CN209938932U - Folding unmanned aerial vehicle - Google Patents

Abstract

The embodiment of the application discloses foldable unmanned aerial vehicle, foldable unmanned aerial vehicle includes an organism, a camera device, 2N wings and 2N telescopic guide, camera device locates on the organism, N the wing is located one side of organism, N in addition the wing is located the opposite side of organism, each the wing is through one telescopic guide installs extremely the organism, telescopic guide is extendible or shortens, thereby makes the wing can be followed and is kept away from or be close to the direction of organism removes, wherein, N is 1 or is greater than 1 natural number. This foldable unmanned aerial vehicle is collapsible or expand, conveniently carries.

Description

Folding unmanned aerial vehicle

Technical Field

The embodiment of the application relates to the technical field of unmanned aerial vehicles, especially relates to a foldable unmanned aerial vehicle.

Background

A drone is an unmanned aerial vehicle that is operated by a radio remote control device or by its own programmed control means. With the rapid development of the unmanned aerial vehicle industry, more and more unmanned aerial vehicles are applied to industries such as agriculture, forestry, electric power, surveying and mapping, remote measurement and the like. Unmanned aerial vehicle can realize image real-time transport, high-risk area and survey the function through carrying on multiclass sensor, and wherein, unmanned aerial vehicle obtains the wide application in a plurality of fields.

Based on cell-phone App and advanced airborne equipment, unmanned aerial vehicle shoots the function now and possess: the system has the functions of automatic tracking shooting, automatic surrounding shooting, face recognition, voice control, one-key shooting of small videos and the like. However, in order to bring convenience for users to carry in a trip, a folding unmanned aerial vehicle is to be provided.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a foldable unmanned aerial vehicle, collapsible or expansion conveniently carry.

In order to achieve the above object, the utility model discloses a foldable unmanned aerial vehicle, foldable unmanned aerial vehicle includes an organism, a camera device, 2N wings and 2N telescopic guide, camera device locates on the organism, N the wing is located one side of organism, N in addition the wing is located the opposite side of organism, each the wing is through one telescopic guide installs extremely the organism, telescopic guide is extendible or shortens, thereby makes the wing can be followed and is kept away from or be close to the direction of organism removes, wherein, N is 1 or is greater than 1 natural number.

Further, the image pickup device is provided at an end portion of the body.

Furthermore, one end of the machine body penetrates through the upper surface and the lower surface to be provided with an installation groove, and the camera shooting device is pivotally arranged in the installation groove.

Furthermore, the wing includes a motor and locates the screw on the motor, the motor is located on the telescopic rail.

Furthermore, the telescopic guide rail is a multi-section guide rail which is sleeved.

Further, foldable unmanned aerial vehicle still includes both sides board and link mechanism, two the curb plate is located respectively the both sides of organism, the wing reaches telescopic guide is located two between the curb plate, link mechanism connects the curb plate extremely the organism, link mechanism is scalable to make the curb plate be close to or keep away from the organism.

Further, the number of the link mechanisms is 4, wherein 2 of the link mechanisms respectively connect the upper end and the lower end of one side plate to the upper end and the lower end of the machine body, and the other 2 of the link mechanisms respectively connect the upper end and the lower end of the other side plate to the upper end and the lower end of the machine body.

Furthermore, the wings are connected with the connecting rod mechanisms, and the telescopic guide rails can be driven to extend or shorten by unfolding or folding the connecting rod mechanisms.

Further, the link mechanism comprises a plurality of rows of telescopic diamond-shaped links or a plurality of rows of telescopic hexagonal links.

Furthermore, foldable unmanned aerial vehicle still includes a battery unit and a interface that charges, the battery unit is located in the organism, the interface that charges is located on the organism for the battery unit charges.

