CN220147598U - GPS support and unmanned aerial vehicle - Google Patents

Abstract

The embodiment of the utility model provides a GPS (Global positioning System) bracket and an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. The GPS bracket comprises a mounting frame and a buckling piece. The mounting bracket includes installation department, supporting part and buckling parts, and the both ends of supporting part are connected with buckling parts and installation department respectively, and the installation department is used for installing GPS, and the buckling piece is connected with the one end that supporting part was kept away from to buckling parts, and the buckling piece and buckling parts prescribe a limit to the lock space jointly. Because the both ends of supporting part are connected with buckling parts and installation department respectively for the GPS support has certain height, when the installation department at the mounting bracket is installed to GPS, and the supporting part can support certain height with GPS, makes GPS can keep away from the buckling parts of mounting bracket, thereby reduces GPS and installs the interference to GPS at the unmanned aerial vehicle upper time body inside components and parts. The unmanned aerial vehicle provided by the utility model comprises a GPS bracket.

Description

GPS support and unmanned aerial vehicle

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a GPS bracket and an unmanned aerial vehicle.

Background

Unmanned aerial vehicles are a collective name of unmanned aerial vehicles, are provided with equipment such as an autopilot, a program control device and the like, and can track and position flying equipment through ground stations or flying hands. Compared with manned plane, it has the advantages of small size, low cost, convenient use, etc. and may be taken off vertically under radio remote control, recovered, landed automatically and reused.

The inventor researches find that when the GPS is installed on the unmanned aerial vehicle by using some existing GPS brackets, the GPS can generate larger interference with components in the unmanned aerial vehicle body.

Disclosure of Invention

The utility model aims to provide a GPS bracket which can reduce the interference between a GPS and components in an unmanned aerial vehicle body.

Embodiments of the present utility model are implemented as follows:

in a first aspect, the present utility model provides a GPS bracket for use in an unmanned aerial vehicle, comprising:

the mounting frame comprises a mounting part, a supporting part and a buckling part, wherein two ends of the supporting part are respectively connected with the buckling part and the mounting part, and the mounting part is used for mounting a GPS;

the buckling piece is connected with one end of the buckling part far away from the supporting part, and the buckling space is defined by the buckling piece and the buckling part together.

In an alternative embodiment, the buckling part comprises a first connecting plate, a third connecting plate and two second connecting plates, the first connecting plate is connected with the supporting part, the first connecting plate and the third connecting plate are arranged at intervals along a first direction, the two second connecting plates are arranged at intervals along a second direction, and a first included angle is formed between the first direction and the second direction;

the first connecting plate and the third connecting plate are both provided with a first buckling groove, the two second connecting plates are located at the notch end of the first buckling groove, two sides of each second connecting plate are connected with the first connecting plate and the second connecting plate respectively, and the second connecting plates are used for being connected with buckling pieces.

In an alternative embodiment, the two second connection plates are located on the same plane, the plane on which the first connection plate is located forms a second included angle with the plane on which the second connection plate is located, and the plane on which the third connection plate is located forms a third included angle with the plane on which the second connection plate is located.

In an alternative embodiment, the second web is provided with a first mounting hole and the fastener is provided with a second mounting hole corresponding to the first mounting hole.

In an alternative embodiment, the fastener comprises two first matching plates arranged at intervals along a first direction and two second matching plates arranged at intervals along a second direction, wherein the first direction and the second direction form a first included angle;

the two first matching plates are provided with second buckling grooves, the two second matching plates are located at notch ends of the second buckling grooves, two sides of each second matching plate are connected with the two first matching plates respectively, and the second matching plates are used for being connected with buckling parts.

In an alternative embodiment, the two second mating plates are located on the same plane, and the plane of each first mating plate forms a fourth included angle with the plane of the second mating plate.

In an alternative embodiment, the two first mating plates are parallel to each other and the fourth included angle is 90 °.

In an alternative embodiment, the end of the first mating plate remote from the second mating plate forms a plane.

In an alternative embodiment, the fastening portion of the mounting frame is provided with a first mounting hole, and the second mating plate is provided with a second mounting hole corresponding to the first mounting hole.

In an alternative embodiment, the fastener has a semi-circular shape in a projection along the first direction.

