CN215851840U

CN215851840U - Unmanned aerial vehicle moves airfoil quick assembly disassembly's constructional device entirely

Info

Publication number: CN215851840U
Application number: CN202122561739.8U
Authority: CN
Inventors: 金�一; 刘晨晖; 李新
Original assignee: Jiangxi Tongyi Uav Technology Co ltd
Current assignee: Jiangxi Tongyi Uav Technology Co ltd
Priority date: 2021-10-25
Filing date: 2021-10-25
Publication date: 2022-02-18
Anticipated expiration: 2031-10-25

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, and particularly discloses a structural device for quickly dismounting a full-motion wing surface of an unmanned aerial vehicle. Through the fixed plate, the notch plate, the connecting piece, the metal sleeve, the position structural design of connecting rod and becket, effectively realized between antagonism stay bolt and the unmanned aerial vehicle mounting base dismantle effect rapid and convenient more, need not the staff and utilize assembly and disassembly tools to come to antagonize in addition and operate between stay bolt and the unmanned aerial vehicle, and simultaneously, position structure and the line design of tensile bolt nut part through spring telescopic link and splint, can effectively realize the protection restriction effect to tensile bolt, thereby make the connection status between tensile bolt and the unmanned aerial vehicle more stable, safety.

Description

Unmanned aerial vehicle moves airfoil quick assembly disassembly's constructional device entirely

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a structural device for quickly dismounting and mounting a full-motion wing surface of an unmanned aerial vehicle.

Background

Unmanned aerial vehicle is unmanned aerial vehicle of unmanned aerial vehicle cockpit on board, internally mounted has each equipment such as automatic pilot, program control device, remote control station personnel then track it through equipment such as remote control radar, operations such as location or control, however, there is inconvenience when utilizing to be connected or dismantle between bolt and the base with the wing, it consumes longer time to dismantle it to need the staff to utilize external instrument to handle, and after long-time the use, it utilizes the position department that the bolt connects the phenomenon that becomes flexible easily to appear, be unfavorable for long-time safe handling, therefore, it is necessary to design a full-motion wing face quick assembly disassembly's of unmanned aerial vehicle constructional device, thereby solve the above-mentioned problem.

SUMMERY OF THE UTILITY MODEL

Aiming at the defects of the prior art, the utility model provides the structural device for quickly dismounting the full-motion wing surface of the unmanned aerial vehicle, which has the advantages of rapidness and convenience in dismounting, restriction effect on bolts and the like, and solves the problems of inconvenience in dismounting and poor safety of the traditional unmanned aerial vehicle wing.

The utility model discloses a structural device for quickly dismounting and mounting a full-motion wing surface of an unmanned aerial vehicle, which comprises an unmanned aerial vehicle wing, two mounting plates and a tensile bolt, wherein a nut part of the tensile bolt is provided with a metal block, the right side surface of each mounting plate is provided with two fixing plates, the inner sides of the fixing plates are all provided with spring telescopic rods, the output ends of the spring telescopic rods are provided with clamping plates, the surfaces of the clamping plates and the nut part of the metal block are respectively carved with meshed lines, the outer sides of the fixing plates are all provided with slide ways, concave plates are respectively arranged between the fixing plates through the slide ways, the inner concave surfaces of the concave plates are provided with rotating grooves and are rotatably connected with connecting pieces, the left side surface of each connecting piece is provided with a metal sleeve, the right side of each connecting piece is provided with a connecting rod, and the outer sides of the connecting rods are provided with a plurality of metal rods.

Through the design of the technical scheme, the unmanned aerial vehicle wing can be assembled and disassembled more conveniently and rapidly without operating by using an external tool, and meanwhile, the limiting effect of the tensile bolts for installation can be realized, so that the tensile bolts can be always kept in a stable state with the unmanned aerial vehicle installation base.

As a further design of the utility model, equidistant spaces are reserved among the metal rods, and metal rings are annularly arranged among the end parts of the metal rods.

