CN216916318U

CN216916318U - A adhesion magnetite for unmanned aerial vehicle cloud platform

Info

Publication number: CN216916318U
Application number: CN202122373744.6U
Authority: CN
Inventors: 伏旭龙; 邬冰冰
Original assignee: Ningbo Saipai Technology Co ltd
Current assignee: Ningbo Saipai Technology Co ltd
Priority date: 2021-09-29
Filing date: 2021-09-29
Publication date: 2022-07-08
Anticipated expiration: 2031-09-29

Abstract

The utility model provides an adhesion magnet for an unmanned aerial vehicle holder, which comprises: the magnet is arranged on a fixing piece far away from one end of the magnet, two groups of adhesive storage sleeves are arranged on the inner wall of the magnet in a mirror image mode, and oblique openings of the two groups of adhesive storage sleeves are formed, wherein the two groups of adhesive storage sleeves are provided with oblique openings; the magnetite laminating behind the mounting, the mounting can extrude two sets ofly the cover is stored to the adhesion agent to make emollient follow the slant opening flows, and is concrete, lets the adhesion agent store the cover pressurized adhesion agent through the work of magnetite laminating mounting, and the adhesion agent is attached to between magnetite and mounting, has guaranteed swift adhesion effect between magnetite and the mounting, has improved the fixed efficiency of magnetite of unmanned aerial vehicle cloud platform.

Description

A adhesion magnetite for unmanned aerial vehicle cloud platform

Technical Field

The utility model relates to the technical field of magnets, in particular to an adhesion magnet for an unmanned aerial vehicle holder.

Background

The unmanned aerial vehicle cloud platform is that unmanned aerial vehicle is used for the supporting equipment of task load such as installation, fixed camera, because the difference of unmanned aerial vehicle function and usage, various different sensors or camera can be carried on at the unmanned aerial vehicle cloud platform.

The unmanned aerial vehicle cloud platform is gone up and needs to utilize the magnetite to adsorb the location to carrying on equipment sometimes, and the connected mode of magnetite has that the adhesion is fixed and the bolt fastening, and the adhesion mode of current magnetite is convenient inadequately, lets the fixed efficiency of magnetite of unmanned aerial vehicle cloud platform can not obtain the improvement.

SUMMERY OF THE UTILITY MODEL

The technical problem to be solved by the utility model is as follows: in order to solve the problems in the prior art. The utility model provides an adhesion magnet for an unmanned aerial vehicle holder to solve the problems.

The technical scheme adopted by the utility model for solving the technical problems is as follows: an adhesion magnetite for unmanned aerial vehicle cloud platform, includes: the magnet is arranged on a fixing piece far away from one end of the magnet, two groups of adhesive storage sleeves are arranged on the inner wall of the magnet in a mirror image mode, and oblique openings of the two groups of adhesive storage sleeves are formed, wherein the two groups of adhesive storage sleeves are provided with oblique openings; the magnetite laminating behind the mounting, the mounting can extrude two sets ofly the adhesion agent stores the cover to make emollient follow the slant opening flows out.

Furthermore, the outer wall of the fixing piece is provided with a connecting rod; the inner wall of the magnet is provided with a rectangular notch, wherein the rectangular notch is arranged in the magnet; the magnetite laminating behind the mounting, the connecting rod can alternate the rectangle breach.

Furthermore, the inner wall mirror image of the adhesion agent storage sleeve is provided with a plurality of triangular grooves.

Further, the adhesion magnet for the unmanned aerial vehicle holder further comprises a sealing part; the sealing part comprises an oblique movable rod inserted in the oblique opening and a sealing cover arranged at the lower end of the oblique movable rod, wherein the sealing cover is provided with a sealing hole; the magnetite laminating behind the mounting, the mounting can extrude two sets ofly the cover is stored to the adhesion agent, so that the slant movable rod pressurized drives the closing cap descends.

Furthermore, the sealing part also comprises an oblique sliding chute connected with the oblique opening, a sliding block arranged in the oblique sliding chute and a first spring connected between the sliding block and the oblique sliding chute, wherein the sliding block is connected to one side of the oblique movable rod; after the oblique movable rod is pressed to drive the sealing cover to descend, the movable rod can drive the sliding block to slide along the sliding groove, so that the first spring is compressed.

