No-back-thrust-type complex-wing manned aircraft with turbofan complex ailerons and additional wings
A compound wing and aircraft 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: 2018-11-09
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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[0029] The present invention will be further described below in conjunction with the accompanying drawings.
[0030] Such as Figure 1 to Figure 5 As shown, the non-rear-thrust type compound wing manned aircraft with a turbofan compound auxiliary wing and additional wings is characterized in that the thrust self-powered by the non-rear-thrust type compound wing aircraft and the turbofan thrust assembled on both sides of its wing Composite aileron, additional wing 114 and manned cabin 112; Wherein, described non-rear-thrust type composite wing aircraft comprises body 101, is fixedly installed in body 101 both sides composite lift wing 102; Wherein, wherein, described The body 101 is set as a deck platform, and the self-enclosed ducted fan 104 is built in the composite lift wing 102, and a wing hinge (1028) is designed on the outside of the composite lift wing 102; A turbofan propeller 1064 is provided, and a self-enclosed ducted fan 104 is provided inside the turbofan thrust s...
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The invention relates to a no-back-thrust-type complex-wing manned aircraft with turbofan complex ailerons and additional wings. A deck platform serves as a fuselage; self-sealing ducted fans are built in complex lifting wings, and wing hinges are designed at outer sides of the complex lifting wings; turbofan propellers are arranged below turbofan thrust self-energizing complex ailerons, self-sealing ducted fans are arranged inside the turbofan thrust self-energizing complex ailerons, electrohydraulic gas interfaces and wing hinges are arranged at one side or two sides of each turbofan thrustself-energizing complex aileron and are movably connected with the complex lifting wings through the wing hinges, the wing hinges are arranged at one side, facing to the fuselage, of each additional wing, and the additional wings are mounted at outer sides of the complex lifting wings in a foldable manner through the wing hinges; a manned cabin is mounted below the fuselage. The no-back-thrust-type complex-wing manned aircraft has the characteristics that the taking off and landing distance is short, the flight speed is high, the wings are high in structural strength and can store energy, theenergy consumption of flight is low, the hang time is long, the safety is high, and the like; the ailerons adopt a complex lifting force, so that the adaptation range of power is ensured.
Description
technical field [0001] The invention relates to an aircraft, in particular to a thrustless composite wing manned aircraft with a turbofan compound auxiliary wing and an additional 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 disadvan...
Claims
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Patent Timeline
Login to View More IPC IPC(8): B64C27/20B64C27/26B64C37/02
CPCB64C27/20B64C27/26B64C37/02B64U50/12B64U50/19
Inventor任曲波
OwnerJIANGSU CHANGTAN ROBOT CO LTD