Vertical take-off and landing unmanned conveyor and control method thereof

A technology for vertical take-off and landing and transport aircraft, applied in the field of aviation, can solve the problems of difficult control of unmanned aerial vehicles, increase the cargo space of the aircraft, and small carrying capacity, so as to eliminate the dihedral reflection effect, reduce the area of ​​the flight site, and reduce the carrying capacity. big effect

Pending Publication Date: 2020-03-27
SHENYANG AEROSPACE UNIVERSITY
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to solve the above problems, the present invention provides a vertical take-off and landing unmanned transport aircraft and its control method, using a lift fan to provide lift and assist balance during vertical take-off and landing, and at the same time reduce the control of the aircraft by designing the aircraft structure and aerodynamic layout. Difficulty, increase the cargo space of the aircraft, effectively solve the problems of control difficulties and small load capacity of the existing vertical take-off and landing unmanned aerial vehicles, in order to achieve vertical and short-distance take-off and landing, with flexible and stable flight, wide application range, and high load capacity Its specific technical solutions are as follows:

Method used

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  • Vertical take-off and landing unmanned conveyor and control method thereof
  • Vertical take-off and landing unmanned conveyor and control method thereof
  • Vertical take-off and landing unmanned conveyor and control method thereof

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Embodiment Construction

[0035] The present invention will be further described below in conjunction with specific examples of implementation, but the present invention is not limited to these examples.

[0036] A vertical take-off and landing unmanned transport aircraft, comprising a fuselage 1, a wing 2, an empennage 6, a landing gear 8, an engine compartment 10, and a cargo compartment 20, and is characterized in that, two sides of the fuselage 1 are provided with wings 2, and 1 and the wing 2 are a wing-body fusion body; three landing gears 8 are arranged under the fuselage 1 and the wing 2; an aileron 3 and two flaps 4 are arranged at the rear end of the wing 2; The tip of the wing 2 is provided with a winglet 5; the tail of the fuselage 1 is provided with an empennage 6, the empennage 6 is a single vertical tail, and the empennage 6 is provided with a rudder 7; the wing 2 is close to the inside of the fuselage 1 An engine compartment 10 is provided, the front end of the engine compartment 10 is ...

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Abstract

The invention discloses a vertical take-off and landing unmanned aerial vehicle and a control method thereof, and belongs to the field of aviation. According to the unmanned transport plane, the liftfan is used for providing lift and assisting balance during vertical take-off and landing; meanwhile, through the design of the aircraft structure and the aerodynamic layout, the control difficulty ofthe aircraft is reduced, the goods carrying space of the aircraft is increased, the problems that an existing vertical take-off and landing unmanned aerial vehicle is difficult to control and small in load capacity are effectively solved, vertical and short-distance take-off and landing are achieved, and the aircraft has the advantages of flexible and stable flight, wide application range, largeload capacity and the like.

Description

technical field [0001] The invention belongs to the field of aviation, and in particular relates to a vertical take-off and landing unmanned transport aircraft and a control method thereof. Background technique [0002] In recent years, UAV technology has developed rapidly. UAVs have great application value in aerial photography, transportation, inspection, plant protection and other fields. UAVs are now widely used in various military and civilian fields, among which vertical take-off and landing As a special type of UAV, UAV can take off and land at zero speed without opening up a special takeoff and landing runway. Compared with conventional UAVs, vertical take-off and landing UAVs have the advantages of flexible takeoff and landing methods, convenient launch and recovery, and good maneuverability, and also have the general functions of conventional UAVs. The development of new vertical take-off and landing UAVs has high practical value for winning the initiative in the ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C29/00B64C3/00B64C27/20B64D27/02B64C1/06B64C25/04
CPCB64C1/068B64C3/00B64C25/04B64C27/20B64C29/00B64D27/02
Inventor 杨靖宇张峻渤唐寅峰
Owner SHENYANG AEROSPACE UNIVERSITY
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