Through the design of the technical scheme, the metal sleeve pressing device is more beneficial to the working personnel to press and rotate the metal sleeve.

As a further design of the utility model, the inner diameter of the metal sleeve is larger than the outer diameter of the metal block, and a plurality of rubber pads are arranged on the inner side of the metal sleeve.

Through the design of the technical scheme, the limiting effect on the metal block can be realized, and the installation between the tension resisting bolt and the installation plate and between the tension resisting bolt and the installation base can be more favorably realized.

As a further design of the present invention, the concave surface of the concave plate is provided with two convex plates, the surfaces of the plurality of convex plates are provided with first protrusions, the surface of the spring telescopic rod output rod is provided with a special-shaped plate, and the surface of the special-shaped plate is provided with second protrusions corresponding to the first protrusions.

Through the design of the technical scheme, the driving effect of the spring telescopic rod output rod can be realized, so that the clamping plate and the tensile bolt are kept away from each other, and the anti-tension bolt is more favorably subjected to dismounting operation.

As a further design of the utility model, the first protrusion and the second protrusion are both designed in a semicircular structure, and the surfaces of the first protrusion and the second protrusion are both designed to be smooth surfaces.

Through the design of the technical scheme, the first bulge is more favorable for the second bulge to have a jacking effect.

As a further design of the utility model, a group of limiting plates are arranged on the surface of the spring telescopic rod fixing rod, and a plurality of groups of limiting plates are respectively positioned on the outer sides of the special-shaped plates and are mutually contacted.

Through the design of the technical scheme, the limiting effect on the output rod of the telescopic spring rod can be realized, and the situation that the output rod of the telescopic spring rod drives the special-shaped plate and the second protrusion to rotate and displace is prevented from occurring.

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

1. according to the utility model, through the position structure design of the fixing plate, the concave plate, the connecting piece, the metal sleeve, the connecting rod and the metal ring, the effect that the anti-pulling bolt and the unmanned aerial vehicle mounting base are disassembled more rapidly and conveniently is effectively realized, a worker does not need to additionally utilize a disassembling tool to operate between the anti-pulling bolt and the unmanned aerial vehicle, and meanwhile, through the position structures of the spring telescopic rod and the clamping plate and the line design of the nut part of the anti-pulling bolt, the protection limiting effect on the anti-pulling bolt can be effectively realized, so that the connection state between the anti-pulling bolt and the unmanned aerial vehicle is more stable and safer.

2. According to the utility model, through the position structural design of the convex plate, the first bulge, the special-shaped plate and the second bulge, workers can conveniently detach the tensile bolt by using the metal sleeve, the inconvenient situation that the connection state between the clamping plate and the tensile bolt needs to be manually and independently processed by the workers is prevented, the limiting effect on the output rod of the telescopic spring rod can be realized through the structural design of the limiting plate, and the situation that the output rod of the telescopic spring rod rotates randomly is prevented.

Drawings

The accompanying drawings, which are included to provide a further understanding of the application and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the application and together with the description serve to explain the application and not to limit the application. In the drawings:

FIG. 1 is a schematic front view of the present invention;

fig. 2 is a schematic front sectional view of the fixing plate according to the present invention.

In the figure: 1. an unmanned wing; 2. mounting a plate; 3. a tensile bolt; 4. a metal block; 5. a fixing plate; 6. a slideway; 7. a concave plate; 8. a connecting member; 9. a metal sleeve; 10. a rubber pad; 11. a connecting rod; 12. a metal ring; 13. a convex plate; 14. a first protrusion; 15. a spring telescopic rod; 16. a splint; 17. a shaped plate; 18. a second protrusion; 19. a limiting plate; 20. a metal rod.

Detailed Description

In the following description, for purposes of explanation, numerous specific details are set forth in order to provide a thorough understanding of the various embodiments of the utility model. It should be understood, however, that these physical details should not be construed as limiting the utility model. That is, in some embodiments of the utility model, such physical details are not necessary. In addition, some conventional structures and components are shown in simplified schematic form in the drawings.