In an alternative embodiment, the number of the fastening pieces, the supporting portions and the fastening portions is plural, and the plural supporting portions are disposed on the mounting portion at intervals along the first direction, and each fastening portion is connected with one fastening piece.

In an alternative embodiment, the number of the fastening pieces, the number of the supporting portions and the number of the fastening portions are two, and the two supporting portions are arranged on the outer peripheral edge of the mounting portion at intervals along the first direction.

In an alternative embodiment, at least one of the support portion, the mounting portion and the fastening portion is provided with a lightening hole.

In an alternative embodiment, the mounting portion is provided with a wire passing hole and a plurality of third mounting holes, the plurality of third mounting holes are distributed at intervals along the circumferential direction of the mounting portion, the third mounting holes are used for mounting the GPS, and the wire passing hole is used for enabling a signal wire of the GPS to pass through.

In an alternative embodiment, the mounting frame is integrally tower-like in configuration.

In an alternative embodiment, the buckling part of the mounting frame is provided with a first mounting hole, and the buckling piece is provided with a second mounting hole corresponding to the first mounting hole; the GPS bracket further comprises a fastener connected with the first mounting hole and the second mounting hole, and the buckling part of the mounting frame is fastened and connected with the buckling piece through the first mounting hole, the second mounting hole and the fastener.

In an alternative embodiment, the mounting frame is integrally formed by stamping from sheet metal; and/or

The buckling piece is formed by stamping and integrating metal plates.

In a second aspect, the present utility model provides an unmanned aerial vehicle, comprising a casing, a frame, a GPS and any of the GPS brackets in the foregoing embodiments, the casing being connected to the frame, the GPS bracket being snap-fit connected to the frame, the GPS being mounted on the GPS bracket.

The embodiment of the utility model has the beneficial effects that: the embodiment of the utility model provides a GPS (Global positioning System) bracket and an unmanned aerial vehicle. The mounting bracket includes installation department, supporting part and buckling parts, and the both ends of supporting part are connected with buckling parts and installation department respectively, and the installation department is used for installing GPS, and the buckling piece is connected with the one end that supporting part was kept away from to buckling parts, and the buckling piece and buckling parts prescribe a limit to the lock space jointly. Because the both ends of supporting part are connected with buckling parts and installation department respectively for the GPS support has certain height, when the installation department at the mounting bracket is installed to GPS, and the supporting part can support certain height with GPS, makes GPS can keep away from the buckling parts of mounting bracket, thereby reduces GPS and installs the interference to GPS at the unmanned aerial vehicle upper time body inside components and parts. The unmanned aerial vehicle provided by the utility model comprises the GPS bracket, so that the unmanned aerial vehicle has the advantages.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the drawings that are needed in the embodiments will be briefly described below, it being understood that the following drawings only illustrate some embodiments of the present utility model and therefore should not be considered as limiting the scope, and other related drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.

FIG. 1 is a schematic diagram of a GPS bracket and GPS and frame assembly provided by an embodiment of the present utility model;

FIG. 2 is a schematic diagram of a GPS bracket and GPS assembly according to an embodiment of the present utility model;

fig. 3 is a schematic structural view of a mounting frame according to an embodiment of the present utility model;

FIG. 4 is a schematic structural view of a fastener according to an embodiment of the present utility model.

Icon 1-GPS cradle; 10-mounting frame; 11-an installation part; 111-a third mounting hole; 112-wire vias; 12-a support; 13-a buckling part; 131-a first connection plate; 132-a second connection plate; 1321-a first mounting hole; 133-a third connection plate; 134-first snap groove; 14-lightening holes; 20-a fastener; 21-a first mating plate; 22-a second mating plate; 221-a second mounting hole; 23-a second buckling groove; 30-a screw; 40-self-locking nut; 2-GPS; 3-frame.

Detailed Description

For the purpose of making the objects, technical solutions and advantages of the embodiments of the present utility model more apparent, the technical solutions of the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model, and it is apparent that the described embodiments are some embodiments of the present utility model, but not all embodiments of the present utility model. The components of the embodiments of the present utility model generally described and illustrated in the figures herein may be arranged and designed in a wide variety of different configurations.

