A propeller-drive composite-wing manned aircraft provided with two-propeller auxiliary wings and ailerons
A twin-propeller, manned aircraft technology, applied in the field of aircraft, can solve the problems of low structural strength of the wing, slow horizontal flight speed, and unsatisfactory controllability, etc., to achieve expanded wing area, fast flight speed, and improved lift effect
Inactive Publication Date: 2018-12-04
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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[0034] The present invention will be further described below in conjunction with the accompanying drawings.
[0035] Such as Figure 1 to Figure 5 Shown, a kind of propulsion composite wing manned aircraft with double propeller auxiliary wing and attached wing, comprises rear single propeller compound wing aircraft, propeller thrust self-powered composite auxiliary wing assembled on both sides of its wing and additional wing 114 ; Wherein, the rear single propeller compound wing aircraft comprises a body 101, fixedly installed on the body 101 both sides compound lift wing 102, propeller 106; wherein, the body 101 is set to a deck platform; The lift wing 102 has a built-in self-enclosed ducted fan 104, and a wing hinge 1028 is designed on the outside of the composite lift wing 102; A self-enclosed ducted fan 104 is arranged inside the propeller thrust self-powered composite aileron, and an electro-hydraulic interface 1036 and a wing hinge 1028 are arranged on both sides, and t...
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A propeller-drive composite-wing manned aircraft provided with two-propeller auxiliary wings and ailerons is provided. A composite-wing aircraft with one rear propeller includes a fuselage, compositelifting wings fixedly mounted at two sides of the fuselage, and a propeller, wherein self-sealing ducted fans are disposed in the composite lifting wings; wing hinges are designed at outsides of the composite lifting wings; the propeller is disposed at the front end of a propeller thrust self-powered composite auxiliary wing; self-sealing ducted fans are disposed in the propeller thrust self-powered composite auxiliary wing; two sides of the propeller thrust self-powered composite auxiliary wing are provided with electro-hydraulic gas connectors and wing hinges and are movably connected to thecomposite lifting wings through the wing hinges; and one side of each aileron, facing the fuselage, is provided with a wing hinge and an electro-hydraulic gas connector, and is mounted, in a foldablemanner, to the outside of the propeller thrust self-powered composite auxiliary wing through the wing hinge. Composite lifting force is adopted by the auxiliary wings to ensure the suitable application range of power.
Description
technical field [0001] The invention relates to an aircraft, in particular to a screw thruster compound wing manned aircraft with double propeller auxiliary wings and attached wings, 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): B64C27/26B64C27/20
CPCB64C27/26B64C27/20
Inventor任曲波
OwnerJIANGSU CHANGTAN ROBOT CO LTD