CN216943580U

CN216943580U - Unmanned aerial vehicle device with ground satellite station function

Info

Publication number: CN216943580U
Application number: CN202220594085.0U
Authority: CN
Inventors: 李长有
Original assignee: China Science Star Control Tianjin Information Technology Co ltd
Current assignee: China Science Star Control Tianjin Information Technology Co ltd
Priority date: 2022-03-17
Filing date: 2022-03-17
Publication date: 2022-07-12
Anticipated expiration: 2032-03-17

Abstract

The utility model discloses an unmanned aerial vehicle device with a ground station function, which relates to the technical field of unmanned aerial vehicles and comprises an unmanned aerial vehicle main body, a ground station device connected with the unmanned aerial vehicle main body through an installation mechanism, and a sealing ring connected with the unmanned aerial vehicle main body through a locking mechanism; installation mechanism is including seting up the mounting groove at unmanned aerial vehicle main part top, fixed connection at the mount pad of ground station device bottom, seting up the mounting hole at the mount pad top and with mounting hole threaded connection's fixing bolt, solid locking mechanism including inlay in the electro-magnet at unmanned aerial vehicle main part top, set up at the spring groove of mounting groove inside wall, fixed connection is at the coupling spring of spring groove tank bottom, fixed connection is at the solid locking piece of the coupling spring other end. The utility model relates to an unmanned aerial vehicle device with a ground station function, which can prevent a fixing bolt from contacting with moisture in the air by fixing a sealing ring and prolong the service life of the fixing bolt.

Description

Unmanned aerial vehicle device with ground satellite station function

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle device with a ground station function.

Background

The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine is not provided with a cockpit, but is provided with an autopilot, a program control device and other equipment. Personnel at a ground, naval vessel or mother aircraft remote control station track, position, remote control, remote measurement and digital transmission through equipment such as radar, and the ground station is a component of a satellite or a space system. Namely ground equipment which is arranged on the earth and used for space communication. Generally refers to ground based equipment located on the surface of the earth, including those aboard ships and aircraft, for satellite communication.

Ground station is generally through fixing its surface at unmanned aerial vehicle with the bolt on the existing market, and its unmanned aerial vehicle often can produce the strong wind and blow the surface of ground station device when high altitude flight, and after long-time use, not hard up condition can appear in its bolt, and under high altitude environment, its steam destroys the bolt easily.

SUMMERY OF THE UTILITY MODEL

The utility model mainly aims to provide an unmanned aerial vehicle device with a ground station function, which can effectively solve the problems that bolts can be loosened after long-time use in the background technology and water vapor is easy to damage the bolts in a high-altitude environment.

In order to achieve the purpose, the utility model adopts the technical scheme that: an unmanned aerial vehicle device with a ground station function comprises an unmanned aerial vehicle main body, a ground station device and a sealing ring, wherein the ground station device is connected with the unmanned aerial vehicle main body through a mounting mechanism, and the sealing ring is connected with the unmanned aerial vehicle main body through a locking mechanism;

the mounting mechanism comprises a mounting groove formed in the top of the unmanned aerial vehicle main body, a mounting seat fixedly connected to the bottom of the ground station device, a mounting hole formed in the top of the mounting seat, and a fixing bolt in threaded connection with the mounting hole;

the solid locking mechanism comprises an electromagnet inlaid at the top of the unmanned aerial vehicle main body, a spring groove formed in the inner side wall of the mounting groove, a connecting spring fixedly connected to the bottom of the spring groove, a solid locking block fixedly connected to the other end of the connecting spring and a solid locking groove formed in the outer side wall of the sealing ring, wherein the outer diameter of the solid locking block is equal to the inner diameter of the solid locking groove.

Preferably, the outer diameter of the mounting seat is equal to the inner diameter of the mounting groove, and six groups of mounting holes are arranged and distributed at equal intervals in a ring shape.

Preferably, the number of the fixing bolts is six, and the fixing bolts are hexagon socket head cap bolts.

Preferably, the bottom fixedly connected with of mount pad is six groups, is the plug-in block of annular equidistant distribution, the cross section of plug-in block and the cross section phase-match of fixing bolt nut.

Preferably, the mounting groove is provided with a positioning groove in the inner side wall, the mounting seat is fixedly connected with a positioning block in the outer side wall, and the inner diameter of the positioning groove is equal to the outer diameter of the positioning block.

Preferably, the limiting groove is formed in the inner side wall of the spring groove, the outer side wall of the locking block is fixedly connected with a limiting block, the limiting block is of an annular structure, and the cross section of the limiting block is matched with that of the limiting groove.