In addition, the descriptions related to the first, the second, etc. in the present invention are only used for description purposes, do not particularly refer to an order or sequence, and do not limit the present invention, but only distinguish components or operations described in the same technical terms, and are not understood to indicate or imply relative importance or implicitly indicate the number of indicated technical features. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In addition, technical solutions between various embodiments may be combined with each other, but must be realized by a person skilled in the art, and when the technical solutions are contradictory or cannot be realized, such a combination should not be considered to exist, and is not within the protection scope of the present invention.

Referring to fig. 1-2, the structural device for quickly dismounting and mounting a full-motion wing surface of an unmanned aerial vehicle comprises an unmanned aerial vehicle wing 1, two mounting plates 2 and a tensile bolt 3, wherein a nut part of the tensile bolt 3 is provided with a metal block 4, the right side surface of the mounting plate 2 is provided with two fixing plates 5, the inner sides of the fixing plates 5 are all provided with spring telescopic rods 15, the output ends of the spring telescopic rods 15 are provided with clamping plates 16, the surfaces of the clamping plates 16 and the nut part of the metal block 4 are all engraved with meshed lines, the outer sides of the fixing plates 5 are all provided with slideways 6, concave plates 7 are respectively arranged among the fixing plates 5 through the slideways 6, the inner concave surfaces of the concave plates 7 are provided with rotating grooves and are rotatably connected with a connecting piece 8, the left side surface of the connecting piece 8 is provided with a metal sleeve 9, the right side of the connecting piece 8 is provided with a connecting rod 11, and the outer sides of the connecting rod 11 are provided with a plurality of metal rods 20, have equidistant space between a plurality of metal poles 20 in advance, be equipped with becket 12 along the annular between the tip of a plurality of metal poles 20, through the design of above-mentioned technical scheme, can obtain 1 dismouting of this unmanned aerial vehicle wing more convenient rapidly, need not to utilize external instrument to operate, simultaneously, can realize realizing the restriction effect to the tensile bolt 3 of installation usefulness, make it can with unmanned aerial vehicle mount pad between can remain stable state all the time.

Referring to fig. 2, the inner diameter of the metal sleeve 9 is larger than the outer diameter of the metal block 4, and the inner side of the metal sleeve 9 is provided with a plurality of rubber pads 10, so that the metal block 4 can be limited by the above technical scheme, and the installation of the tensile bolt 3, the installation plate 2 and the installation base is facilitated.

Please refer to fig. 1-2, the concave surface of the concave plate 7 is provided with two convex plates 13, the surfaces of the convex plates 13 are provided with first protrusions 14, the surface of the output rod of the spring telescopic rod 15 is provided with a special-shaped plate 17, the surface of the special-shaped plate 17 is provided with second protrusions 18 corresponding to the first protrusions 14, the first protrusions 14 and the second protrusions 18 are both in a semicircular structure design, the surfaces of the first protrusions 14 and the second protrusions 18 are both set to be smooth surfaces, through the above technical scheme design, the driving effect of the output rod of the spring telescopic rod 15 can be realized, the clamping plate 16 and the tensile bolt 3 are kept away from each other, the anti-tensile bolt 3 can be more favorably disassembled and assembled, and the first protrusions 14 can be more favorably jacked to the second protrusions 18.

Referring to fig. 1-2, a set of limiting plates 19 is disposed on the surface of the fixing rod of the spring telescopic rod 15, and the multiple sets of limiting plates 19 are respectively located outside the special-shaped plate 17 and contact with each other.

