CN212580151U

CN212580151U - Unmanned aerial vehicle article carry structure

Info

Publication number: CN212580151U
Application number: CN202021539934.XU
Authority: CN
Inventors: 徐旺
Original assignee: Hunan Jiefei Technology Co ltd
Current assignee: Hunan Jiefei Technology Co ltd
Priority date: 2020-07-29
Filing date: 2020-07-29
Publication date: 2021-02-23
Anticipated expiration: 2030-07-29

Abstract

The utility model relates to the technical field of unmanned aerial vehicle article mounting, in particular to an unmanned aerial vehicle article mounting structure, which is convenient for the rapid installation and disassembly of the hook shell and the machine body, is easy to change the use function of the unmanned aerial vehicle according to the use requirement of the unmanned aerial vehicle, has lower use limitation and better adaptability, meanwhile, the supporting plate in the supporting frame can adjust the height according to the size of the hung object, has higher practicability and comprises a machine body and a hook shell, the equal fixedly connected with slip pipe in bottom front side and the bottom rear side of organism, two the handle hole has all been seted up to the one end of keeping away from each other of slip pipe, and the equal sliding connection of left side inner wall and the right side inner wall of slip pipe has a slide bar, two the equal fixedly connected with action bars in the one end that is close to each other of slide bar, two the one end fixedly connected with pressure spring that is close to each other of action bar, two the equal fixedly connected with locking plate in the one end that is kept away from each other of slide bar.

Description

Unmanned aerial vehicle article carry structure

Technical Field

The utility model relates to an unmanned aerial vehicle article carry technical field specifically is an unmanned aerial vehicle article carry structure.

Background

As is known, the unmanned aerial vehicle article carry structure is one kind and is used for unmanned aerial vehicle article transportation in-process, carries out article carry to the auxiliary device of better transportation article, it obtains extensive application in unmanned aerial vehicle article transportation field.

Chinese patent is CN 201922003995.8's utility model discloses an unmanned aerial vehicle article carry structure, it includes the organism, the undercarriage connecting plate, the couple casing, the lead screw, the hand wheel, servo motor, the couple, female piece of joint subblock and joint, the organism is connected with the undercarriage connecting plate, the undercarriage connecting plate welds with the couple casing mutually, couple casing and female piece sliding connection of joint subblock and joint, be provided with mechanisms such as lead screw in the inside intracavity of couple casing, the one end and the hand wheel connection of lead screw, the other end and servo motor's the output of lead screw are connected, the bottom and the couple of couple casing are connected, when using, hang article on the couple, form the support to the object with the mutual joint of female piece of joint subblock and joint, the transportation of unmanned aerial vehicle completion article.

However, the above prior art solutions still have the following drawbacks: its organism undercarriage connecting plate is the welding with the couple casing, and it is comparatively inconvenient to dismantle, is difficult for changing unmanned aerial vehicle's service function according to unmanned aerial vehicle's user demand, and the use limitation is higher, and adaptability is relatively poor to the joint subblock is highly fixed with the object support frame that the female piece joint of joint formed, is difficult for adjusting to the size of hanging dress object, thereby leads to its practicality relatively poor.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

Not enough to prior art, the utility model provides an installation and dismantlement convenient to couple casing and organism are quick, and it needs to change unmanned aerial vehicle's service function according to unmanned aerial vehicle's use more easily, uses the limitation lower, and adaptability is better, and the backup pad in its support frame can carry out altitude mixture control to the size of hanging the dress object simultaneously, the higher unmanned aerial vehicle article carry structure of practicality.