Thus, the following detailed description of the embodiments of the utility model, as presented in the figures, is not intended to limit the scope of the utility model, as claimed, but is merely representative of selected embodiments of the utility model. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

It should be noted that: like reference numerals and letters denote like items in the following figures, and thus once an item is defined in one figure, no further definition or explanation thereof is necessary in the following figures.

In the description of the present utility model, it should be noted that, directions or positional relationships indicated by terms such as "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., are directions or positional relationships based on those shown in the drawings, or are directions or positional relationships conventionally put in use of the inventive product, are merely for convenience of describing the present utility model and simplifying the description, and are not indicative or implying that the apparatus or element to be referred to must have a specific direction, be constructed and operated in a specific direction, and thus should not be construed as limiting the present utility model. Furthermore, the terms "first," "second," "third," and the like are used merely to distinguish between descriptions and should not be construed as indicating or implying relative importance.

Furthermore, the terms "horizontal," "vertical," and the like do not denote a requirement that the component be absolutely horizontal or overhang, but rather may be slightly inclined. As "horizontal" merely means that its direction is more horizontal than "vertical", and does not mean that the structure must be perfectly horizontal, but may be slightly inclined.

In the description of the present utility model, it should also be noted that, unless explicitly specified and limited otherwise, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.

The specific structure of the GPS bracket and the corresponding technical effects thereof provided by the embodiment of the utility model are described in detail below with reference to the accompanying patent drawings.

Referring to fig. 1-2, a GPS bracket 1 according to an embodiment of the present utility model includes a mounting frame 10 and a fastener 20.

The mounting frame 10 comprises a mounting part 11, a supporting part 12 and a buckling part 13, wherein two ends of the supporting part 12 are respectively connected with the buckling part 13 and the mounting part 11, the mounting part 11 is used for mounting the GPS2, the buckling piece 20 is connected with one end, far away from the supporting part 12, of the buckling part 13, and the buckling piece 20 and the buckling part 13 jointly define a buckling space.

In other words, since the two ends of the supporting portion 12 are respectively connected with the fastening portion 13 and the mounting portion 11, when the GPS2 is mounted on the mounting portion 11, the GPS2 and the fastening portion 13 can have a certain distance under the action of the supporting portion 12, that is, the supporting portion 12 can support the GPS2 at a certain height, so that the GPS2 can be far away from the fastening portion 13 of the mounting frame 10, and thus, the interference of components in the body to the GPS when the GPS2 is mounted on the unmanned aerial vehicle is reduced.

It should be noted that, in this embodiment, the fastening space formed by connecting the fastening portion 13 and the fastening member 20 is used for being connected with the frame 3 of the unmanned aerial vehicle, when assembling, the fastening portion 13 may be attached to the frame 3 of the unmanned aerial vehicle, and then the fastening member 20 is connected with the fastening portion 13, so that a portion of the frame 3 of the unmanned aerial vehicle is located in the fastening space to complete the assembling.

It can be appreciated that the frame 3 is located inside the casing of the unmanned aerial vehicle, the GPS bracket 1 is mounted on the frame 3 of the unmanned aerial vehicle, that is, the GPS bracket 1 is located inside the casing of the unmanned aerial vehicle, the GPS2 is also located inside the casing of the unmanned aerial vehicle, and compared with the GPS mounted outside the casing, the GPS2 is mounted inside the casing, so that the influence of the external environment on the GPS2 can be avoided, and meanwhile, the wind resistance in the flight process of the unmanned aerial vehicle can be reduced.

Of course, in other embodiments, the fastening space created by the attachment of the fastening portion 13 to the fastening member 20 is used for attachment to other locations on the drone.

Further, the number of the fastening members 20, the supporting portions 12 and the fastening portions 13 is plural, the plurality of supporting portions 12 are disposed on the mounting portion 11 at intervals along the first direction, and each fastening portion 13 is connected to one fastening member 20.

It can be appreciated that, since the plurality of supporting portions 12 and the fastening portion 13 are provided, and the supporting portions 12 are disposed at intervals along the first direction on the mounting portion 11, the overall strength of the mounting frame 10 can be enhanced by the arrangement of the plurality of supporting portions 12, so as to avoid easy damage thereof.