Further, the slider is hemispherical.

Further, the adhesion magnet for the unmanned aerial vehicle holder further comprises an elastic part; the elastic part comprises a plurality of fixing rods arranged on the inner sides of the two groups of the adhesive storage sleeves in a mirror image manner, a plurality of second springs arranged between the inner sides of the two groups of the adhesive storage sleeves and the plurality of fixing rods in a mirror image manner, and the two adjacent groups of the fixing rods are hinged and fixed; the magnetite laminating behind the mounting, the mounting can extrude two sets ofly the cover is stored to the adhesion agent, so that it is a plurality of the dead lever is rotatory to drive a plurality of second spring compression.

The utility model has the beneficial effects that: work through magnetite laminating mounting lets the adhesion agent store the cover pressurized adhesion agent, and the adhesion agent is attached to between magnetite and mounting, has guaranteed swift adhesion effect between magnetite and the mounting, has improved the fixed efficiency of magnetite of unmanned aerial vehicle cloud platform.

Drawings

The utility model is further illustrated by the following examples in conjunction with the drawings.

FIG. 1 is a schematic structural view of an adhesion magnet for an unmanned aerial vehicle cradle head according to the present invention;

FIG. 2 is a schematic view of a magnet attachment fixture according to the present invention;

FIG. 3 is a schematic cross-sectional side view of an adhesive storage sleeve of the present invention;

fig. 4 is an enlarged view of the utility model at a in fig. 3.

In the drawings

1. A magnet;

2. a fixing member;

3. an adhesive storage sleeve;

4. an oblique opening;

5. a connecting rod;

6. a rectangular notch;

7. a triangular groove;

8. a closing part; 81. an oblique movable rod; 82. sealing the cover; 83. a slider; 84. an oblique chute; 85. a first spring;

9. an elastic part; 91. fixing the rod; 92. a second spring.

Detailed Description

Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are illustrative only for the purpose of explaining the present invention, and are not to be construed as limiting the present invention. On the contrary, the embodiments of the utility model include all changes, modifications and equivalents coming within the spirit and terms of the claims appended hereto.

In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "axial", "radial", "circumferential", and the like, indicate orientations and positional relationships based on the orientations and positional relationships shown in the drawings, and are used merely for convenience of description and for simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be considered as limiting the present invention.

Furthermore, the terms "first," "second," and the like 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 "connected" and "connected" are to be interpreted broadly, e.g., as being fixed or detachable or integrally connected; can be mechanically or electrically connected; may be directly connected or indirectly connected through an intermediate. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art. In addition, in the description of the present invention, "a plurality" means two or more unless otherwise specified.

Referring to fig. 1, fig. 1 is a schematic structural view of an adhesion magnet for an unmanned aerial vehicle cradle head according to the present invention; referring to FIG. 2, FIG. 2 is a schematic view of a magnet connecting and fixing member according to the present invention; referring to fig. 3, fig. 3 is a schematic cross-sectional side view of an adhesive storage case according to the present invention; referring to FIG. 4, FIG. 4 is an enlarged view taken at A of FIG. 3 according to the present invention; as shown in fig. 1-4, the present invention provides an adhesion magnet for an unmanned aerial vehicle pan-tilt, comprising: the magnetic module comprises a magnet 1, a fixing piece 2 arranged at one end far away from the magnet 1, two groups of adhesive storage sleeves 3 arranged on the inner wall of the magnet 1 in a mirror image manner, and oblique openings 4 arranged in the two groups of adhesive storage sleeves 3, wherein the two groups of adhesive storage sleeves 3 are provided with a plurality of oblique openings; 1 laminating of magnetite behind mounting 2, mounting 2 can extrude two sets ofly the adhesion agent stores cover 3, so that emollient is followed 4 flows out of slant opening, and is concrete, lets the adhesion agent store cover 3 pressurized adhesion agents through 1 work of the mounting 2 of laminating of magnetite, and the adhesion agent is attached to between magnetite 1 and mounting 2, has guaranteed swift adhesion effect between magnetite 1 and the mounting 2, has improved the 1 fixed efficiency of magnetite of unmanned aerial vehicle cloud platform.

