阅读说明：本技术 一种可拆卸使用的垂直起降无人机 (Can dismantle VTOL unmanned aerial vehicle of use ) 是由 朱超 易佳宁 冯冠钦 谌海云 许瑾 赵书朵 岑汝平 沈炽炯 于 2019-09-23 设计创作，主要内容包括：本发明提供的一种可拆卸使用的垂直起降无人机,包括机身、旋翼、机翼、尾翼和水平动力电机；旋翼采用十字结构固定在机身上；机翼通过插接的方式与机身相连接；尾翼在机身尾部通过卡接的方式进行拼接；水平动力电机放置在机身前端。包括四个旋翼。本发明提供的一种可拆卸使用的垂直起降无人机,大大的节省了携带运输所需的空间；其在拆卸后,可当作一种四旋翼无人机进行独立工作；在需要长途巡航时,拼装好后即可按照复合式垂直起降无人机模式进行作业。(The invention provides a detachable vertical take-off and landing unmanned aerial vehicle, which comprises a body, a rotor wing, wings, an empennage and a horizontal power motor, wherein the rotor wing is arranged on the body; the rotor wing is fixed on the machine body by adopting a cross structure; the wings are connected with the fuselage in an inserting manner; the tail wings are spliced at the tail part of the machine body in a clamping manner; the horizontal power motor is arranged at the front end of the machine body. Comprising four rotors. The detachable vertical take-off and landing unmanned aerial vehicle greatly saves the space required by carrying and transporting; after being disassembled, the unmanned plane can be used as a four-rotor unmanned plane to independently work; when long-distance cruise is needed, operation can be carried out according to the combined type vertical take-off and landing unmanned aerial vehicle mode after the unmanned aerial vehicle is assembled.)

1. The utility model provides a can dismantle VTOL unmanned aerial vehicle of use which characterized in that: comprises a fuselage, a rotor wing, a wing, an empennage and a horizontal power motor; the rotor wing is fixed on the machine body by adopting a cross structure; the wings are connected with the fuselage in an inserting manner; the tail wings are spliced at the tail part of the machine body in a clamping manner; the horizontal power motor is arranged at the front end of the machine body.

2. The detachable VTOL UAV of claim 1, wherein: comprising four rotors.

3. The detachable VTOL UAV of claim 1, wherein: the two wings are inserted on the two sides of the fuselage through a tubular structure which preferably traverses the fuselage.

Technical Field

The invention relates to the technical field of unmanned aerial vehicles, in particular to a vertical take-off and landing unmanned aerial vehicle capable of being detached for use.

Background

Because the vertical take-off and landing unmanned aerial vehicle has the capabilities of vertical take-off and landing and quick maneuvering, the vertical take-off and landing unmanned aerial vehicle is more and more widely applied to the aspects of complex terrain take-off and landing, military reconnaissance, aerial photography and the like. For the VTOL unmanned aerial vehicle, have the characteristics that cruise time is long, take off conveniently, but the existence of its fixed wing makes the occupation amount to the space too big when ground transportation or cluster are put in, has increased the cost of transportation.

Disclosure of Invention

In order to solve the problems, the invention provides a vertical take-off and landing unmanned aerial vehicle capable of being detached for use, which comprises the following components:

A detachable vertical take-off and landing unmanned aerial vehicle is provided, wings are arranged on the unmanned aerial vehicle body and can be detached; the four rotary wings are fixed on the machine body in a cross structure; the tail wing is arranged at the rear part of the fuselage and can be detached; the horizontal power motor is arranged on the machine head.

For easier and more reliable flight, the structure of the drone is as simple as possible.

The utility model provides a can dismantle VTOL unmanned aerial vehicle who uses, two wings are through the tubular structure of a desirable cross fuselage, peg graft in the fuselage both sides.

the utility model provides a can dismantle unmanned aerial vehicle that takes off and land that uses, the fin passes through the mode of joint and fuselage afterbody connection.

The advantages of the invention are as follows:

The detachable vertical take-off and landing unmanned aerial vehicle greatly saves the space required by carrying and transporting; after being disassembled, the unmanned plane can be used as a four-rotor unmanned plane to independently work; when long-distance cruise is needed, operation can be carried out according to the combined type vertical take-off and landing unmanned aerial vehicle mode after the unmanned aerial vehicle is assembled.

Drawings

FIG. 1 is a schematic top view of the present invention.

Detailed Description

The present invention will be described in further detail with reference to the following examples and the accompanying drawings.

As shown in fig. 1, a vertical take-off and landing unmanned aerial vehicle capable of being detached for use comprises a body 1, a rotor 2, wings 3, a tail 4 and a horizontal power motor; the rotor 2 is fixed on the fuselage 1 by adopting a cross structure; the wings 3 are connected with the fuselage 1 in an inserting manner; the tail wing 4 is spliced at the tail part of the machine body 1 in a clamping manner; the horizontal power motor is arranged at the front end of the machine body 1.

Comprising four rotors 2.

Two wings 3 are inserted on both sides of the fuselage 1 through a tubular structure which preferably traverses the fuselage 1.

The utility model provides a can dismantle VTOL unmanned aerial vehicle that uses, wing 3 and fin 4 are dismantling the back, can be independent as 2 unmanned aerial vehicles of a four rotors to carry out independent operation.

The wings 3 can be connected with the fuselage 1 by a splicing method, and the tail wings 4 are connected with the tail part of the fuselage 1 by a clamping method. After the assembly is completed, the aircraft can vertically take off and then is converted into fixed wing flight through simple operation to carry out long-distance operation.

on the basis of the prior art, the detachable vertical take-off and landing unmanned aerial vehicle is more convenient to carry and transport and saves space through modular processing, and the unmanned aerial vehicle can be operated in a multi-rotor 2 mode and a fixed wing mode, so that the unmanned aerial vehicle is fully utilized. The operation is freely changed according to different working environments and operation requirements.