Back single ducted fan type compound wing manned craft with propeller thrust compound auxiliary wing
A ducted fan and propeller technology, which is applied in the field of aircraft, can solve the problems of low wing structure strength, slow horizontal flight speed, and unsatisfactory controllability, and achieves expansion of wing area, fast flight speed, and convenient clustering. effect of flight
Pending Publication Date: 2019-06-11
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 type composite wing manned aircraft with propeller thrust compound auxiliary wing is characterized in that the propeller thrust self-supplied by the rear single duct fan type composite wing aircraft and the propellers assembled on both sides of its wing Composite auxiliaries and a manned cabin 112; wherein, the rear single-duct fan compound wing aircraft includes a body 101, a composite lift wing 102 fixedly installed on both sides of the body 101, and a propeller 106; wherein, The body 101 is set as a 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 front end of the propeller thrust self-powered composite aileron is provided with a propeller pro...
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The invention relates to a back single ducted fan type compound wing manned craft with a propeller thrust compound auxiliary wing. The back single ducted fan type compound wing manned craft comprisesa body, compound lift force wings and a manned cabin fixedly mounted on two sides of the body, wherein the body is arranged as a deck platform; a self-closed ducted fan is arranged in the compound lift force wing, and a wing hinge is designed on the outer side of the compound lift force wing; a propeller thruster is arranged at the front end of the propeller thrust self energy-supplying compound auxiliary wing, the self-closed ducted fan is arranged in the propeller thrust self energy-supplying compound auxiliary wing, an electro-hydraulic-gas interface and the wing hinge are arranged on one side or two sides of the propeller thrust self energy-supplying compound auxiliary wing and are movably connected to the compound lift force wing through the wing hinge, and the manned cabin is mountedbelow the body. The back single ducted fan type compound wing manned craft not only has the characteristics of being short in landing and take-off distance, high in flying speed, high in strength ofwing structure, capable of storing energy by the wing, low in flying energy consumption, long in hang time, high in safety and the like. The auxiliary wing employs a compound lift force, so that the application range of power is ensured.
Description
technical field [0001] The invention relates to an aircraft, in particular to a rear single-duct fan compound wing manned 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 disadvantage...
Claims
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Login to View More IPC IPC(8): B64C27/20B64C27/26B64C37/02
Inventor任曲波
OwnerJIANGSU CHANGTAN ROBOT CO LTD