Optionally, a connecting rod 5 is arranged on the outer wall of the fixing piece 2; the inner wall of the magnet 1 is provided with a rectangular notch 6, wherein; magnet 1 laminating behind mounting 2, connecting rod 5 can alternate rectangle breach 6, it is concrete, connecting rod 5 inserts rectangle breach 6 along with the movable operation of mounting 2 is slided to insert formula, provides good location effect for the combination work of mounting 2 and magnet 1, has improved the accurate effect of combination between it, has avoided the combined position between it to take place the displacement.

Optionally, 3 inner wall mirror images of cover are stored to the adhesion agent are provided with a plurality of triangular grooves 7, and is concrete, and 3 atress compression drive a plurality of triangular grooves 7 compression are stored to the adhesion agent, and the adjacent inclined plane of a plurality of triangular grooves 7 is laminated gradually, lets the compression process that the cover 3 was stored to the adhesion agent take place deformation according to fixed orbit, guarantees the stability of compression process.

Optionally, the adhesion magnet for the unmanned aerial vehicle holder further comprises a sealing part 8; the closing part 8 comprises an oblique movable rod 81 inserted into the oblique opening 4 and a sealing cover 82 arranged at the lower end of the oblique movable rod 81; 1 laminating of magnetite mounting 2 afterwards, mounting 2 can extrude two sets ofly the adhesion agent stores cover 3, so that slant movable rod 81 pressurized drives cover 82 descends, and is specific, and cover 82 plays the jam effect to slant opening 4, avoids the adhesion agent to store the adhesion agent in cover 3 and flows out at the unstressed state, treats that the adhesion agent stores when cover 3 pressurized, and slant movable rod 81 drives cover 82 along slant opening 4's orbit and descends, and cover 82 descends and the separation of cover 3 is stored to the adhesion agent, and at this moment, slant opening 4's jam effort disappears, and the adhesion agent in the adhesion agent storage cover 3 can be smooth and easy flows out from slant opening 4.

Optionally, the closing portion 8 further includes an oblique sliding slot 84 connected to the oblique opening 4, a sliding block 83 disposed in the oblique sliding slot 84, and a first spring 85 connected between the sliding block 83 and the oblique sliding slot 84, where the sliding block 83 is connected to one side of the oblique movable rod 81; the slant movable rod 81 is pressed and is driven the closing cap 82 descends the back, the movable rod can drive the slider 83 is followed slant spout 84 slides, so that first spring 85 compresses, and is concrete, and slant movable rod 81 descends along slant opening 4 and drives slider 83 and slide along slant spout 84, lets slider 83's movable track be by smooth and easy spacing, and slider 83 activity is stretched first spring 85, thereby first spring 85 can play the positioning action to slider 83's position and let closing cap 82's position obtain the location effect, and closing cap 82 atress descends and resets under first spring 85's elastic reaction force and closes slant opening 4 again, makes closing cap 82's activity work more high-efficient nimble.

Optionally, the slider 83 is a hemisphere, and specifically, the shape of the slider 83 is set to reduce the movement resistance.

Optionally, the adhesion magnet for the unmanned aerial vehicle holder further comprises an elastic part 9; the elastic part 9 comprises a plurality of fixing rods 91 arranged at the inner sides of the two groups of the adhesive storage sleeves 3 in a mirror image manner, a plurality of second springs 92 arranged between the inner sides of the two groups of the adhesive storage sleeves 3 and the plurality of fixing rods 91 in a mirror image manner, and two adjacent groups of the fixing rods 91 are hinged and fixed; 1 laminating of magnetite the mounting 2 afterwards, mounting 2 can extrude two sets ofly the cover 3 is stored to the adhesion agent, so that it is a plurality of the rotatory a plurality of second springs 92 of drive of dead lever 91 compress, it is concrete, the adhesion agent is stored the cover 3 pressurized and is driven a plurality of two adjacent dead lever 91 opposite rotation, its rotation process slows down the compression effort that the adhesion agent stored cover 3, and simultaneously, the slope of a plurality of second springs 92 mirror image sets up, two adjacent dead lever 91 opposite rotation make a plurality of second springs 92 flexible, a plurality of second springs 92 are flexible to let a plurality of two adjacent dead lever 91 opposite rotation processes more gentle, avoid the adhesion agent to store the state dislocation after cover 3 deformation, the atress effect that makes the adhesion agent store 3 each positions is even, let the atress distribution of adhesion agent balanced, the bonding face between 1 and the mounting 2 has been increased.

