Combined wing aircraft with double-propeller-thrust combined auxiliary wings
A technology of double propellers and compound wings, which is applied in the field of aircraft, can solve the problems of low structural strength of the wings, unsatisfactory controllability, and slow horizontal flight speed, etc., so as to expand the wing area, facilitate cluster flight, and increase the flight speed. fast effect
Inactive Publication Date: 2018-11-06
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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[0030] The present invention will be further described below in conjunction with the accompanying drawings.
[0031] Such as Figure 1 to Figure 5 As shown, a compound wing aircraft with double propeller thrust compound ailerons is composed of a non-rear thrust type compound wing aircraft and self-powered composite ailerons assembled on both sides of its wing with propeller thrust; The compound-wing aircraft includes a body 101 and a compound lift wing 102 fixedly installed on both sides of the body 101; wherein, the body 101 is set as a deck platform; the compound lift wing 102 has a built-in self-enclosed ducted fan 104 The composite lift wing 102 is designed with a wing hinge (1028) on the outside; the front end of the propeller thrust self-powered composite aileron is provided with a propeller propeller 1062, and the inside of the propeller thrust self-powered composite aileron is provided with a self-enclosed ducted fan 104. One or both sides of the propeller thrust self...
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The invention relates to a combined wing aircraft with double-propeller-thrust combined auxiliary wings. The combined wing aircraft comprises a rear-thrust-free type combined wing aircraft and propeller-thrust self-power combined auxiliary wings which are arranged on the two sides of wings of the rear-thrust-free type combined wing aircraft, wherein the rear-thrust-free type combined wing aircraftcomprises a machine body and combined lift force wings fixedly arranged on the two sides of the machine body, the machine body is set as a deck platform, self-sealed ducted fans are arranged in the combined lift force wings, and wing hinges are designed on the outer sides of the combined lift force wings; propeller thrusters are arranged at the front ends of the propeller-thrust self-power combined auxiliary wings, spaces are reserved between lift force auxiliary wings and balance auxiliary tail wings, and horizontal elevating rudder wings are arranged in the spaces; one or more self-sealed ducted fan is arranged in each lift force auxiliary wings. The combined wing aircraft disclosed by the invention has the characteristics of short rising and landing distance, quick flying speed, high wing structure strength, low flying energy consumption, long hang time, high safety and the like; the wings can be used for storing energy; the auxiliary wings utilize combined lift force, so that a power adaption range is ensured.
Description
technical field [0001] The invention relates to an aircraft, in particular to a compound-wing aircraft with double-propeller thrust and compound auxiliary wings, 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 disadvantages of high energy c...
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