Fixing structure for unmanned aerial vehicle navigation device

Abstract

The utility model provides a fixing structure for an unmanned aerial vehicle navigation device, which comprises an unmanned aerial vehicle body, Beidou navigation equipment is slidably connected in an upper end groove of the unmanned aerial vehicle body, a connecting plug is fixedly connected in the upper end groove of the unmanned aerial vehicle body, and the lower end of the Beidou navigation equipment is fixedly connected with a connecting socket. By means of the design, the problems that when a Beidou navigation device is fixedly installed on an unmanned aerial vehicle for use through an original device, rain, snow and dust enter a sliding assembly, the sliding assembly is corroded, the service life of the sliding assembly is shortened, and the Beidou navigation device is not prone to being taken down are solved; the Beidou navigation device is reasonable in structure and good in practicability, after the Beidou navigation device is installed on the unmanned aerial vehicle body, the connecting position of the Beidou navigation device and the unmanned aerial vehicle body is in a sealed state, a user can conveniently and rapidly disassemble and assemble the Beidou navigation device, and meanwhile the connecting structure is prevented from being affected by external rain, snow and dust.

Description

TECHNICAL FIELD

[0001] The utility model relates to a fixing structure for unmanned plane navigation device belongs to unmanned plane technical field. BACKGROUND

[0002] Unmanned aircraft is called "drone" for short, is the use of radio remote control equipment and self-provided program control device manipulates the aircraft without people, or by onboard computer completely or intermittently self-operated, in the application of aerial photography, agriculture, plant protection, miniature self -photography, express delivery, disaster rescue, observation wild animal, monitoring infectious disease, surveying and mapping, news report, power patrol, disaster relief, film and television shooting, manufacture romance and the like.

[0003] The utility model discloses a kind of beidou unmanned plane navigation positioning devices, by the setting of T-shaped slot, inner slot, clamping block, fixed block, first sliding slot and first spring, the cooperation of first spring and clamping block can complete the positioning of beidou unmanned plane navigation, it can be disassembled by stirring fixed block in first sliding slot, solve the problem that existing beidou unmanned plane navigation is not easy to disassemble, but this device is fixed and installed in unmanned plane when using after beidou navigation, rain and dust can enter sliding assembly, can cause corrosion to sliding assembly, reduce the service life of sliding assembly, beidou navigation is not easy to take down, there is an urgent need for a fixing structure for unmanned plane navigation device to solve the above problems. UTILITY MODEL CONTENTS

[0004] In view of the deficiencies in the prior art, the utility model aims to provide a fixing structure for unmanned plane navigation device to solve the problems raised in the background art, the utility model has good practicability, after the beidou navigation equipment is installed on the unmanned plane body, the connection between the beidou navigation equipment and the unmanned plane body is in a sealed state, which facilitates the user to quickly disassemble and assemble the beidou navigation equipment while preventing external rain and dust from affecting the connection structure.

[0005] In order to achieve the above-mentioned purpose, the utility model is implemented by the following technical scheme: a fixing structure for unmanned plane navigation device, comprising an unmanned plane body, a beidou navigation device is slidably connected in the upper end slot of the unmanned plane body, a connecting plug is fixedly connected in the upper end slot of the unmanned plane body, a connecting socket is fixedly connected to the lower end of the beidou navigation device, and the connecting socket and the connecting plug are electrically connected.

[0006] The upper end of the Beidou navigation equipment is penetrated and rotationally connected with two rotating dismounting rods, the lower ends of the two rotating dismounting rods are fixedly connected with limiting clamping blocks, the upper end of the unmanned aerial vehicle body is fixedly connected with two butt joint circular clamping seats in the circular groove, rotating clamping grooves are formed in the two butt joint circular clamping seats, and the two butt joint circular clamping seats are fixedly connected with two magnetic attraction blocks.

[0007] Further, the circumferential surface of the Beidou navigation equipment is fixedly connected with a sealing baffle ring made of rubber material.

[0008] Further, the inner wall of the upper end of the unmanned aerial vehicle body is fixedly connected with two positioning mounting blocks, and the two positioning mounting blocks are matched with the Beidou navigation equipment.

[0009] Further, the upper end of the Beidou navigation equipment is provided with a taking pinch groove.

[0010] Further, the two limiting clamping blocks are matched with the two groups of magnetic attraction blocks.

[0011] Further, the surface of the Beidou navigation equipment is provided with an anti-corrosion layer.

