Mounting structure of GPS positioning module of unmanned aerial vehicle

Abstract

The utility model discloses a mounting structure of an unmanned aerial vehicle GPS positioning module, which comprises an unmanned aerial vehicle GPS positioning module B mounting frame, a fixed vertical rod and a mounting plate connected with the top end of the fixed vertical rod, an unmanned aerial vehicle GPS positioning module B installation cover comprises an installation lower half shell connected with an installation plate, an installation upper half shell connected with the installation lower half shell through threads in a screwed mode and a connecting stud perpendicular to the circle center position of the surface of the bottom of the installation lower half shell, and a circular ring edge is arranged on the outer surface of the installation upper half shell. The limiting assembly comprises a fixed sleeve arranged on the outer side of the fixed vertical rod in a sleeving mode; according to the utility model, the unmanned aerial vehicle GPS positioning module B is convenient to disassemble and assemble and has a protective mounting design, the connecting method of the mounting lower half shell and the mounting upper half shell for mounting the unmanned aerial vehicle GPS positioning module B is simple, the number of screws is reduced, the unmanned aerial vehicle GPS positioning module B is convenient to assemble, and the fixing plate and the protective net plate protect the outer side of the box body, so that the protective property is achieved; and the box body is prevented from being collided and damaged.

Description

TECHNICAL FIELD

[0001] The utility model belongs to unmanned plane GPS module installation device technical field, specifically related to a kind of installation structure of unmanned plane GPS positioning module. BACKGROUND

[0002] Unmanned plane GPS positioning module is integrated RF radio frequency chip, baseband chip and core CPU, and is added relevant peripheral circuit and is composed of circuit device, and unmanned plane GPS positioning module and other devices, such as GPS receiver, antenna, processor and output interface, are jointly composed of complete GPS positioning processing device, and the specific working principle of GPS positioning processing device is that GPS module on unmanned plane receives radio signal from GPS satellite through antenna, these signals carry satellite positioning and time information, after amplification, filtering, demodulation etc., effective GPS signal is extracted, and the position coordinate of unmanned plane is calculated through trigonometry etc.

[0003] In the above-mentioned unmanned plane GPS positioning module installation process, more screws are needed, and the disassembly and assembly of unmanned plane GPS positioning module need to disassemble and assemble screws, and the disassembly and assembly of unmanned plane GPS positioning module installed in the box body are more cumbersome, in addition, the box body is placed at a certain height from the unmanned plane, and the box body is placed in the air, in the flight process of unmanned plane, the box body may be hit or damaged, resulting in failure of unmanned plane GPS positioning module in the box body;The box body containing unmanned plane GPS positioning module is not protected on the vertical rod support, and the box body cannot be opened, and after replacing unmanned plane GPS positioning module, it is reassembled.

[0004] The existing unmanned plane GPS positioning module is installed at a certain height on unmanned plane, and there is no installation design that is convenient for disassembling and assembling unmanned plane GPS positioning module and has protection, therefore, the application provides an installation structure of unmanned plane GPS positioning module. UTILITY MODEL CONTENTS

[0005] The utility model aims at providing an installation structure of unmanned plane GPS positioning module to solve the problem of no installation design that is convenient for disassembling and assembling unmanned plane GPS positioning module and has protection in the above background technology.

[0006] To achieve the above object, the utility model provides the following technical scheme: an installation structure of unmanned plane GPS positioning module, comprising

[0007] Unmanned plane GPS positioning module B mounting bracket, including fixed vertical rod, and the installation plate is connected with the top end of fixed vertical rod.

[0008] The unmanned aerial vehicle GPS positioning module B mounting cover comprises a mounting lower half shell connected with a mounting plate, a mounting upper half shell connected with the mounting lower half shell through thread screwing, and a connecting stud vertically mounted at the center position of the bottom surface of the mounting lower half shell, and the outer surface of the mounting upper half shell is provided with a circular ring edge.

[0009] The limiting assembly comprises a fixing sleeve sleeved outside the fixing vertical rod, elastic rods symmetrically distributed on the fixing sleeve, and a limiting sleeve threadedly and rotatably connected with one end of the elastic rod, and the elastic rod is provided with a blocking piece.