(II) technical scheme

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle article hanging structure comprises a machine body and a hook shell, wherein sliding pipes are fixedly connected to the front side of the bottom end and the rear side of the bottom end of the machine body, operation holes are formed in the ends, far away from each other, of the two sliding pipes, sliding rods are slidably connected to the inner walls of the left side and the right side of each sliding pipe, the ends, close to each other, of the two sliding rods are fixedly connected with operation rods, the ends, close to each other, of the two operation rods are fixedly connected with pressure springs, the ends, far away from each other, of the two sliding rods are fixedly connected with locking plates, the ends, far away from each other, of the two locking plates are fixedly connected with wedges, a quick-connection hook is arranged at the bottom end of the hook shell, locking grooves matched with the wedges are formed in the positions of four corners of the top end of the hook shell, an installation cavity is arranged in the hook shell, the sliding hole is communicated with the installation cavity, a sliding rod is installed in the installation cavity, the left end and the right end of the sliding rod are fixedly connected with the inner wall of the installation cavity, the outer wall of the left side and the outer wall of the right side of the sliding rod are respectively sleeved with a pushing spring, one end of each pushing spring, which is close to each other, is fixedly connected with a vertical plate, the bottom ends of the two vertical plates are respectively connected with the inner bottom wall of the installation cavity in a sliding manner, the bottom ends of the two vertical plates are respectively fixedly connected with a connecting block which is connected with the sliding hole in a sliding manner, the bottom ends of the two connecting blocks, the bottom of left guide arm and the bottom of right guide arm all fixedly connected with backup pad, two the one end that is close to each other of backup pad is respectively fixedly connected with concave joint fishplate bar and the convex joint fishplate bar of mutually supporting, two the bottom of backup pad all rotates and is connected with the threaded rod to the bottom threaded connection of the top of threaded rod and connecting block.

Preferably, the top ends of the two support plates are fixedly connected with a baffle, and the baffle is connected with the connecting block in a sliding manner.

Preferably, the four corners of the bottom end of the machine body are fixedly connected with limit blocks for limiting the position of the locking plate.

Preferably, the bottom ends of the two threaded rods are fixedly connected with rotating discs.

Preferably, a plurality of rotating rods are fixedly connected to the side wall of the rotating disc.

Preferably, oil filler points are arranged on the outer side wall of the left side and the outer side wall of the right side of the sliding pipe respectively, and the oil filler points are communicated with the inside of the sliding pipe.

Preferably, the compression spring and the push spring are both made of high-strength and high-toughness metal materials.

(III) advantageous effects

Compared with the prior art, the utility model provides an unmanned aerial vehicle article carry structure possesses following beneficial effect:

1. this unmanned aerial vehicle article carry structure, through the design in wedge and locking groove, the organism of being convenient for and the installation and the dismantlement of couple casing, the easy service function that needs to change unmanned aerial vehicle according to unmanned aerial vehicle's use, the use flexibility is higher, adaptability is better, through the cooperation of pressure spring, action bars, slide bar and slip pipe, be convenient for realize the organism and the quick lock installation and the dismantlement of couple casing, it is comparatively convenient to use.

2. This unmanned aerial vehicle article carry structure, through the cooperation of connecting block, left guide arm, right guide arm and threaded rod, be convenient for carry out the regulation of backup pad height according to the size of carry article, the practicality is higher.

Drawings

Fig. 1 is a schematic sectional perspective view of the present invention;

FIG. 2 is a schematic view of a portion of the enlarged structure of FIG. 1;

FIG. 3 is a schematic view of the overall three-dimensional structure of the present invention;

fig. 4 is a schematic diagram of a partial enlarged structure at B in fig. 3 according to the present invention.

In the figure: 1. a body; 2. a hook housing; 3. a sliding tube; 4. a slide bar; 5. an operating lever; 6. a pressure spring; 7. a locking plate; 8. a wedge block; 9. a quick-connection hook; 10. a slide bar; 11. pushing a spring; 12. a vertical plate; 13. connecting blocks; 14. a left guide bar; 15. a right guide bar; 16. a support plate; 17. concave splice plates; 18. a convex connector tile; 19. a threaded rod; 20. a baffle plate; 21. a limiting block; 22. rotating the disc; 23. rotating the rod; 24. and an oil filling hole.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Examples