And the connection stability with the frame 3 of the unmanned aerial vehicle can be enhanced through the cooperation of the plurality of buckling parts 13 and the buckling parts 20.

The above-mentioned plural means two or more.

Specifically, in the present embodiment, the number of the fastening members 20, the number of the supporting portions 12, and the number of the fastening portions 13 are two, and the two supporting portions 12 are disposed at intervals along the first direction on the outer periphery of the mounting portion 11.

In detail, in the present embodiment, the mounting portion 11 has a rectangular plate shape, and the two supporting portions 12 are respectively connected to two opposite side walls of the mounting portion 11 in the first direction, so that the width of the mounting frame 10 in the first direction is increased to ensure stable support of the mounting portion 11.

Of course, in other embodiments, the mounting portion 11 may have other shapes, which are not specifically limited herein.

It can be appreciated that in this embodiment, the two supporting portions 12 are respectively disposed at the peripheral edges of the mounting portion 11, so that the mounting portion 11 can be supported, the strength of the mounting frame 10 is also ensured, the weight of the mounting frame 10 is also moderate, and the weight of the mounting frame 10 is prevented from being excessively heavy, so that the weight of the unmanned aerial vehicle is increased.

The whole tower-shaped structure that is of the installation frame 10, namely, the two supporting parts 12 and the installation part 11 form the installation frame 10 in a tower shape, the width of the GPS bracket 1 is increased, the structural strength of the installation frame 10 is ensured, and the installation frame 10 is also enabled to have a certain height, so that the interference of the GPS installed on the installation part 11 and the internal components of the unmanned aerial vehicle is reduced.

In other embodiments, the number of fasteners 20, supports 12, and fasteners 13 may be three, four, or five.

Further, in order to reduce the weight of the mount 10, at least one of the mount portion 11, the support portion 12, and the engagement portion 13 is provided with a weight-reducing hole 14.

In the present embodiment, the support portion 12 is provided with the lightening hole 14. It will be appreciated that the support 12 is provided with weight-reducing apertures 14 which, while reducing the weight of the mount 10, also facilitate the threading of the signal lines for the GPS2 and for the GPS2.

Of course, in other embodiments, only the mounting portion 11 may be provided with the lightening hole 14, only the engaging portion 13 may be provided with the lightening hole 14, only the mounting portion 11 and the supporting portion 12 may be provided with the lightening hole 14, only the mounting portion 11 and the engaging portion 13 may be provided with the lightening hole 14, only the supporting portion 12 and the engaging portion 13 may be provided with the lightening hole 14, or all of the mounting portion 11, the supporting portion 12 and the engaging portion 13 may be provided with the lightening hole 14.

Referring to fig. 3, in detail, the fastening portion 13 includes a first connecting plate 131, a third connecting plate 133, and two second connecting plates 132, where the first connecting plate 131 is connected to the supporting portion 12, the first connecting plate 131 and the third connecting plate 133 are arranged at intervals along a first direction, and the two second connecting plates 132 are arranged at intervals along a second direction, and the first direction and the second direction form a first included angle. The first connecting plate 131 and the third connecting plate 133 are respectively provided with a first buckling groove 134, the two second connecting plates 132 are positioned at the notch ends of the first buckling grooves 134, two sides of each second connecting plate 132 are respectively connected with the first connecting plate 131 and the third connecting plate 133, and the second connecting plates 132 are used for being connected with the buckling pieces 20.

Optionally, the two second connecting plates 132 are located on the same plane, the plane on which the first connecting plate 131 is located forms a second included angle with the plane on which the second connecting plate 132 is located, and the plane on which the third connecting plate 133 is located forms a third included angle with the plane on which the second connecting plate 132 is located.

