CN221114411U - Super-large span unmanned aerial vehicle final assembly transfer device - Google Patents
Super-large span unmanned aerial vehicle final assembly transfer device Download PDFInfo
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- CN221114411U CN221114411U CN202323033951.2U CN202323033951U CN221114411U CN 221114411 U CN221114411 U CN 221114411U CN 202323033951 U CN202323033951 U CN 202323033951U CN 221114411 U CN221114411 U CN 221114411U
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- 238000012546 transfer Methods 0.000 title claims abstract description 57
- 238000006073 displacement reaction Methods 0.000 claims abstract description 19
- 238000013016 damping Methods 0.000 claims description 10
- 239000002184 metal Substances 0.000 claims description 3
- 244000309464 bull Species 0.000 claims 2
- 238000000034 method Methods 0.000 abstract description 12
- 230000003405 preventing effect Effects 0.000 abstract description 4
- 238000013461 design Methods 0.000 description 9
- 230000000694 effects Effects 0.000 description 8
- 230000002349 favourable effect Effects 0.000 description 6
- 238000003860 storage Methods 0.000 description 5
- 230000009286 beneficial effect Effects 0.000 description 3
- 239000007769 metal material Substances 0.000 description 3
- 238000004891 communication Methods 0.000 description 2
- 238000000151 deposition Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
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- 239000011435 rock Substances 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
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Abstract
The utility model discloses an oversized-span unmanned aerial vehicle assembly transfer device, and relates to the technical field of unmanned aerial vehicles. The automatic transfer box comprises a transfer box body, wherein a placing plate is connected inside the transfer box body in a sliding manner, a supporting rod is fixedly connected to the side face of the transfer box body, a fixing device is arranged on the side face of the transfer box body, the fixing device comprises a control box, the side face of the control box body is fixedly connected to the bottom of the supporting rod, and a supporting rod is fixedly connected to the top of the control box body. According to the utility model, through the mutual matching among components such as the control box, the motor, the worm wheel, the gear bar and the like in the fixing device, the unmanned aerial vehicle is clamped and fixed in the transferring process of the unmanned aerial vehicle assembly, the displacement preventing effect is realized, the displacement, jolt or collision in the transporting and carrying processes can be effectively prevented, the damage risk is reduced, the unmanned aerial vehicle displacement is prevented, and the safety of operators and other personnel is ensured.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to an oversized-span unmanned aerial vehicle final assembly transfer device.
Background
With the development of multi-rotor unmanned aerial vehicle technology, multi-rotor unmanned aerial vehicles are increasingly applied to the production field, and higher requirements are also put forward on unmanned aerial vehicle transportation. At present, a device for transferring unmanned aerial vehicles can only transfer an unmanned aerial vehicle alone, and load unmanned aerial vehicle on transfer device and remove unmanned aerial vehicle from transfer device's process more difficult, work efficiency is lower.
According to a publicly-shown unmanned aerial vehicle transfer device (CN 215513722U), this unmanned aerial vehicle transfer device includes frame and roll-over stand, is provided with in the frame and is used for depositing unmanned aerial vehicle's first storage area and with the opening of first storage area intercommunication, the roll-over stand rotates with the frame to be connected to open or seal the opening, the roll-over stand deviates from the first second storage area that is used for depositing unmanned aerial vehicle that stores of one side regional formation of storage area. Unmanned aerial vehicle assembly is in the in-process of transporting, unmanned aerial vehicle deposits in the inside of transfer box, can rock and the displacement at its inside, and the displacement can make unmanned aerial vehicle produce jolting and collision, has increased the risk of damage, consequently need reduce the risk of damage and reduce jolting and collision, mutually support between components such as through roll-over stand, frame, first storage area, be difficult to realize reducing the risk of damage and reduce jolting collision, wait to improve.
Disclosure of utility model
The utility model aims to provide the unmanned aerial vehicle assembly transfer device with the ultra-large span, which realizes the effects of clamping and fixing the unmanned aerial vehicle in the transfer process and preventing displacement by mutually matching components such as a control box, a motor, a worm wheel, a gear bar and the like in the fixing device, can effectively prevent displacement, jolt or collision in the transportation and carrying processes, reduces the risk of damage, prevents the unmanned aerial vehicle from displacing, is also helpful for ensuring the safety of operators and other personnel, and solves the existing problems.
In order to solve the technical problems, the utility model is realized by the following technical scheme:
The utility model relates to an oversized span unmanned aerial vehicle final assembly transfer device which comprises a transfer box, wherein a placing plate is connected inside the transfer box in a sliding manner, a supporting rod is fixedly connected to the side face of the transfer box, a fixing device is arranged on the side face of the transfer box, the fixing device comprises a control box, the side face of the control box is fixedly connected to the bottom of the supporting rod, a supporting rod is fixedly connected to the top of the control box, one end, far away from the control box, of the supporting rod is fixedly connected with a motor, a worm is fixedly connected to an output shaft of the motor, a rotating rod is connected to the inner wall of the control box in a rotating manner, a worm wheel is fixedly connected to the circumferential face of the rotating rod, a round rod is connected to the inner wall of the control box in a rotating manner, a gear bar is fixedly connected to the circumferential face of the round rod, a clamping rod is fixedly connected to the bottom of the gear bar, and a notch is formed in the top of the control box.
Further, worm wheel intermeshing, worm wheel, gear strip are provided with two, and along the vertical axis mutual symmetry of control box, the spout has been seted up to the side of control box, the spout is located the displacement orbit of gear strip, and such design is favorable to making worm drive the worm wheel rotation.