Referring to fig. 1-4, an unmanned aerial vehicle article carrying structure comprises a machine body 1 and a hook housing 2, wherein both the front side and the rear side of the bottom end of the machine body 1 are fixedly connected with a sliding tube 3, the installation of the sliding rods 4 is facilitated, operation holes are formed at the ends of the two sliding tubes 3 far away from each other, the operation rods 5 are conveniently operated, the inner walls of the left side and the right side of the sliding tubes 3 are respectively and slidably connected with a sliding rod 4, the ends of the two sliding rods 4 close to each other are respectively and fixedly connected with an operation rod 5, the ends of the two operation rods 5 close to each other are respectively and fixedly connected with a pressure spring 6, the quick lock installation and disassembly of the machine body 1 and the hook housing 2 are conveniently realized, the use is convenient, the ends of the two sliding rods 4 far away from each other are respectively and fixedly connected with a locking plate 7, the ends of the two locking plates 7 far away from each other are respectively, the hook comprises a hook shell 2, a hook body 1 and a hook shell 2, wherein the hook shell 2 is provided with a plurality of locking grooves matched with wedge blocks 8 at four corners at the top end, the hook shell is convenient to mount and dismount, the use function of an unmanned aerial vehicle can be changed easily according to the use requirement of the unmanned aerial vehicle, the hook shell 2 is high in use flexibility and good in adaptability, a mounting cavity is arranged in the hook shell 2, the left side and the right side of the bottom end of the hook shell 2 are respectively provided with a sliding hole which is communicated with the mounting cavity, a sliding rod 10 is arranged in the mounting cavity, the left end and the right end of the sliding rod 10 are respectively fixedly connected with the inner wall of the mounting cavity, the outer wall at the left side and the outer wall at the right side of the sliding rod 10 are respectively sleeved with a push spring 11, one ends, close to each other, of the two push springs 11 are respectively and fixedly connected with a vertical plate 12, the concave, the bottom of two risers 12 all fixedly connected with sliding hole sliding connection's connecting block 13, the bottom of two connecting blocks 13 respectively sliding connection have a plurality of left guide arms 14 and a plurality of right guide arms 15, be convenient for direction when backup pad 16 altitude mixture control removes, the bottom of left guide arm 14 and the bottom of right guide arm 15 all fixedly connected with backup pad 16, the one end that is close to each other of two backup pads 16 respectively fixedly connected with concave joint plate 17 and convex joint plate 18 of mutually supporting, the bottom of two backup pads 16 all rotates and is connected with threaded rod 19, and the top of threaded rod 19 and the bottom threaded connection of connecting block 13, be convenient for carry out the regulation of backup pad 16 height according to the size of hanging load article, the practicality is higher, the equal fixedly connected with baffle 20 in top of two backup pads 16, and baffle 20 and connecting block 13 sliding connection, be convenient for protect article, be convenient for simultaneously left guide, The right guide rod 15 and the threaded rod 19 are used for protection, the use reliability is higher, the four corners of the bottom end of the machine body 1 are fixedly connected with limiting blocks 21 for limiting the position of the locking plate 7, the relative positions of the two sliding rods 4 are convenient to limit, the use reliability is improved, the bottom ends of the two threaded rods 19 are fixedly connected with rotating discs 22, the threaded rods 19 are convenient to twist, thereby facilitating the height adjustment of the supporting plate 16, the side wall of the rotating disc 22 is fixedly connected with a plurality of rotating rods 23 which facilitate the rotation of the threaded rod 19, saving labor, the left side outer side wall and the right side outer side wall of the sliding pipe 3 are both provided with oil injection holes 24, and oil filler point 24 is linked together with the inside of sliding tube 3, is convenient for annotate the oil, improves lubricated effect, and the reliability of use is higher, and pressure spring 6 and push away spring 11 and all adopt high strength high tenacity metal material, are convenient for improve the reliability of use.

