Rear single-ducted fan type composite wing aircraft with propeller thrust composite auxiliary wings
A ducted fan and propeller 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 convenient clustering The effect of flying
Inactive Publication Date: 2018-11-13
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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[0031] The present invention will be further described below in conjunction with the accompanying drawings.
[0032] Such as figure 1 As shown, a rear single-duct fan compound wing aircraft with propeller thrust compound auxiliary wing is characterized in that the rear single duct fan compound wing aircraft and the propeller thrust self-powered compound mounted on both sides of its wing Auxiliary wing is formed; Wherein, described rear single duct fan type composite wing aircraft comprises body 101, is fixedly installed in body 101 both sides composite lift wing 102, propeller 106; Wherein, 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; the propeller 106 is a ducted fan propeller; the propeller thrust self-powered composite auxiliary The front end of the wing is provided with a propeller propeller 1062, and the inside ...
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The invention discloses a rear single-ducted fan type composite wing aircraft with propeller thrust composite auxiliary wings. A rear single-ducted fan type composite wing aircraft body comprises a fuselage, composite lift wings fixedly mounted on the two sides of the fuselage, and a ducted fan thruster. The fuselage body is arranged as a deck platform; the composite lift wings are internally provided with self-closed ducted fans, and wing hinges are designed on the outer sides of the composite lift wings; and propeller thrusters are arranged at the front ends of the propeller thrust self-energy-supply composite auxiliary wings, self-closed ducted fans are arranged inside the propeller thrust self-energy-supply composite auxiliary wings, and one sides or the two sides of the propeller thrust self-energy-supply composite auxiliary wings are provided with electro-hydraulic gas connectors and wing hinges, and movably connected with the composite lift wings through the wing hinges. The rear single-ducted fan type composite wing aircraft has the characteristics that the takeoff and landing distance is short, the flight speed is high, the wings are high in structural strength and can store energy, flight energy consumption is low, the hang time is long, and safety is high; and the auxiliary wings adopt composite lift, and the applicable range of power is guaranteed.
Description
technical field [0001] The invention relates to an aircraft, in particular to a rear single duct fan type compound wing aircraft with a propeller thrust compound auxiliary 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 disadvantages ...
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