Rear single-propeller compound-wing plane with twin-duct compound ailerons and additional wings
A compound wing and auxiliary wing technology, which is applied in the field of aircraft, can solve the problems of low structural strength of the wing, unsatisfactory controllability, and slow horizontal flight speed, so as to expand the area of the wing, increase the lift force, and speed up the flight Effect
Inactive Publication Date: 2018-11-02
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.
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[0035] The present invention will be further described below in conjunction with the accompanying drawings.
[0036] Such as Figure 1 to Figure 5 As shown, a rear single-screw compound wing aircraft with double-duct compound ailerons and additional wings includes a rear single-screw compound wing aircraft, propeller thrust self-powered compound ailerons assembled on both sides of its wing and additional Wing 114; Wherein, described rear single propeller compound wing aircraft comprises body 101, is fixedly installed in body 101 both sides compound lift wing 102, propeller 106; Wherein, described body 101 is set to deck platform; The composite 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 provided inside the composite aileron, and an electro-hydraulic interface 1036 and a wing hinge 1028 are provided on both sides of the propeller thrust self-powered...
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The invention relates to a rear single-propeller compound-wing plane with twin-duct compound ailerons and additional wings. A rear single-propeller compound-wing aircraft comprises a plane, compound lift wings fixedly installed on the two sides of the plane and ducted-fan propellers; self-sealing ducted-fans are arranged in the compound lift wings, and wing hinges are designed on the outer sides of the compound lift wings; the ducted-fan propellers are arranged at the front ends of the propeller thrust self-energized compound ailerons, self-sealing ducted fans are arranged in the propeller thrust self-energized compound ailerons, power fluid and gas connectors and the wing hinges are arranged on the two sides of the propeller thrust self-energized compound ailerons, and the airscrew thrustself-energized compound ailerons are movably connected with the compound lift wings through the wing hinges on one sides; a manned cabin is installed on the bottom of the plane. The rear single-propeller compound-wing plane with the twin-duct compound ailerons and the additional wings not only has the advantages of being short in take-off and landing distance, high in flying speed, high in wing structure strength, capable of energy storage by means of the wings, low in flying energy consumption, long in hang time, high in safety and the like, but also compound lift is adopted by the ailerons,so that the power adaptive range is ensured.
Description
technical field [0001] The invention relates to an aircraft, in particular to a rear single-blade compound-wing aircraft with a double-duct compound auxiliary wing and an additional wing, and 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 disa...
Claims
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Login to View More IPC IPC(8): B64C27/20B64C27/26B64C37/02
CPCB64C27/20B64C27/26B64C37/02
Inventor任曲波
OwnerJIANGSU CHANGTAN ROBOT CO LTD