Has the advantages that: the utility model discloses a foldable unmanned aerial vehicle includes an organism, a camera device, 2N wings and 2N telescopic guide, camera device locates on the organism, N the wing is located one side of organism, another N the wing is located the opposite side of organism, each the wing is through one telescopic guide installs extremely the organism, telescopic guide is extendible or shortens, thereby makes the wing can be followed and is kept away from or be close to the direction of organism removes, wherein, N is 1 or is greater than 1 natural number. The telescopic guide rail is extended to enable the wing to reach a proper position, so that the wing is convenient to use; the telescopic guide rail is shortened, so that the wings are close to the machine body as much as possible, and the telescopic guide rail is convenient to pack and carry.

Drawings

Fig. 1 is a first schematic view of the folding unmanned aerial vehicle of the present invention, showing the retractable diamond-shaped link;

FIG. 2 is an exploded view of FIG. 1;

fig. 3 is a second schematic view of the folding drone of the present invention, showing the retractable hexagonal link;

FIG. 4 is an exploded view of FIG. 2;

fig. 5 is the utility model discloses foldable unmanned aerial vehicle's camera device's structural schematic.

Detailed Description

In order to make the objects, technical solutions and advantages of the present application more apparent, specific embodiments of the present application will be described in detail with reference to the accompanying drawings. It is to be understood that the specific embodiments described herein are merely illustrative of the application and are not limiting of the application. It should be further noted that, for the convenience of description, only some but not all of the relevant portions of the present application are shown in the drawings. Before discussing exemplary embodiments in more detail, it should be noted that some exemplary embodiments are described as processes or methods depicted as flowcharts. Although a flowchart may describe the operations (or steps) as a sequential process, many of the operations can be performed in parallel, concurrently or simultaneously. In addition, the order of the operations may be re-arranged. The process may be terminated when its operations are completed, but may have additional steps not included in the figure. The processes may correspond to methods, functions, procedures, subroutines, and the like.

The utility model aims at providing a foldable unmanned aerial vehicle 1, collapsible or expansion conveniently carries. As shown in fig. 1 to 4, the folding type unmanned aerial vehicle 1 includes a body 10, a camera device 20, 2N wings 30, 2N telescopic guide rails 40, two side plates 50, and a link mechanism 60.

The camera device 20 is disposed on the machine body 10, and specifically, the camera device 20 is disposed at an end portion of the machine body 10, and a viewing angle of the camera device 20 is adjustable. In another embodiment, as shown in fig. 5, an end of the body 10 is provided with a mounting groove 11 penetrating through the upper and lower surfaces, the camera device 20 is pivotally mounted in the mounting groove 11, and the pivotal structure enables the shooting angle of the camera device 20 to be larger.

With reference to fig. 1 to 4, N wings 30 are disposed on one side of the body 10, and the other N wings 30 are disposed on the other side of the body 10. N is 1 or a natural number greater than 1, and in the present embodiment, N is 2. The wing 30 includes an electric motor 32 and a propeller 34 mounted on the motor 32. Each wing 30 is mounted to the airframe 10 by a telescopic rail 40, the telescopic rail 40 being extendable or retractable so that the wing 30 can move in a direction away from or toward the airframe 10, wherein the motor 32 is disposed on the telescopic rail 40. The telescopic guide rail 40 is a multi-section guide rail which is sleeved; a sliding groove may be provided in the body 10 along which the telescopic guide rail 40 slides to extend or retract with respect to the body 10; other structures of the telescopic guide rail 40 that can play the same role are all applicable to this scheme.

The two side plates 50 are respectively arranged at two sides of the machine body 10, the wings 30 and the telescopic guide rails 40 are positioned between the two side plates 50, the link mechanism 60 connects the side plates 50 to the machine body 10, and the link mechanism 60 can extend and retract, so that the side plates 50 are close to or far away from the machine body 10. The number of the link mechanisms 60 is 4, wherein 2 link mechanisms 60 respectively connect the upper end and the lower end of one side plate 50 to the upper end and the lower end of the machine body 10, and the other 2 link mechanisms 60 respectively connect the upper end and the lower end of the other side plate 50 to the upper end and the lower end of the machine body 10.