[0012] The fixing structure for the unmanned aerial vehicle navigation device has the advantages that the fixing structure for the unmanned aerial vehicle navigation device is reasonable in structure and good in practicability, the Beidou navigation equipment is installed on the unmanned aerial vehicle body, the connection between the Beidou navigation equipment and the unmanned aerial vehicle body is in a sealed state, the Beidou navigation equipment can be quickly dismounted, and the influence of external rain, snow and dust on the connection structure is prevented. BRIEF DESCRIPTION OF DRAWINGS

[0013] Other features, objects and advantages of the present application will become more apparent from the following detailed description of non-limiting embodiments with reference to the attached drawings:

[0014] Figure 1 It is a whole structure perspective schematic view of the fixing structure for the unmanned aerial vehicle navigation device of the present application;

[0015] Figure 2 It is a local section structure schematic view of the fixing structure for the unmanned aerial vehicle navigation device of the present application;

[0016] Figure 3 It is a fixing structure for the unmanned aerial vehicle navigation device of the present application Figure 2 Structure schematic view at A in the fixing structure for the unmanned aerial vehicle navigation device of the present application;

[0017] Figure 4 For the utility model discloses a kind of fixed structures for unmanned aerial vehicle navigation device, the structure diagram of docking round clamping seat in it;

[0018] Figure 5 For the utility model discloses a kind of fixed structures for unmanned aerial vehicle navigation device, the structure diagram of rotating dismounting rod in it;

[0019] Figure 6 For the utility model discloses a kind of fixed structures for unmanned aerial vehicle navigation device, the structure diagram of the section of docking round clamping seat in it.

[0020] In the drawing: 1-unmanned aerial vehicle body, 2-Beidou navigation equipment, 3-rotating dismounting rod, 4-take pinch groove, 5-limiting block, 6-docking round clamping seat, 7-rotary clamping slot, 8-positioning mounting block, 9-sealing baffle ring, 10-connection socket, 11-magnetic block, 12-connection plug. DETAILED DESCRIPTION

[0021] To make the technical means, creative features, achieve purposes and effects of the utility model easy to understand, the utility model is further described below in combination with specific embodiments.

[0022] Please refer to Figures 1-6 The utility model provides a kind of technical scheme: a kind of fixed structure for unmanned aerial vehicle navigation device, including unmanned aerial vehicle body 1, the upper end groove of unmanned aerial vehicle body 1 is slidably connected with Beidou navigation equipment 2, the upper end groove of unmanned aerial vehicle body 1 is fixedly connected with connection plug 12, the lower end of Beidou navigation equipment 2 is fixedly connected with connection socket 10, connection socket 10 is electrically connected with connection plug 12, the upper end of Beidou navigation equipment 2 is penetrated and rotationally connected with two rotating dismounting rods 3, the lower end of two rotating dismounting rods 3 is fixedly connected with limiting block 5, the upper end circular groove of unmanned aerial vehicle body 1 is fixedly connected with two docking round clamping seats 6, rotary clamping slot 7 is set in two docking round clamping seats 6, two magnetic blocks 11 are fixedly connected in two docking round clamping seats 6, two limiting blocks 5 are rotationally connected in two rotary clamping slots 7 respectively, this design solves the problem that original device is used when being fixedly installed in unmanned aerial vehicle, rain and dust will enter into sliding assembly, will cause corrosion to sliding assembly, reduce the service life of sliding assembly, not easy to take down Beidou navigation.

[0023] As a first embodiment of the utility model: the circumferential surface of big dipper navigation equipment 2 is fixedly connected with sealing baffle ring 9, sealing baffle ring 9 is made of rubber material, sealing baffle ring 9 installed on the surface of big dipper navigation equipment 2 can increase the sealing property between big dipper navigation equipment 2 and the unmanned aerial vehicle body 1 connection, prevent the outside rain and snow from entering big dipper navigation equipment 2 through the connecting gap, sealing baffle ring 9 is made of rubber, and the elastic ability effectively blocks the connecting place of the circular groove of unmanned aerial vehicle body 1 and big dipper navigation equipment 2. The inner wall of the upper end of unmanned aerial vehicle body 1 is fixedly connected with two positioning mounting blocks 8, two positioning mounting blocks 8 are matched with big dipper navigation equipment 2, the positioning mounting block 8 installed in unmanned aerial vehicle body 1 can assist the mutual connection of connecting plug 12 and connecting socket 10, and big dipper navigation equipment 2 is provided with power supply and data connection by connecting plug 12. The upper end of big dipper navigation equipment 2 is provided with taking pinch groove 4, and the taking pinch groove 4 arranged on big dipper navigation equipment 2 facilitates the user to take down or install big dipper navigation equipment 2. Two limiting clamping blocks 5 and two groups of magnetic attraction blocks 11 are matched with each other, when limiting clamping block 5 rotates in rotating clamping groove 7, magnetic attraction block 11 and limiting clamping block 5 are mutually adsorbed and connected, so that unmanned aerial vehicle body 1 and big dipper navigation equipment 2 are fixedly connected, and the gap between unmanned aerial vehicle body 1 and big dipper navigation equipment 2 is eliminated. The surface of big dipper navigation equipment 2 is provided with an anticorrosion layer, which can reduce the corrosion of external rain and snow on big dipper navigation equipment 2 and increase the service life of big dipper navigation equipment 2.