Optionally, the first included angle is 90 °, the second included angle is 90 °, and the third included angle is 90 °, that is, the first direction is perpendicular to the second direction, the plane of the first connecting plate 131 is perpendicular to the plane of the second connecting plate 132, and the plane of the third connecting plate 133 is perpendicular to the plane of the second connecting plate 132. However, the present utility model is not limited thereto, and the first angle, the second angle and the third angle may be appropriately adjusted according to actual needs. In this embodiment, it can be understood that, through the above arrangement, the first connecting plate 131 and the third connecting plate 133 are arranged at intervals along the first direction, and two sides of each second connecting plate 132 are connected with the first connecting plate 131 and the third connecting plate 133 respectively, and the two second connecting plates 132 are arranged at intervals along the second direction, so that the strength of the fastening portion 13 can be increased while the weight of the fastening portion can be ensured not to be excessively heavy, and the space between the first connecting plate 131 and the third connecting plate 133 can be understood as a weight-reducing space, so that the strength of the fastening portion can be ensured while the weight of the fastening portion can be reduced.

It should be noted that, the shapes of the first fastening grooves 134 formed on the first connecting plate 131 and the third connecting plate 133 are matched with the frame 3 of the unmanned aerial vehicle, so as to be attached to the frame 3 of the unmanned aerial vehicle, and the two second connecting plates 132 are connected with the fastening pieces 20, so that the connection strength with the fastening pieces 20 can be improved.

In this embodiment, the fastening portion 13 of the mounting bracket 10 is provided with a first mounting hole 1321, and the fastening member 20 is provided with a second mounting hole 221 corresponding to the first mounting hole 1321; the GPS bracket 1 further includes a fastener coupled to the first mounting hole 1321 and the second mounting hole 221, and the fastening portion 13 of the mounting bracket 10 is fastened to the fastening member 20 through the first mounting hole 1321, the second mounting hole 221, and the fastener. Specifically, the second connection plate 132 of the fastening portion 13 is provided with a first mounting hole 1321, and the fastening member 20 is provided with a second mounting hole 221 corresponding to the first mounting hole 1321. Of course, in other embodiments, the fastener 20 may also be coupled to the mounting frame 10 by being snapped or welded to the second connecting plate 132 to allow the mounting frame 10 to be assembled to a drone.

So long as it is ensured that the fastener 20 is stably mounted on the unmanned aerial vehicle after being connected to the second connecting plate 132.

In this embodiment, the fastener includes the screw 30 and the self-locking nut 40, that is, when the GPS bracket 1 is mounted on the frame 3 of the unmanned aerial vehicle, the groove wall of the first fastening groove 134 of the fastening portion 13 may be attached to the frame 3, and the fastening member 20 may be attached to the second connecting plate 132 of the fastening portion 13, so that the first mounting hole 1321 corresponds to the second mounting hole 221, and then the bolt passes through the first mounting hole 1321 and the second mounting hole 221, and the self-locking nut 40 is screwed. It can be appreciated that the GPS bracket 1 can be effectively and firmly installed on the unmanned aerial vehicle through the screw 30 and the self-locking nut 40, and the self-locking nut 40 has a good anti-loosening effect.

Of course, in alternative embodiments, the fastener may also be a screw 30 and clinch nut.

Alternatively, in other embodiments, the fastener may be a screw 30 or other types of nuts, so long as the GPS bracket 1 is stably mounted on the frame 3 of the unmanned aerial vehicle.

Further, in this embodiment, in order to ensure the overall strength of the mounting frame 10, the mounting frame 10 is integrally formed by stamping a metal plate, that is, the mounting portion 11, the supporting portion 12 and the fastening portion 13 are integrally formed by stamping a metal plate.

It is easy to understand that since the mounting frame 10 is integrally formed by stamping a metal plate, the mounting frame 10 has not only a high overall structural strength but also a light weight, and also can reduce its own process cost.

Referring to fig. 4, further, the fastening component 20 includes two first engaging plates 21 spaced apart along a first direction and two second engaging plates 22 spaced apart along a second direction, wherein the first direction and the second direction form a first included angle; the two first matching plates 21 are respectively provided with a second buckling groove 23, the two second matching plates 22 are positioned at the notch ends of the two second buckling grooves 23, two sides of each second matching plate 22 are respectively connected with the two first matching plates 21, and the second matching plates 22 are used for being connected with the buckling parts 13. Alternatively, the clasp 20 is semi-circular in shape as projected in the first direction.

Optionally, the two second mating plates 22 are located on the same plane, and the plane of each first mating plate 21 forms a fourth included angle with the plane of the second mating plate 22.

