Rear single propeller type composite wing aircraft with propeller thrust composite ailerons
A propeller and compound wing 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 group flight Effect
Inactive Publication Date: 2018-09-07
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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[0035] The present invention will be further described below in conjunction with the accompanying drawings.
[0036] like Figure 1 to Figure 5 Shown, a kind of rear single propeller compound wing aircraft with propeller thrust compound aileron is made up of rear single propeller type compound wing aircraft and the propeller thrust self-powered composite aileron assembled on its wing both sides;
[0037] Wherein, the rear single propeller compound 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 set as a deck platform; the The compound lift wing 102 has a built-in self-enclosed ducted fan 104, and the outer side of the compound lift wing 102 is designed with a wing hinge 1028;
[0038] The front end of the propeller thrust self-powered composite aileron is provided with a propeller propeller 1062, the inside of the propeller thrust self-powered composite aileron is provid...
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The invention provides a rear single propeller type composite wing aircraft with propeller thrust composite ailerons. The rear single propeller type composite wing aircraft with the propeller thrust composite ailerons comprises a rear single propeller type composite wing aircraft and propeller thrust self-energized composite ailerons which are assembled on a wing, wherein the rear single propellertype composite wing aircraft comprises an aircraft body, composite lift wings and a thruster, wherein the composite lift wings are fixedly mounted on the two sides of aircraft body; the aircraft bodyis arranged as a deck platform; self-sealed ducted fans are embedded in the composite lift wings; wing hinges are designed on the external sides of the composite lift wings; and the thruster is a propeller type thruster. The rear single propeller type composite wing aircraft with the propeller thrust composite ailerons has the advantages that the take-off and landing distance is short, the flyingspeed is high, the wing structural strength is high, the wing can store energy, the flying energy consumption is low, the aircraft can stay in the air for long time, the safety is high and so on; andthe ailerons adopt composite lift forces so that the application range of the power is guaranteed.
Description
technical field [0001] The invention relates to an aircraft, in particular to a rear single propeller 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 of hig...
Claims
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Login to View More IPC IPC(8): B64C27/22B64C27/20B64C3/00B64C9/00B64C1/00
Inventor任曲波
OwnerJIANGSU CHANGTAN ROBOT CO LTD