In conclusion, the working principle and the working process of the unmanned aerial vehicle article mounting structure are that, when in use, the locking groove at the top end of the hook shell 2 is aligned with the bottom end of the wedge-shaped block 8, the hook shell 2 is lifted upwards relative to the machine body 1, the wedge-shaped block 8 moves under the action of the pressure of the locking groove and overcomes the elastic force of the pressure spring 6, the wedge-shaped block 8 is completely immersed into the pressing groove to complete the connection between the machine body 1 and the hook shell 2, the mounted article is hung on the quick-connecting hook 9, the rotating rod 23 is pushed, the rotating rod 23 drives the threaded rod 19 to rotate through the rotating disc 22, so that the relative height of the supporting plate 16 is changed, the height of the supporting plate 16 is adjusted according to the height of the mounted article, after the adjustment is completed, the two connecting blocks 13 are respectively separated to the left, the object is adjusted to contact the supporting plate 16, the two connecting plates, through the cooperation of concave joint piece and protruding joint piece, improve the supporting effect of backup pad 16, when unmanned aerial vehicle is used for other usage, with the close promotion of two action bars 5, the elasticity that pressure spring 6 was overcome in thrust makes the close removal of slide bar 4, slide bar 4 drives wedge 8 through locking plate 7 and removes, thereby make wedge 8 withdraw from the locking inslot, accomplish the dismantlement of couple casing 2 and organism 1, unmanned aerial vehicle is more easily used for other usage, the use flexibility is higher, it is comparatively convenient to operate.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an unmanned aerial vehicle article carry structure, includes organism (1) and couple casing (2), its characterized in that: the bottom front side and the bottom rear side of the machine body (1) are fixedly connected with sliding pipes (3), the ends of the two sliding pipes (3) far away from each other are respectively provided with an operation hole, the left inner wall and the right inner wall of the sliding pipes (3) are respectively and slidably connected with sliding rods (4), the ends of the two sliding rods (4) close to each other are respectively and fixedly connected with an operation rod (5), the ends of the two operation rods (5) close to each other are respectively and fixedly connected with a pressure spring (6), the ends of the two sliding rods (4) far away from each other are respectively and fixedly connected with a locking plate (7), the ends of the two locking plates (7) far away from each other are respectively and fixedly connected with a wedge block (8), the bottom end of the hook shell (2) is provided with a quick-connection hook (9), and the positions of four corners at the top end of the hook shell (2) are respectively provided with a, a mounting cavity is arranged in the hook shell (2), sliding holes are formed in the left side and the right side of the bottom end of the hook shell (2) and communicated with the mounting cavity, a sliding rod (10) is mounted in the mounting cavity, the left end and the right end of the sliding rod (10) are fixedly connected with the inner wall of the mounting cavity, pushing springs (11) are sleeved on the outer wall of the left side and the outer wall of the right side of the sliding rod (10), vertical plates (12) are fixedly connected to the ends, close to each other, of the two pushing springs (11), the bottom ends of the two vertical plates (12) are slidably connected with the inner bottom wall of the mounting cavity, connecting blocks (13) slidably connected with the sliding holes are fixedly connected to the bottom ends of the two vertical plates (12), a plurality of left guide rods (14) and a plurality of right guide rods (15) are slidably connected to the bottom ends of the two connecting blocks (13), and supporting plates (16) are fixedly connected to the bottom ends, the two supporting plates (16) are fixedly connected with a concave connecting plate (17) and a convex connecting plate (18) which are matched with each other at one end close to each other respectively, a threaded rod (19) is rotatably connected to the bottom ends of the two supporting plates (16), and the top end of the threaded rod (19) is in threaded connection with the bottom end of the connecting block (13).

2. The unmanned aerial vehicle article mounting structure of claim 1, wherein: the top ends of the two supporting plates (16) are fixedly connected with a baffle (20), and the baffle (20) is in sliding connection with the connecting block (13).

3. The unmanned aerial vehicle article mounting structure of claim 2, wherein: the bottom four corners of the machine body (1) are fixedly connected with limit blocks (21) used for limiting the position of the locking plate (7).

4. The unmanned aerial vehicle article mounting structure of claim 3, wherein: the bottom ends of the two threaded rods (19) are fixedly connected with rotating discs (22).

5. The unmanned aerial vehicle article mounting structure of claim 4, wherein: the side wall of the rotating disc (22) is fixedly connected with a plurality of rotating rods (23).

6. The unmanned aerial vehicle article mounting structure of claim 5, wherein: oil filler point (24) have all been seted up on the left side lateral wall of slip pipe (3) and on the right side lateral wall to oil filler point (24) are linked together with the inside of slip pipe (3).

7. The unmanned aerial vehicle article mounting structure of claim 6, wherein: the pressure spring (6) and the push spring (11) are both made of high-strength and high-toughness metal materials.