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A vertical take-off and landing fixed-wing unmanned aerial vehicle with variable torque propeller

A technology for vertical take-off and landing and unmanned aerial vehicles, which is applied in vertical take-off and landing aircraft, unmanned aerial vehicles, landing gear, etc., can solve the problems of poor maneuverability, low flight speed, and can not meet the fast flight of unmanned aerial vehicles, etc. To achieve good stability and reduce the dependence of the venue runway

Inactive Publication Date: 2020-01-07
SHENYANG AEROSPACE UNIVERSITY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Most of the existing UAVs have the following problems: 1. Most of the fixed-wing UAVs need to use the runway to take off and land. Therefore, the fixed-wing UAVs have relatively high requirements for the venue; Perform vertical take-off and landing, but the flight speed is low, which cannot meet the conditions for the rapid flight of drones and has poor maneuverability

Method used

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  • A vertical take-off and landing fixed-wing unmanned aerial vehicle with variable torque propeller
  • A vertical take-off and landing fixed-wing unmanned aerial vehicle with variable torque propeller
  • A vertical take-off and landing fixed-wing unmanned aerial vehicle with variable torque propeller

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Embodiment Construction

[0021] The present invention will be described in further detail below in conjunction with embodiment.

[0022] according to figure 1 , figure 2 and Figure 4 As shown, a vertical take-off and landing fixed-wing unmanned aerial vehicle with a variable torque propeller comprises a fuselage 1, and the middle and tail of the fuselage 1 are respectively equipped with a wing 2 and an empennage 3, and the empennage 3 has at least three The angle between two adjacent empennages 3 is less than 180 degrees, and the empennages 3 distributed on both sides of the fuselage are symmetrically arranged, and an aileron 7 is hinged at the rear edge of the wing 2, and the empennage 3 There is a tail rudder 8 hinged on it. During the flight, the roll of the UAV is controlled by adjusting the aileron 7, and the pitch and yaw of the UAV are controlled by the tail rudder 8. The engine 5 is installed at the top, and two sets of variable torque propellers 6 are installed on the output shaft of the...

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Abstract

The present invention is a vertical take-off and landing fixed-wing unmanned aerial vehicle with a variable torque propeller, comprising a fuselage, the middle and tail of the fuselage are respectively equipped with wings and empennage, the fuselage head is equipped with an engine, and the output shaft of the engine Two sets of variable torque propellers are installed on the drone. When the UAV is running, the two sets of variable torque propellers rotate in opposite directions. A buffer landing mechanism is provided on the tail. The buffer landing mechanism includes: a connecting rod, a buffer device and a roller, and one end of the connecting rod It is hinged to the empennage, the other end of which is hinged to the roller, and the middle part of the connecting rod is hinged to the buffer device fixed in the empennage. The vertical take-off and landing and parking are carried out through the buffer take-off and landing mechanism. On the one hand, it has the flying speed of a fixed-wing UAV. Due to the dependence of the drone on the runway, the tail fins of the drone are equipped with rollers. During the flight, the rollers are driven by the airflow to rotate at a high speed, so that the attitude of the drone during the flight has better stability.

Description

Technical field: [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a vertical take-off and landing fixed-wing unmanned aerial vehicle with variable torque propellers. Background technique: [0002] With the changes of the times, although the popularity of manned aircraft has not decreased, it has gradually exposed many disadvantages. For example, the cost of the aircraft is too high, and the crash of the aircraft threatens the life of the pilot, which makes the safety and technical requirements of manned aircraft continue to increase. Thereby, the cost of the aircraft is also continuously increased. In order to reduce the cost of manned aircraft and adapt to the development needs of modern warfare and society, countries have successively developed an unmanned aircraft, referred to as UAV. In recent years, in global local wars, the military has used drones to attack terrorists, conduct reconnaissance and surveys on battlefields...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C29/00B64C25/34B64C25/62B64C17/00
CPCB64C17/00B64C25/34B64C25/62B64C29/0025B64U10/25B64U70/80B64U30/20
Inventor 徐光延孟亭磊陈侠
Owner SHENYANG AEROSPACE UNIVERSITY
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