Preferably, the locking block is a permanent magnet and mutually attracts adjacent positions of the electromagnet, and the connecting spring is a compression spring.

Compared with the prior art, the utility model has the following beneficial effects:

according to the utility model, the mounting seat is inserted into the mounting groove, then the mounting seat and the mounting groove are fixed through the fixing bolt, then the positioning block fixedly connected to the outer side wall of the sealing ring is aligned to the positioning groove formed in the inner side wall of the mounting groove, the sealing ring is inserted into the mounting groove, at the moment, the insertion block fixedly connected to the bottom of the sealing ring is inserted into the nut of the fixing bolt, so that the fixing bolt is prevented from loosening, then the electromagnet is closed, at the moment, a part of the insertion block slides out of the spring groove under the elastic force action of the connecting spring and is inserted into the inner part of the locking groove, so that the sealing ring is fixed, further, the fixing bolt is prevented from contacting with moisture in the air, and the service life of the fixing bolt is prolonged.

Drawings

FIG. 1 is a schematic view of an overall structure of an unmanned aerial vehicle device with a ground station function according to the present invention;

FIG. 2 is a schematic diagram of a disassembled structure of an unmanned aerial vehicle device with a ground station function according to the present invention;

FIG. 3 is a schematic view of a bottom structure of a sealing ring of an unmanned aerial vehicle device with a ground station function according to the present invention;

FIG. 4 is an internal schematic view of a mounting structure of a sealing ring of an unmanned aerial vehicle device and a main body of an unmanned aerial vehicle, which has a ground station function, according to the present invention;

fig. 5 is an enlarged view of a structure a of fig. 4 of an unmanned aerial vehicle apparatus having a ground station function according to the present invention.

In the figure: 1. an unmanned aerial vehicle main body; 2. a ground station device; 3. a seal ring; 4. mounting grooves; 5. a mounting seat; 6. mounting holes; 7. fixing the bolt; 8. an insertion block; 9. positioning a groove; 10. positioning blocks; 11. an electromagnet; 12. a spring slot; 13. a connecting spring; 14. fixing a locking block; 15. fixing the locking groove; 16. a limiting groove; 17. and a limiting block.

Detailed Description

In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the utility model easy to understand, the utility model is further described with the specific embodiments.

In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, such as "connected," which may be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in a specific case to those of ordinary skill in the art.

Referring to fig. 1 to 5, the present invention is an unmanned aerial vehicle device with a ground station function, including an unmanned aerial vehicle main body 1, a ground station device 2 connected to the unmanned aerial vehicle main body 1 through an installation mechanism, and a sealing ring 3 connected to the unmanned aerial vehicle main body 1 through a locking mechanism;

the mounting mechanism comprises a mounting groove 4 arranged at the top of the unmanned aerial vehicle main body 1, a mounting seat 5 fixedly connected to the bottom of the ground station device 2, a mounting hole 6 arranged at the top of the mounting seat 5, and a fixing bolt 7 in threaded connection with the mounting hole 6;

the solid locking mechanism comprises an electromagnet 11 embedded at the top of the unmanned aerial vehicle main body 1, a spring groove 12 formed in the inner side wall of the mounting groove 4, a connecting spring 13 fixedly connected to the bottom of the spring groove 12, a solid locking block 14 fixedly connected to the other end of the connecting spring 13, and a solid locking groove 15 formed in the outer side wall of the sealing ring 3, wherein the outer diameter of the solid locking block 14 is equal to the inner diameter of the solid locking groove 15.

The external diameter size of mount pad 5 equals with the internal diameter size of mounting groove 4, and the quantity of mounting hole 6 has six groups, and is the equidistant distribution of annular, improves the multiunit mounting hole 6 that sets up to make fixing bolt 7 run through mounting hole 6, improve the stability between mount pad 5 and the mounting groove 4 with this.

The number of the fixing bolts 7 is six, and the fixing bolts 7 are inner hexagon bolts which are convenient to detach.

Six groups of bottom fixedly connected with of mount pad 5 are the equidistant distribution's of annular plug block 8, and the cross section of plug block 8 and the cross section phase-match of fixing bolt 7 nut are pegged graft through plug block 8 inside fixing bolt 7's the nut to this fixes fixing bolt 7, prevents that it from becoming flexible.

Constant head tank 9 has been seted up to the inside wall of mounting groove 4, and the lateral wall fixedly connected with locating piece 10 of mount pad 5, and the internal diameter size of constant head tank 9 equals with the external diameter size of locating piece 10, through the cooperation of constant head tank 9 with locating piece 10, guarantees to plug in the piece 8 and can plug in the nut of fixing bolt 7, and can guarantee that the opening of spring groove 12 is just to solid locked groove 15.

