing is movably connected with a composite lift force wing through the wing hinge; the wing hinge is arranged on one side, facing towards a machine body, of the additional wing;the additional wing is foldably arranged on the outer side of the composite lift force wing through the wing hinge; a battery / fuel is arranged in the additional wing; and a solar battery panel is arranged on the surface of the additional wing. The non-rear-thrust type composite wing aircraft has the characteristics of short take-off and landing distance, low flight energy consumption, long hang time, high safety and the like; and the auxiliary wing adopts a composite lift force, so that the power application range is guaranteed.
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...
Claims
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Login to View More IPC IPC(8): B64C27/22B64C27/26H02J7/35
CPCB64C27/22B64C27/26H02J7/35
Inventor任曲波
OwnerJIANGSU CHANGTAN ROBOT CO LTD