Optionally, the first angle is 90 °, i.e. the first direction is perpendicular to the second direction. The two first mating plates 21 are parallel to each other and the fourth included angle is 90 °, i.e. the two first mating plates 21 are parallel to each other, and the plane of the first mating plate 21 is perpendicular to the plane of the second mating plate 22. However, the present utility model is not limited in sequence, and the first included angle and the fourth included angle can be properly adjusted according to actual needs.

In the present embodiment, the second connection plate 132 of the fastening portion 13 of the mounting bracket 10 is provided with a first mounting hole 1321, and the second mating plate 22 is provided with a second mounting hole 221 corresponding to the first mounting hole 1321. Specifically, the two second fitting plates 22 correspond to the two second connection plates 132, respectively, and the two second fitting plates 22 are each provided with the second mounting hole 221. During installation, the second mounting holes 221 of the two second matching plates 22 of the fastener 20 correspond to the first mounting holes 1321 of the second connecting plate 132 of the fastening part 13 of the mounting frame 10, the screws 30 penetrate through the first mounting holes 1321 and the second mounting holes 221 and are screwed with nuts, the first fastening grooves 134 are opposite to the second fastening grooves 23, fastening spaces are formed, and at the moment, the groove walls of the first fastening grooves 134 and the second fastening grooves 23 are attached to the frame 3 of the unmanned aerial vehicle, so that the mounting frame 10 and the fastener 20 are fixedly installed.

Similarly, the space where the two first engaging plates 21 are arranged at intervals in the first direction can be also understood as a weight-reduction space, similarly to the engaging portion 13, by the above arrangement, that is, by the above arrangement, not only the strength of the whole of the engaging member 20 is ensured, but also the weight of the engaging member itself can be effectively reduced to reduce the weight of the unmanned aerial vehicle.

In this embodiment, to ensure the overall strength of the fastener 20. The fastener 20 is formed by sheet metal stamping integrally, in other words, the two first mating plates 21 and the two second mating plates 22 of the fastener 20 are formed by sheet metal stamping integrally.

Likewise, the fastener 20 is integrally formed by stamping sheet metal, so that the overall structural strength is high, the weight is light, and the process cost of the fastener can be reduced.

Further, an end of the first mating plate 21 remote from the second mating plate 22 forms a plane. It is easy to understand that the fastener 20 is not easy to align when being installed on the mounting frame 10, and the side, far away from the second matching plate 22, of the first matching plate 21 is set to be a plane structure, so that the fastener 20 can be in a horizontal state by matching with the plane through a tool or other structures, and the fastener 20 can be conveniently and smoothly assembled with the fastening part 13 of the mounting frame 10.

In order to install the GPS2, a side of the installation portion 11 far away from the support portion 12 is provided with a wire passing hole 112 and a plurality of third installation holes 111, the plurality of third installation holes 111 are arranged at intervals along the circumferential direction of the installation portion 11, the third installation 111 is used for installing the GPS2, the wire passing hole 112 is used for allowing a signal wire of the GPS2 to pass through, and the weight of the installation frame 10 can be reduced through the wire passing hole 112.

Specifically, the mounting portion 11 of the mounting frame 10 in this embodiment is rectangular plate-shaped, the number of the third mounting holes 111 is four, and the four third mounting holes 111 are respectively disposed at four corners of the mounting portion 11, so that the GPS2 is stably mounted on the mounting portion 11, and it is easy to understand that the GPS2 is connected with the fastener through the third mounting holes 111. After installation, the signal line of the GPS2 can also be connected with devices inside the unmanned aerial vehicle after passing through the line hole 112.

Optionally, in this embodiment, a fillet is provided at a connection between the mounting portion 11 and the supporting portion 12 of the mounting bracket 10.

Optionally, in this embodiment, a fillet is formed at a connection between the first connecting plate 131 and the second connecting plate 132 of the fastening portion 13 of the mounting bracket 10, and a fillet is formed at a connection between the third connecting plate 133 and the second connecting plate 132.

Optionally, in this embodiment, a fillet is formed at a connection between the first mating plate 21 and the second mating plate 22 of the fastener 20.