Spacing groove 16 has been seted up to the inside wall of spring groove 12, and the lateral wall fixedly connected with stopper 17 of solid locking piece 14, stopper 17 are the annular structure, and stopper 17's cross section and spacing groove 16's cross section phase-match, through the cooperation of spacing groove 16 with stopper 17 for solid locking piece 14 removes more steadily, and can prevent that solid locking piece 14 from breaking away from spring groove 12.

The fixing and locking block 14 is a permanent magnet and is mutually attracted with the adjacent position of the electromagnet 11, the connecting spring 13 is a compression spring, when the electromagnet 11 is closed, the connecting spring 13 is restored to an initial state, and then a part of the fixing and locking block 14 is inserted into the fixing and locking groove 15, so that the sealing ring 3 is fixed.

The working principle of the utility model is as follows: through pegging graft the mount pad 5 in mounting groove 4, then run through mounting hole 6 through fixing bolt 7, come to mount pad 5 and mounting groove 4 fixed mutually, later with the positioning block 10 alignment of fixed connection at the sealing ring 3 lateral wall set up the constant head tank 9 in mounting groove 4 inside wall, and peg graft sealing ring 3 in mounting groove 4, fixed connection is in the nut of fixing bolt 7 will be pegged graft in the plug-in block 8 of sealing ring 3 bottom this moment, prevent fixing bolt 7 not hard up with this, later close electro-magnet 11, at this moment, the solid locking block 14 will be under coupling spring 13's spring action, partly roll-off spring groove 12, and the plug-in is to the inside of solid locking groove 15, with this to come to seal ring 3 fixedly, and then prevent the moisture contact in fixing bolt 7 and the air, improve fixing bolt 7's life.

The foregoing shows and describes the general principles and broad features of the present invention and advantages thereof. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the utility model as claimed. The scope of the utility model is defined by the appended claims and equivalents thereof.

Claims

1. An unmanned aerial vehicle device with ground station function which characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle main body (1), a ground station device (2) connected with the unmanned aerial vehicle main body (1) through an installation mechanism, and a sealing ring (3) connected with the unmanned aerial vehicle main body (1) through a locking mechanism;

the mounting mechanism comprises a mounting groove (4) formed in the top of the unmanned aerial vehicle main body (1), a mounting seat (5) fixedly connected to the bottom of the ground station device (2), a mounting hole (6) formed in the top of the mounting seat (5), and a fixing bolt (7) in threaded connection with the mounting hole (6);

solid locking mechanism is including inlaying in electro-magnet (11) at unmanned aerial vehicle main part (1) top, seting up spring groove (12) at mounting groove (4) inside wall, fixed connection at connecting spring (13) of spring groove (12) tank bottom, fixed connection at solid locking piece (14) of connecting spring (13) the other end and seting up at solid locked groove (15) of sealing ring (3) lateral wall, the external diameter size of solid locking piece (14) equals with the internal diameter size of solid locked groove (15).

2. The unmanned aerial vehicle device with ground station function of claim 1, wherein: the outer diameter of mount pad (5) is equal with the inner diameter of mounting groove (4), the quantity of mounting hole (6) has six groups, and is the annular equidistant distribution.

3. The unmanned aerial vehicle apparatus having a ground station function of claim 2, wherein: six groups of fixing bolts (7) are arranged, and the fixing bolts (7) are inner hexagon bolts.

4. The unmanned aerial vehicle device with ground station function of claim 3, wherein: the bottom fixedly connected with of mount pad (5) is six groups, is the plug-in block (8) of annular equidistant distribution, the cross section of plug-in block (8) and the cross section phase-match of fixing bolt (7) nut.

5. The unmanned aerial vehicle device with ground station function of claim 4, wherein: constant head tank (9) have been seted up to the inside wall of mounting groove (4), the lateral wall fixedly connected with locating piece (10) of mount pad (5), the internal diameter size of constant head tank (9) equals with the external diameter size of locating piece (10).

6. The unmanned aerial vehicle device with ground station function of claim 5, wherein: spacing groove (16) have been seted up to the inside wall of spring groove (12), lateral wall fixedly connected with stopper (17) of solid locking piece (14), stopper (17) are the loop configuration, and the cross section of stopper (17) and the cross section phase-match of spacing groove (16).

7. The unmanned aerial vehicle device with ground station function of claim 6, wherein: the fixed locking block (14) is a permanent magnet and mutually attracts the adjacent position of the electromagnet (11), and the connecting spring (13) is a compression spring.