Rear single-propeller type composite wing manned aircraft with propeller thrust composite auxiliary wings
A propeller and composite wing technology, applied in the field of aircraft, can solve the problems of low wing structure strength, slow horizontal flight speed, unsatisfactory controllability, etc. Effect
Inactive Publication Date: 2018-11-16
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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[0033] The present invention will be further described below in conjunction with the drawings.
[0034] Such as Figure 1 to Figure 5 As shown, the rear single propeller composite wing manned aircraft with propeller thrust composite ailerons consists of a rear single propeller composite wing aircraft and the propeller thrust self-powered composite ailerons assembled on both sides of its wing;
[0035] Wherein, the rear single-propeller composite wing aircraft includes a body 101, a composite lift wing 102 and a propeller 106 fixedly installed on both sides of the body 101; wherein, the body 101 is configured as a deck platform; The composite lift wing 102 has a built-in self-enclosed ducted fan 104, and the outside of the composite lift wing 102 is designed with a wing hinge 1028;
[0036] The front end of the propeller thrust self-powered composite wing is provided with a propeller thruster 1062, the propeller thrust self-powered composite wing is provided with a self-enclosed duct...
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The invention relates to a rear single-propeller type composite wing manned aircraft with propeller thrust composite auxiliary wings. The rear single-propeller type composite wing manned aircraft is composed of a rear single-propeller type composite wing aircraft body and the propeller thrust self-energy-supply composite auxiliary wings assembled on the two sides of wings of the rear single-propeller type composite wing aircraft body. The rear single-propeller type composite wing aircraft body comprises a fuselage, the composite lift wings fixedly mounted on the two sides of the fuselage, anda thruster. The fuselage is arranged as a deck platform. Self-closed culvert fans are arranged in the composite lift wings, and wing hinges are designed on the outer sides of the composite lift wings.The thruster is a propeller thruster. The rear single-propeller type composite wing manned aircraft has the characteristics that the takeoff and landing distance is short, the flight speed is high, the structure strength of the wings is high, the wings can store energy, flight energy consumption is low, and the hang time is long; and the auxiliary wings adopt composite lift to ensure the adaptionrange of power, and meanwhile, the composite lift wings with the large area can achieve the action of a glider under the emergency situations, so that the safety of the aircraft is greatly improved,and the safety of personnel and materials is guaranteed.
Description
Technical field [0001] The invention relates to an aircraft, in particular to a rear single-propeller type composite wing manned aircraft with a propeller thrust composite aileron, which 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 the main wing and the horizontal tail are not connected before and after, the wing structure is not strong, easy to damage, high take-off and landing requirements, and long take-off and landing distances; the traditional vertical Take-off and landing aircraft have the advantages of convenient take-off and landing, but they have disadvantages such as high energy consumption, low safety fac...
Claims
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IPC IPC(8): B64C27/20B64C27/26B64C37/02
Inventor任曲波
OwnerJIANGSU CHANGTAN ROBOT CO LTD