In summary, the embodiment of the utility model provides a GPS bracket 1, and the GPS bracket 1 includes a mounting frame 10 and a fastener 20. The mounting frame 10 comprises a mounting part 11, a supporting part 12 and a buckling part 13, wherein two ends of the supporting part 12 are respectively connected with the buckling part 13 and the mounting part 11, the mounting part 11 is used for mounting the GPS2, the buckling piece 20 is connected with one end, far away from the supporting part 12, of the buckling part 13, and the buckling piece 20 and the buckling part 13 jointly define a buckling space. Because the both ends of supporting part 12 are connected with buckling parts 13 and installation department 11 respectively for GPS support 1 has certain height, when GPS2 installs the installation department 11 at mounting bracket 10, supporting part 12 can support certain height with GPS2, makes GPS2 can keep away from buckling parts 13 of mounting bracket 10, thereby reduces the interference of GPS at the inside components and parts of unmanned aerial vehicle when installing. The GPS support 1 provided by the embodiment of the utility model can be arranged on the frame 3 in the shell of the unmanned aerial vehicle, and when the GPS2 is arranged on the GPS support 1, the GPS2 can be far away from the frame 3 of the unmanned aerial vehicle due to the certain height of the GPS support 1, so that the interference of components in the space surrounded by the frame 3 on the GPS can be reduced. Meanwhile, the GPS support 1 of the embodiment of the utility model can be arranged in the shell of the unmanned aerial vehicle, so that the GPS support 1 and the GPS2 are both positioned in the shell of the unmanned aerial vehicle, and the wind resistance in the flight process of the unmanned aerial vehicle can be reduced.

The embodiment of the utility model also provides an unmanned aerial vehicle, which comprises a shell (not shown in the figure), a frame 3, a GPS2 and the GPS support 1, wherein the shell is connected with the frame 3, the GPS support 1 is buckled and connected with the frame 3, and the GPS2 is arranged on the GPS support 1. In other words, the groove wall of the first fastening groove 134 of the fastening portion 13 of the mounting bracket 10 is attached to the frame 3, the groove wall of the second fastening groove 23 of the fastening member 20 is attached to the frame 3 and corresponds to the fastening portion 13, and the nut is screwed through the first mounting hole 1321 of the second connecting plate 132 and the second mounting hole 221 of the second fastening plate 22 by the bolt. If the GPS2 is directly arranged on the frame 3 or the fuselage of the unmanned aerial vehicle, the interference of components in the fuselage on the GPS2 is large; the unmanned aerial vehicle that this embodiment provided, the GPS support 1 that adopts has certain height, through installing GPS2 on GPS support 1, install GPS support 1 on frame 3 for GPS2 can keep away from unmanned aerial vehicle's frame 3, thereby can reduce the interference of components and parts in the space that frame 3 encloses to GPS. If the GPS2 is directly arranged outside the unmanned aerial vehicle or arranged outside the shell through the mounting frame, the wind resistance of the unmanned aerial vehicle is easily increased in the flight process of the unmanned aerial vehicle; the unmanned aerial vehicle that this embodiment provided, frame 3 are located inside the casing, and GPS support 1 is connected with frame 3, and GPS2 is connected with GPS support 1 for GPS2 and GPS support 1 all are located inside unmanned aerial vehicle's the casing, can reduce the windage in the unmanned aerial vehicle flight.

The above description is only of the preferred embodiments of the present utility model and is not intended to limit the present utility model, but various modifications and variations can be made to the present utility model by those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present utility model should be included in the protection scope of the present utility model.

Claims (18)

1. A GPS bracket for use with an unmanned aerial vehicle, comprising:

the GPS device comprises a mounting frame, a GPS device and a GPS device, wherein the mounting frame comprises a mounting part, a supporting part and a buckling part, two ends of the supporting part are respectively connected with the buckling part and the mounting part, and the mounting part is used for mounting the GPS device;

the buckling piece is connected with one end, far away from the supporting part, of the buckling part, and the buckling space is defined by the buckling piece and the buckling part together.

