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Vertical take-off and landing tailstock type supersonic unmanned aerial vehicle

An unmanned aerial vehicle, vertical take-off and landing technology, applied in vertical take-off and landing aircraft, supersonic aircraft, aircraft and other directions, can solve the problems of difficult take-off and landing, high man-machine cost, and achieve the effect of high safety and reliability

Pending Publication Date: 2020-01-14
XIAN FLIGHT SELF CONTROL INST OF AVIC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, the carrier-based fighters equipped on the naval aircraft carrier platform are currently facing the following two important problems: 1. The cost of manned aircraft is high, and casualties should be avoided as much as possible during the confrontation
2 For carrier-based aircraft that roll and take off and land, it is also quite difficult to take off and land on an aircraft carrier

Method used

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  • Vertical take-off and landing tailstock type supersonic unmanned aerial vehicle
  • Vertical take-off and landing tailstock type supersonic unmanned aerial vehicle
  • Vertical take-off and landing tailstock type supersonic unmanned aerial vehicle

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Embodiment Construction

[0019] see figure 1 , the vertical take-off and landing tail seat type unmanned aerial vehicle of the present invention comprises fuselage 1, wing, engine 3 and vertical tail 4 four parts, and wing comprises inner wing 2 and outer wing 5.

[0020] The unmanned aerial vehicle adopts the aerodynamic layout of the double-swept single-wing, and the power adopts the engine 3 with thrust vectoring. All rooms are fusion designed.

[0021] The fuselage 1 has a slenderness ratio of 13; the design of the head side strip 0.3d or a shark head improves the asymmetrical nose vortex at a high angle of attack and suppresses the occurrence of side forces; the front fuselage: slenderness ratio: ln / d: 3, parabolic shape, shape curve: r / R=(x / ln)0.75, R is the radius of the bottom of the machine head 220mm, ln the length of the machine head is 0.8m; rear fuselage; tapered contraction; the middle part is used to place the fuel tank , flight control system, power supply and electrical system, etc...

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Abstract

The invention belongs to the aerial vehicle design technology, and particularly relates to a vertical take-off and landing tailstock type supersonic unmanned aerial vehicle. The vertical take-off andlanding tailstock type supersonic unmanned aerial vehicle comprises a fuselage, airfoils, engines and vertical fins. Each airfoil comprises an inner wing and an outer wing. The engines are installed between the inner wings and the outer wings. The front edge of each inner wing is provided with a vortex flap, and the rear edge of each inner wing is provided with a flap. The front edge of each outerwing is provided with a front edge slat, and the rear edge of each outer wing is provided with an aileron. Each vertical fin is provided with a rudder. Thrust vector engines are adopted as the engines, and the lower end of the belly part of each engine is provided with a folding supporting rod with a vertical take-off and landing assisting function. At different flight stages, through the cooperation of the thrust provided by the engines, the angle adjustment of all control surfaces and thrust vectoring nozzles, the attitude of the aerial vehicle is controlled. The vertical take-off and landing unmanned aerial vehicle with relative tilting power is simpler and higher in safety and reliability, and meanwhile the heavy-load transportation task requirement of the aerial vehicle can be met.

Description

technical field [0001] The invention belongs to aircraft design technology, in particular to a tail seat type supersonic unmanned aircraft capable of vertical take-off and landing. Background technique [0002] At present, for non-aircraft carrier platforms, the aircraft equipped by the Navy includes manned / unmanned helicopters and small reconnaissance drones. The purpose is to help non-aircraft carrier platforms obtain sea surface information and gain sea control. With the development of science and technology, the prerequisite for non-aircraft carrier platforms to obtain sea domination is to obtain air dominance. Relying on existing equipment strength is obviously not enough to seize air dominance in a strong confrontation environment. Of course, in the future joint combat mode under the multi-dimensional and complex environment of "land, sea, air, space, electricity, magnetism, and light", the aircraft carrier will still be the main platform for carrying and projecting ma...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C3/00B64C3/10B64C3/28B64D27/02B64C29/00B64C30/00
CPCB64C3/00B64C3/10B64C3/28B64D27/02B64C29/00B64C30/00
Inventor 赵超杨兆
Owner XIAN FLIGHT SELF CONTROL INST OF AVIC
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