In the description herein, references to the description of the term "one embodiment," "some embodiments," "an example," "a specific example," or "some examples," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the utility model. In this specification, a schematic representation of the term does not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.

In light of the foregoing description of the preferred embodiment of the present invention, many modifications and variations can be made by the worker in the light of the above teachings without departing from the spirit of the utility model. The technical scope of the present invention is not limited to the content of the specification, and must be determined according to the scope of the claims.

Claims

1. The utility model provides an adhesion magnetite for unmanned aerial vehicle cloud platform which characterized in that includes: the adhesive storage device comprises a magnet (1), a fixing piece (2) arranged at one end far away from the magnet (1), two groups of adhesive storage sleeves (3) arranged on the inner wall of the magnet (1) in a mirror image mode, and oblique openings (4) arranged in the two groups of adhesive storage sleeves (3), wherein the two groups of adhesive storage sleeves are provided with a plurality of holes;

magnet (1) laminating behind mounting (2), mounting (2) can extrude two sets ofly cover (3) are stored to adhesion agent to make emollient follow slant opening (4) flow.

2. The adhesion magnetite used for unmanned aerial vehicle cloud platform of claim 1,

the outer wall of the fixing piece (2) is provided with a connecting rod (5);

a rectangular notch (6) is formed in the inner wall of the magnet (1);

magnetite (1) laminating behind mounting (2), connecting rod (5) can alternate rectangle breach (6).

3. The adhesive magnet for the PTZ of the unmanned aerial vehicle as claimed in claim 2,

the inner wall of the adhesive storage sleeve (3) is provided with a plurality of triangular grooves (7) in a mirror image manner.

4. The adhesive magnet for the PTZ of the unmanned aerial vehicle as claimed in claim 3,

the adhesion magnet for the unmanned aerial vehicle holder further comprises a sealing part (8);

the closing part (8) comprises an oblique movable rod (81) inserted into the oblique opening (4) and a sealing cover (82) arranged at the lower end of the oblique movable rod (81), wherein the oblique movable rod is connected with the sealing cover;

magnetite (1) laminating behind mounting (2), mounting (2) can extrude two sets ofly cover (3) are stored to adhesion agent, so that slant movable rod (81) pressurized drives closing cap (82) descend.

5. The adhesive magnet for the PTZ of the unmanned aerial vehicle as claimed in claim 4,

the closing part (8) further comprises an oblique sliding chute (84) connected to the oblique opening (4), a sliding block (83) arranged in the oblique sliding chute (84) and a first spring (85) connected between the sliding block (83) and the oblique sliding chute (84), wherein the sliding block (83) is connected to one side of the oblique movable rod (81);

after the oblique movable rod (81) is pressed to drive the sealing cover (82) to descend, the movable rod can drive the sliding block (83) to slide along the sliding groove (84), so that the first spring (85) is compressed.

6. The adhesive magnet for the PTZ of the unmanned aerial vehicle as claimed in claim 5,

the sliding block (83) is hemispherical.

7. The adhesive magnet for the PTZ of the unmanned aerial vehicle as claimed in claim 6,

the adhesion magnet for the unmanned aerial vehicle holder further comprises an elastic part (9);

the elastic part (9) comprises a plurality of fixing rods (91) arranged on the inner sides of the two groups of the adhesive storage sleeves (3) in a mirror image manner, a plurality of second springs (92) arranged between the inner sides of the two groups of the adhesive storage sleeves (3) and the plurality of fixing rods (91) in a mirror image manner, and the two adjacent groups of the fixing rods (91) are hinged and fixed, wherein;

magnetite (1) laminating behind mounting (2), mounting (2) can extrude two sets ofly cover (3) are stored to the adhesion agent, so that it is a plurality of dead lever (91) rotation drives a plurality of second springs (92) compression.