2. The GPS support of claim 1, wherein the GPS support comprises a GPS support body,

the buckling part comprises a first connecting plate, a third connecting plate and two second connecting plates, the first connecting plate is connected with the supporting part, the first connecting plate and the third connecting plate are arranged at intervals along a first direction, the two second connecting plates are arranged at intervals along a second direction, and a first included angle is formed between the first direction and the second direction;

the first connecting plates and the third connecting plates are respectively provided with a first buckling groove, the two second connecting plates are located at notch ends of the first buckling grooves, two sides of each second connecting plate are respectively connected with the first connecting plates and the second connecting plates, and the second connecting plates are used for being connected with buckling pieces.

3. The GPS support of claim 2, wherein the GPS support comprises a GPS support body,

the two second connecting plates are located on the same plane, a second included angle is formed between the plane where the first connecting plate is located and the plane where the second connecting plate is located, and a third included angle is formed between the plane where the third connecting plate is located and the plane where the second connecting plate is located.

4. The GPS support of claim 2, wherein the GPS support comprises a GPS support body,

the second connecting plate is provided with a first mounting hole, and the buckling piece is provided with a second mounting hole corresponding to the first mounting hole.

5. The GPS support of claim 1, wherein the GPS support comprises a GPS support body,

the buckling piece comprises two first matching plates and two second matching plates, wherein the first matching plates are arranged at intervals along a first direction, the second matching plates are arranged at intervals along a second direction, and a first included angle is formed between the first direction and the second direction;

the two first matching plates are provided with second buckling grooves, the two second matching plates are located at notch ends of the second buckling grooves, two sides of each second matching plate are connected with the two first matching plates respectively, and the second matching plates are used for being connected with the buckling parts.

6. The GPS support of claim 5, wherein the GPS support comprises a GPS support body,

the two second matching plates are located on the same plane, and a fourth included angle is formed between the plane where each first matching plate is located and the plane where each second matching plate is located.

7. The GPS support of claim 6, wherein the GPS support comprises a GPS support body,

the two first matching plates are parallel to each other, and the fourth included angle is 90 degrees.

8. The GPS support of claim 5, wherein the GPS support comprises a GPS support body,

one end of the first matching plate far away from the second matching plate forms a plane.

9. The GPS support of claim 5, wherein the GPS support comprises a GPS support body,

the projection of the buckling piece along the first direction is semi-circular.

10. The GPS support of claim 5, wherein the GPS support comprises a GPS support body,

the buckling part of the mounting frame is provided with a first mounting hole, and the second matching plate is provided with a second mounting hole corresponding to the first mounting hole.

11. The GPS support of any one of claims 1-10,

the number of the buckling pieces, the supporting parts and the buckling parts is multiple, the supporting parts are arranged on the mounting part at intervals along the first direction, and each buckling part is connected with one buckling piece.

12. The GPS support of any one of claims 1-10,

the number of the buckling pieces, the number of the supporting parts and the number of the buckling parts are two, and the two supporting parts are arranged at intervals along the first direction and at the periphery of the mounting part.

13. The GPS support of any one of claims 1-10,

at least one of the supporting part, the mounting part and the buckling part is provided with a lightening hole.

14. The GPS support of any one of claims 1-10,

the GPS mounting device comprises a mounting part and is characterized in that a wire passing hole and a plurality of third mounting holes are formed in the mounting part, the third mounting holes are distributed at intervals along the circumferential direction of the mounting part, the third mounting holes are used for mounting the GPS, and the wire passing hole is used for enabling a signal wire of the GPS to pass through.

15. The GPS support of any one of claims 1-10,

the whole tower-shaped structure that is of mounting bracket.

16. The GPS bracket according to any of claims 1-3, 5-9, wherein a first mounting hole is provided in a fastening portion of the mounting bracket, and a second mounting hole corresponding to the first mounting hole is provided in the fastening member; the GPS bracket further comprises a fastener connected with the first mounting hole and the second mounting hole, and the buckling part of the mounting frame is fastened and connected with the buckling piece through the first mounting hole, the second mounting hole and the fastener.

17. The GPS support of any one of claims 1-10,

the mounting frame is integrally formed by stamping a metal plate; and/or

The buckling piece is formed by stamping and integrating metal plates.

18. An unmanned aerial vehicle, comprising a casing, a frame, a GPS and the GPS bracket according to any one of claims 1 to 17, wherein the casing is connected to the frame, the GPS bracket is fastened to the frame, and the GPS is mounted on the GPS bracket.