[0010] The protection piece comprises a fixing plate mounted outside the mounting upper half shell, protection net plates symmetrically mounted on the fixing plate, and a limiting piece connected with the fixing plate.

[0011] Preferably, the inside of the mounting lower half shell is provided with a stabilizing plate, and the locking stud penetrates through the stabilizing plate and the unmanned aerial vehicle GPS positioning module B.

[0012] Preferably, the blocking piece is in a curved shape, and one end of the blocking piece is tangent to the surface of the circular ring edge.

[0013] Preferably, the limiting piece comprises a circular rod part connected with the fixing plate and a circular ring part sleeved outside the limiting sleeve.

[0014] Preferably, one end of the elastic rod connected with the fixing sleeve is in a curved shape, and the fixing sleeve is provided with a hand-tightening plum blossom screw penetrating through the fixing vertical rod.

[0015] Preferably, the bottom surface of the fixing sleeve is provided with a pressing plate, one end of the pressing plate away from the fixing sleeve is in a curved shape, and the surface of the pressing plate facing the fixing vertical rod is provided with a hemispherical protrusion.

[0016] Preferably, the fixing plate is in a circular ring shape, and the protection net plate is in a curved shape of a circular arc.

[0017] Compared with the prior art, the unmanned aerial vehicle GPS positioning module B mounting cover has the advantages that:

[0018] In the unmanned aerial vehicle GPS positioning module B mounting cover, the mounting design is convenient for dismounting and mounting the unmanned aerial vehicle GPS positioning module B and has protection performance, the mounting lower half shell and the mounting upper half shell for mounting the unmanned aerial vehicle GPS positioning module B are connected in a simple method, the number of screws is reduced, the unmanned aerial vehicle GPS positioning module B is convenient to assemble, the fixing plate and the protection net plate protect the outside of the box body, have protection performance, and the box body is prevented from being collided and damaged. BRIEF DESCRIPTION OF DRAWINGS

[0019] Figure 1 The figure is a structural schematic view of the unmanned aerial vehicle GPS positioning module B mounting cover;

[0020] Figure 2 The figure is a structural schematic view of the unmanned aerial vehicle GPS positioning module B mounting cover;Figure 1 Amplification structure schematic view of middle A part;

[0021] Figure 3 Schematic view of the three-dimensional structure of the fixed plate of the utility model;

[0022] Figure 4 Schematic view of the sectional structure of the utility model for installing the upper half shell;

[0023] Figure 5 Schematic view of the top structure of the utility model for installing the lower half shell;

[0024] Figure 6 Schematic view of the three-dimensional structure of the limiting piece of the utility model;

[0025] In the figure: 5, pressing plate;11, fixed vertical rod;12, mounting plate;21, install lower half shell;22, install upper half shell;31, fixed sleeve;32, elastic rod;33, limiting sleeve;41, fixed plate;42, protective net plate;43, limiting piece;51, hemispherical convex;211, connecting stud;212, stabilizing plate;213, locking stud;221, circular ring edge;321, blocking piece. DETAILED DESCRIPTION

[0026] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, rather than all the embodiments. Based on the embodiments in the utility model, all the other embodiments obtained by those skilled in the art without creative labor fall within the protection scope of the utility model.

