Composite wing manned aircraft having double-propeller composite auxiliary wings with solar additional wings
A dual-propeller, manned aircraft technology, 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 convenience. The effect of group flight
Inactive Publication Date: 2018-08-28
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 to Figure 5 Shown, the compound wing manned aircraft of the twin-screw compound aileron with solar energy additional wing, by non-rear-thrust type compound wing aircraft, the propeller thrust self-powered compound auxiliary wing that is assembled on its wing both sides, additional wing 114 and carrying The human cabin 112 is composed of; wherein, the non-rear-thrust 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 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; A self-enclosed ducted fan 104 is provided inside the propeller thrust self-powered composite aileron, and one or both sides of the propeller thrust self-powered composite...
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The invention relates to a composite wing manned aircraft having double-propeller composite auxiliary wings with solar additional wings. The pushback-free composite wing aircraft comprises an aircraftbody, composite lift force wings fixedly mounted on two sides of the aircraft body, and additional wings, wherein the aircraft body adopts a deck platform; self-closing ducted fans are arranged in the composite lift force wings; wing hinges are designed on the outer sides of the composite lift force wings; batteries / fuels are arranged in the additional wings; solar battery panels are arranged onthe surfaces of the additional wings; a manned bin is mounted below the aircraft body. The composite wing manned aircraft disclosed by the invention has the characteristics of short take-off and landdistances, high flying speed, high wing structure intensity, capability of enabling the wings to store energy, low flying energy consumption, long hang time, high safety and the like; the auxiliary wings adopt composite lift force, so as to guarantee the application range of power.
Description
technical field [0001] The invention relates to an aircraft, in particular to a compound-wing manned aircraft with double-propeller compound auxiliary wings and a solar-attached 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 disadvanta...
Claims
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Login to View More IPC IPC(8): B64C27/28B64C3/00
CPCB64C27/28B64C3/00
Inventor任曲波
OwnerJIANGSU CHANGTAN ROBOT CO LTD