The connecting rod mechanisms 60 are arranged above and below the wings 30 and the telescopic guide rails 40, so that in order to facilitate the operation of extending or shortening the telescopic guide rails 40, the wings 30 are connected with the connecting rod mechanisms 60, and the telescopic guide rails 40 can be driven to extend or shorten by unfolding or folding the connecting rod mechanisms 60.

The linkage mechanism 60 includes a plurality of rows of retractable diamond-shaped links (as shown in fig. 1-2) or a plurality of rows of retractable hexagonal-shaped links (as shown in fig. 3-4).

Foldable unmanned aerial vehicle 1 still includes a battery unit (not shown) and a interface that charges (not shown), and in the battery unit located organism 10, the interface that charges was located on organism 10 for charge for the battery unit.

Has the advantages that: the utility model discloses a foldable unmanned aerial vehicle 1 includes a organism 10, a camera device 20, 2N individual wing 30 and 2N telescopic guide 40, camera device 20 is located on organism 10, one side of organism 10 is located to N individual wing 30, the opposite side of organism 10 is located to N individual wing 30 in addition, each wing 30 is installed to organism 10 through a telescopic guide 40, telescopic guide 40 is extendible or shorten, thereby make wing 30 can follow the direction removal of keeping away from or being close to organism 10, wherein, N is 1 or is greater than 1 natural number. The telescopic guide rail 40 is extended to enable the wing 30 to reach a proper position, so that the use is convenient; the telescoping rail 40 is shortened to bring the wing 30 as close to the airframe 10 as possible for convenient stowage and carrying.

The foregoing is considered as illustrative of the preferred embodiments of the invention and the technical principles employed. The present application is not limited to the particular embodiments described herein, but is capable of various obvious changes, rearrangements and substitutions as will now become apparent to those skilled in the art without departing from the scope of the invention. Therefore, although the present application has been described in more detail with reference to the above embodiments, the present application is not limited to the above embodiments, and may include other equivalent embodiments without departing from the spirit of the present application, and the scope of the present application is determined by the scope of the claims.

Claims (10)

1. A foldable drone, characterized in that it comprises:

a body;

the camera device is arranged on the machine body;

the N wings are arranged on one side of the machine body, and the other N wings are arranged on the other side of the machine body; and

2N telescopic guide rails, wherein each wing is installed on the machine body through one telescopic guide rail, and the telescopic guide rails can be extended or shortened, so that the wings can move in the direction far away from or close to the machine body;

wherein N is 1 or a natural number more than 1.

2. The foldable unmanned aerial vehicle of claim 1, wherein the camera device is disposed at an end of the body.

3. The foldable unmanned aerial vehicle of claim 1 or 2, wherein an end of the body has a mounting slot passing through the upper and lower surfaces, and the camera device is pivotally mounted in the mounting slot.

4. The foldable unmanned aerial vehicle of claim 1, wherein the wing comprises a motor and a propeller disposed on the motor, and the motor is disposed on the telescopic rail.

5. The folding drone of claim 1, wherein the telescoping rail is a telescoping multi-section rail.

6. The folding drone of claim 1, further comprising:

the two side plates are respectively arranged on two sides of the machine body, and the wing and the telescopic guide rail are positioned between the two side plates; and

and the connecting rod mechanism is connected with the side plate to the machine body and can stretch out and draw back, so that the side plate is close to or far away from the machine body.

7. A folding drone according to claim 6, characterised in that there are 4 said linkages, of which 2 connect the upper and lower ends of one of said side plates to the upper and lower ends of the body, respectively, and 2 connect the upper and lower ends of the other of said side plates to the upper and lower ends of the body, respectively.

8. The foldable unmanned aerial vehicle of claim 6, wherein the wings are connected to the linkage mechanism, and the telescopic rail is extended or shortened by unfolding or folding the linkage mechanism.

9. A folding drone according to claim 6, characterised in that the linkage comprises rows of telescopic diamond links or rows of telescopic hexagonal links.

10. The folding drone of claim 1, further comprising:

the battery unit is arranged in the machine body; and

and the charging interface is arranged on the machine body and used for charging the battery unit.

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