[0027] EMBODIMENT

[0028] Please refer to Figures 1 to 6The utility model provides a technical scheme: a kind of installation structure of unmanned plane GPS positioning module, including unmanned plane GPS positioning module B mounting frame, including fixed vertical rod 11, the mounting plate 12 being connected with the top end of fixed vertical rod 11, fixed vertical rod 11 and mounting plate 12 are connected by screwing;Unmanned plane GPS positioning module B mounting cover, including the installation lower half shell 21 being connected with mounting plate 12, the installation upper half shell 22 being connected with installation lower half shell 21 by screwing, the connecting stud 211 being vertically installed lower half shell 21 bottom surface center position, connecting stud 211 is connected by screwing with mounting plate 12, it is convenient to dismount installation lower half shell 21, unmanned plane GPS positioning module B is installed in the inside of installation lower half shell 21 and installation upper half shell 22, so that unmanned plane GPS positioning module B is sealed, protect, the outer surface of this installation upper half shell 22 is equipped with annular edge 221, annular edge 221 is integrally injection molded with installation upper half shell 22, installation lower half shell 21 and installation upper half shell 22 form complete box body, and the box body is combined with mounting plate 12;Limiting component, including the fixed sleeve 31 being sleeved in the outside of fixed vertical rod 11, the elastic rod 32 being symmetrically distributed on fixed sleeve 31, the limiting sleeve 33 being connected with one end of elastic rod 32 by screwing, the blocking piece 321 is equipped on the elastic rod 32, fixed sleeve 31 is firmly held with fixed vertical rod 11 by hand twist plum-blossom screw, and elastic rod 32 plays the role of limiting box body, and elastic rod 32 is made of elastic plastic material, and can be bent, and the blocking piece 321 is made of elastic metal material, when box body is spirally installed, annular edge 221 drives blocking piece 321, when the box body is in accord with mounting plate 12, blocking piece 321 limits annular edge 221, to avoid box body to loosen;Protective piece, including the fixed plate 41 being installed in the outside of installation upper half shell 22, the protective net plate 42 being symmetrically installed on fixed plate 41, the limiting piece 43 being connected with fixed plate 41, limiting piece 43 is fixed with fixed plate 41 by strong glue, limiting sleeve 33 is connected with elastic rod 32 by screwing after penetrating limiting piece 43, so that limiting piece 43 and fixed plate 41 are fixed, and protective net plate 42 is distributed in the periphery of box body, plays the role of protection, avoids that box body is impacted and damaged.

[0029] In the embodiment, the inside of installation lower half shell 21 is equipped with stable plate 212, locking stud 213 penetrating stable plate 212 and unmanned plane GPS positioning module B, locking stud 213 firmly holds unmanned plane GPS positioning module B, so that it is stable in the inside of installation lower half shell 21.

[0030] In the embodiment, the blocking piece 321 is curved shape, the blocking piece 321 one end is tangent with the surface of annular edge 221, and the blocking piece 321 abuts against annular edge 221, to avoid that box body loosens.

[0031] In the embodiment, the limiting piece 43 comprises a round rod part connected with the fixed plate 41 and a round ring part sleeved outside the limiting sleeve 33, the limiting sleeve 33 is threaded through the limiting piece 43 and is connected with the elastic rod 32 through screwing, so that the limiting piece 43 and the fixed plate 41 are fixed.

[0032] In the embodiment, the end of the elastic rod 32 connected with the fixed sleeve 31 is in a curved shape, the fixed sleeve 31 is provided with a hand-tightened plum screw penetrating through the fixed vertical rod 11, and the fixed sleeve 31 is kept stable under the firmness of the hand-tightened plum screw.

[0033] In the embodiment, the bottom surface of the fixed sleeve 31 is provided with the pressing plate 5, the end of the pressing plate 5 away from the fixed sleeve 31 is in a curved shape, the surface of the pressing plate 5 facing the fixed vertical rod 11 is provided with the hemispherical protrusion 51, the fixed plate 41 is in a round ring shape, the protective mesh plate 42 is in a curved shape of a circular arc, the unmanned aerial vehicle GPS positioning module B is connected with the data line a, the data line a can be attached to the fixed vertical rod 11, the data line a is pressed by the pressing plate 5, the data line a passes around the hemispherical protrusion 51, and shaking of the data line a is avoided.

[0034] The working principle and use process of the utility model are as follows:

[0035] When the unmanned aerial vehicle GPS positioning module B is installed, one end of the data line a is connected with a corresponding device inside the unmanned aerial vehicle, and then the bottom end of the fixed vertical rod 11 is firmly connected with the unmanned aerial vehicle shell through a screw;

[0036] Then the unmanned aerial vehicle GPS positioning module B is firmly connected inside the installation lower half shell 21 through the locking stud 213, the installation upper half shell 22 is connected with the installation lower half shell 21 through screwing, and the installation upper half shell 22 and the installation lower half shell 21 form a box body for protecting the unmanned aerial vehicle GPS positioning module B;

[0037] The connecting stud 211 on the installation lower half shell 21 is connected with the installation plate 12 through screwing;

[0038] In the process of connecting the box body with the installation plate 12, the round ring edge 221 on the installation upper half shell 22 drives the blocking piece 321, and when the box body is fitted with the installation plate 12, the elastically reset blocking piece 321 limits the round ring edge 221, so that the box body is prevented from loosening;