When the utility model is used, if the tensile bolt 3 connected with the mounting base of the unmanned aerial vehicle needs to be disassembled, a worker can directly hold the connecting rod 11 to push the concave plate 7 to the inner side, in the pushing process, the first bulge 14 forces the second bulge 18, the special-shaped plate 17, the clamping plate 16, the spring telescopic rod 15 and the nut part of the tensile bolt 3 to be far away, then the metal sleeve 9 is rotationally adjusted and sleeved on the outer side of the metal block 4, so that the rubber pad 10 is pressed and deformed and is tightly contacted with the surface of the metal block 4, then the metal rods 20 and the metal rings 12 arranged on the outer side of the connecting rod 11 are used for pressing and rotating, the tensile bolt 3 is forced to rotate through the metal sleeve 9 and the metal block 4, so that the tensile bolt 3 drives the concave plate 7 to simultaneously slide when moving to the outer side until the tensile bolt 3 is separated from the mounting base and the mounting plate 2, finally to through 4 joints of metal block in metal sleeve 9 in tensile bolt 3 take out can, if need to confront tensile bolt 3 and install again, then the staff can utilize 4 joints of metal block in metal sleeve 9's inside with tensile bolt 3, later with it inboard promotion and rotation once more, until confront tensile bolt 3 installation completion can.

The above description is only an embodiment of the present invention, and is not intended to limit the present invention. Various modifications and alterations to this invention will become apparent to those skilled in the art. Any modification, equivalent replacement, improvement or the like made within the spirit and principle of the present invention should be included in the scope of the claims of the present invention.

Claims

1. The utility model provides an unmanned aerial vehicle moves airfoil quick assembly disassembly's constructional device entirely, includes unmanned aerial vehicle wing (1) and two mounting panels (2) and tensile bolt (3), its characterized in that: the nut part of the tensile bolt (3) is provided with a metal block (4), the right side surface of the mounting plate (2) is provided with two fixing plates (5), the inner sides of the fixing plates (5) are all provided with spring telescopic rods (15), the output end of the spring telescopic rod (15) is provided with a clamping plate (16), the surfaces of the clamping plate (16) and the nut part of the metal block (4) are all carved with meshed grains, the outer sides of the fixing plates (5) are all provided with a slideway (6), concave plates (7) are respectively arranged between the fixing plates (5) through the slideway (6), the inner concave surfaces of the concave plates (7) are provided with rotating grooves, and is rotationally connected with a connecting piece (8), the left side surface of the connecting piece (8) is provided with a metal sleeve (9), the right side of connecting piece (8) is equipped with connecting rod (11), the outside of connecting rod (11) is equipped with a plurality of metal poles (20).

2. The structural device for quickly dismounting and mounting the full-motion airfoil of the unmanned aerial vehicle according to claim 1, is characterized in that: equidistant spaces are reserved among the metal rods (20), and metal rings (12) are annularly arranged among the end parts of the metal rods (20).

3. The structural device for quickly dismounting and mounting the full-motion airfoil of the unmanned aerial vehicle according to claim 1, is characterized in that: the inner diameter of the metal sleeve (9) is larger than the outer diameter of the metal block (4), and a plurality of rubber pads (10) are arranged on the inner side of the metal sleeve (9).

4. The structural device for quickly dismounting and mounting the full-motion airfoil of the unmanned aerial vehicle according to claim 1, is characterized in that: the interior concave surface of concave plate (7) is equipped with two flange (13), and is a plurality of the surface of flange (13) all is equipped with first arch (14), the surface of spring telescopic link (15) delivery rod is equipped with dysmorphism board (17), the surface of dysmorphism board (17) is equipped with and first protruding (14) corresponding second arch (18).

5. The structural device for rapid dismounting and mounting of the full-motion airfoil of the unmanned aerial vehicle as claimed in claim 4, wherein: the first protrusion (14) and the second protrusion (18) are both designed to be of a semicircular structure, and the surfaces of the first protrusion (14) and the second protrusion (18) are both smooth surfaces.

6. The structural device for quickly dismounting and mounting the full-motion airfoil of the unmanned aerial vehicle according to claim 1, is characterized in that: the surface of the fixing rod of the spring telescopic rod (15) is provided with a group of limiting plates (19), and the multiple groups of limiting plates (19) are respectively positioned at the outer sides of the special-shaped plates (17) and are in mutual contact.