[0024] As a second embodiment of the utility model: first, the circular groove at the bottom of big dipper navigation equipment 2 is aligned with positioning mounting block 8, then big dipper navigation equipment 2 is placed in the circular groove of unmanned aerial vehicle body 1, rotating dismounting rod 3 is rotated to drive limiting clamping block 5 to rotate in rotating clamping groove 7, so that magnetic attraction block 11 and limiting clamping block 5 are mutually adsorbed and connected, when unmanned aerial vehicle body 1 is running, power supply and data are provided to big dipper navigation equipment 2 through connecting plug 12, when big dipper navigation equipment 2 needs to be taken down, rotating dismounting rod 3 is pinched to drive limiting clamping block 5 to rotate to release the butt joint circular clamping seat 6, then big dipper navigation equipment 2 is taken down by pinching taking pinch groove 4, when big dipper navigation equipment 2 is not used, the cover needs to cover the circular groove in the upper end of unmanned aerial vehicle body 1 to prevent rain and snow and dust from entering connecting plug 12.

[0025] The basic principle and main features of the present application and the advantages of the present application are shown and described above. For those skilled in the art, it is obvious that the present application is not limited to the details of the above exemplary embodiments, and the present application can be implemented in other specific forms without departing from the spirit or basic characteristics of the present application. Therefore, from any point of view, the embodiments should be regarded as exemplary and non-limiting, and the scope of the present application is defined by the appended claims rather than the above description, and therefore all changes falling within the meaning and scope of the equivalent elements of the claims are intended to be included in the present application. Any reference signs in the claims should not be considered as limiting the claims involved.

[0026] In addition, it should be understood that, although the present application is described in terms of embodiments, not every embodiment contains only one independent technical solution, and the description of the specification is only for the sake of clarity, and those skilled in the art should consider the specification as a whole, and the technical solutions in each embodiment can be properly combined to form other embodiments that those skilled in the art can understand.

Claims

1. A fixing structure for a drone navigation device, comprising a drone body (1), characterized in that: The Beidou navigation device (2) is slidably connected in the upper end groove of the unmanned aerial vehicle body (1), the connecting plug (12) is fixedly connected in the upper end groove of the unmanned aerial vehicle body (1), the lower end of the Beidou navigation device (2) is fixedly connected with the connecting socket (10), and the connecting socket (10) is electrically connected with the connecting plug (12); The upper end of the Beidou navigation device (2) penetrates and is rotatably connected with two rotating dismounting rods (3), the lower ends of the two rotating dismounting rods (3) are fixedly connected with limiting clamping blocks (5), the upper end circular groove of the unmanned aerial vehicle body (1) is fixedly connected with two butt joint circular clamping seats (6), rotating clamping grooves (7) are formed in the two butt joint circular clamping seats (6), and the two butt joint circular clamping seats (6) are fixedly connected with two magnetic attraction blocks (11); the two limiting clamping blocks (5) are rotatably connected in the two rotating clamping grooves (7) respectively.

2. The fixing structure for the UAV navigation device according to claim 1, wherein: The circumferential surface of the Beidou navigation device (2) is fixedly connected with a sealing baffle ring (9), and the sealing baffle ring (9) is made of rubber material.

3. The fixing structure for the UAV navigation device according to claim 1, wherein: The upper end inner wall of the unmanned aerial vehicle body (1) is fixedly connected with two positioning mounting blocks (8), and the two positioning mounting blocks (8) are matched with the Beidou navigation device (2).

4. The fixing structure for the UAV navigation device according to claim 1, wherein: The upper end of the Beidou navigation device (2) is provided with a taking pinch groove (4).

5. The fixing structure for the UAV navigation device according to claim 1, wherein: The two limiting clamping blocks (5) and the two groups of magnetic attraction blocks (11) are matched with each other.

6. The fixing structure for the UAV navigation device according to claim 1, wherein: The surface of the Beidou navigation device (2) is provided with an anti-corrosion layer.

Images