[0039] Then the fixed plate 41 and the protective mesh plate 42 are installed outside the box body, the limiting sleeve 33 is threaded through the limiting piece 43 and is connected with the elastic rod 32 through screwing, the fixed plate 41 covers the top of the box body, the protective mesh plate 42 protects the outside of the box body, and the box body is prevented from being impacted and damaged;

[0040] When the different unmanned aerial vehicle GPS positioning module B is replaced, only the elastic rod 32 is opened outward, the box body is rotated and taken out, and the upper half shell 22 is rotated and opened, so that the different unmanned aerial vehicle GPS positioning module B can be disassembled and replaced, the number of screws is reduced, and the unmanned aerial vehicle GPS positioning module B is convenient to assemble.

[0041] In conclusion, in the application, the unmanned aerial vehicle GPS positioning module B is convenient to disassemble and assemble and has the protective mounting design, the lower half shell 21 and the upper half shell 22 for mounting the unmanned aerial vehicle GPS positioning module B are connected in a simple manner, the number of screws is reduced, the unmanned aerial vehicle GPS positioning module B is convenient to assemble, the outer side of the box body is protected by the fixing plate 41 and the protective net plate 42, has the protective property, and the box body is prevented from being collided and damaged.

[0042] Although the embodiments of the utility model have been shown and described (see the above detailed description), it can be understood by those skilled in the art that various changes, modifications, replacements and variations can be made to these embodiments without departing from the principles and spirits of the utility model, and the scope of the utility model is defined by the appended claims and their equivalents.

Claims

1. An installation structure for a GPS positioning module for an unmanned aerial vehicle (UAV), characterized in that: The application relates to an unmanned aerial vehicle GPS positioning module B mounting frame, which comprises a fixed vertical rod (11) and a mounting plate (12) connected to the top end of the fixed vertical rod (11). The application relates to an unmanned aerial vehicle GPS positioning module B mounting cover, which comprises a mounting lower half shell (21) connected to the mounting plate (12), a mounting upper half shell (22) threadedly connected to the mounting lower half shell (21), and a connecting stud (211) vertically arranged at the bottom surface center of the mounting lower half shell (21). The application relates to a limiting assembly, which comprises a fixed sleeve (31) sleeved on the outer side of the fixed vertical rod (11), elastic rods (32) symmetrically arranged on the fixed sleeve (31), and a limiting sleeve (33) threadedly connected to one end of the elastic rod (32). The application relates to a protection piece, which comprises a fixed plate (41) mounted on the outer side of the mounting upper half shell (22), protection net plates (42) symmetrically mounted on the fixed plate (41), and a limiting piece (43) connected to the fixed plate (41). The inside of the mounting lower half shell (21) is provided with a stabilizing plate (212) and a locking stud (213) penetrating through the stabilizing plate (212) and the unmanned aerial vehicle GPS positioning module B. 2.The mounting structure of a GPS positioning module of a UAV according to claim 1, wherein: The blocking piece (321) is in a curved shape, and one end of the blocking piece (321) is tangent to the surface of the circular ring edge (221). 3.The mounting structure of a GPS positioning module of a UAV according to claim 1, wherein: The limiting piece (43) comprises a circular rod part connected to the fixed plate (41) and a circular ring part sleeved on the outer side of the limiting sleeve (33).

4. The mounting structure for a GPS positioning module of a UAV according to claim 1, wherein: One end of the elastic rod (32) connected to the fixed sleeve (31) is in a curved shape, and the fixed sleeve (31) is provided with a hand-tightened plum-blossom screw penetrating through the fixed vertical rod (11).

5. The mounting structure for a GPS positioning module of a UAV according to claim 1, wherein: The bottom surface of the fixed sleeve (31) is provided with a pressing plate (5), one end of the pressing plate (5) away from the fixed sleeve (31) is in a curved shape, and the surface of the pressing plate (5) facing the fixed vertical rod (11) is provided with a hemispherical protrusion (51).

6. The mounting structure for a GPS positioning module of a UAV according to claim 1, wherein: The fixed plate (41) is in a circular ring shape, and the protection net plate (42) is in a curved shape of a circular arc.

7. The mounting structure for a GPS positioning module of a UAV according to claim 1, wherein: ​

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