Further, the clamping rods, the supporting rods and the supporting rods are arranged in two, and are symmetrical to each other along the vertical central axis of the control box, the fixing devices are arranged in two groups, and are symmetrical to each other along the vertical central axis of the transfer box, so that the two sides can be operated at the same time, and the two sides of the transfer box can be clamped.
Further, be provided with damping device on the inner wall of transfer case, damping device includes the base, the bottom fixedly connected with of base is on the inner wall of transfer case, place the bottom fixedly connected with connector of board, rotate on the inner wall of connector and be connected with the dwang, fixedly connected with connecting rod on the periphery of dwang, the side fixedly connected with stock of base, sliding connection has the fixed block on the periphery of stock, the one end fixedly connected with of dwang is kept away from at the top of fixed block to the connecting rod, the side fixedly connected with spring of fixed block, the one end fixedly connected with of fixed block is kept away from to the spring is on the periphery of stock, and such design is favorable to alleviateing the effect of vibration and impact.
Further, connector, dwang, connecting rod, fixed block are provided with two, and along the vertical axis mutual symmetry of stock, the fixed block sets up to the metal material, and such design is favorable to making for a long time use, and is not fragile.
Further, the base is provided with two, damping device is located the bottom of placing the board, the base sets up to the metal material, and such design is favorable to making damped effect better.
Further, the placing plate is located on the displacement track of the clamping rod, one end, far away from the gear strip, of the clamping rod penetrates through the side face of the transfer box, and the clamping rod can clamp the placing plate through the design.
The utility model has the following beneficial effects:
1. According to the utility model, through the mutual matching among components such as the control box, the motor, the worm wheel, the gear bar and the like in the fixing device, the unmanned aerial vehicle is clamped and fixed in the transferring process of the unmanned aerial vehicle assembly, the displacement preventing effect is realized, the displacement, jolt or collision in the transporting and carrying processes can be effectively prevented, the damage risk is reduced, the unmanned aerial vehicle displacement is prevented, and the safety of operators and other personnel is ensured.
2. According to the utility model, through the mutual matching among the components such as the base, the rotating rod, the spring, the long rod, the fixed block and the like in the shock absorption device, the effects of reducing vibration and impact in the process of transporting the unmanned aerial vehicle are realized, the key systems such as complex electronic equipment, sensors and communication equipment in the unmanned aerial vehicle are effectively protected, the fuselage structure of the aircraft is protected, and the damage or the breakage in the transportation process is prevented.
Of course, it is not necessary for any one product to practice the utility model to achieve all of the advantages set forth above at the same time.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the drawings that are needed for the description of the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present utility model, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a schematic view of a three-dimensional appearance structure of the present utility model;
FIG. 2 is a schematic diagram of a three-dimensional side view of the transfer box of the present utility model;
FIG. 3 is a schematic view of an enlarged three-dimensional structure of the interior of the control box of the present utility model;
FIG. 4 is a schematic view of the three-dimensional enlarged structure of FIG. 3A according to the present utility model;
FIG. 5 is a schematic view of a three-dimensional enlarged structure of a spring according to the present utility model.
In the drawings, the list of components represented by the various numbers is as follows:
1. A transfer box; 2. placing a plate; 3. a support rod; 4. a fixing device; 41. a control box; 42. a support rod; 43. a motor; 44. a worm; 45. a rotating rod; 46. a worm wheel; 47. a round bar; 48. a gear strip; 49. a clamping rod; 410. a chute; 5. a damping device; 51. a base; 52. a connector; 53. a rotating lever; 54. a connecting rod; 55. a long rod; 56. a fixed block; 57. and (3) a spring.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-5, the utility model relates to a final assembly transfer device for an ultra-large span unmanned aerial vehicle, which comprises a transfer box 1, wherein a placing plate 2 is connected in the transfer box 1 in a sliding manner, a supporting rod 3 is fixedly connected to the side surface of the transfer box 1, a fixing device 4 is arranged on the side surface of the transfer box 1, the fixing device 4 comprises a control box 41, the side surface of the control box 41 is fixedly connected to the bottom of the supporting rod 3, a supporting rod 42 is fixedly connected to the top of the control box 41, one end, far away from the control box 41, of the supporting rod 42 is fixedly connected with a motor 43, a worm 44 is fixedly connected to an output shaft of the motor 43, a rotating rod 45 is connected to the inner wall of the control box 41 in a rotating manner, a worm wheel 46 is fixedly connected to the circumferential surface of the rotating rod 45, a round rod 47 is connected to the inner wall of the control box 41 in a rotating manner, a gear bar 48 is fixedly connected to the circumferential surface of the round rod 47, a clamping rod 49 is fixedly connected to the bottom of the gear bar 48, and a notch is formed in the top of the control box 41.
The worm 44 and the worm wheel 46 are meshed with each other, the worm 44, the worm wheel 46 and the gear bar 48 are arranged in two, and are symmetrical to each other along the vertical central axis of the control box 41, a sliding groove 410 is formed in the side face of the control box 41, the sliding groove 410 is located on the displacement track of the gear bar 48, and the design is beneficial to enabling the worm 44 to drive the worm wheel 46 to rotate.
The clamping rods 49, the supporting rods 42 and the supporting rods 3 are arranged in two, and are symmetrical to each other along the vertical central axis of the control box 41, the fixing devices 4 are arranged in two groups, and are symmetrical to each other along the vertical central axis of the transfer box 1, so that the two sides can be operated at the same time, and the two sides of the transfer box 1 can be clamped.
Be provided with damping device 5 on the inner wall of transfer box 1, damping device 5 includes base 51, the bottom fixed connection of base 51 is on the inner wall of transfer box 1, place the bottom fixedly connected with connector 52 of board 2, rotate on the inner wall of connector 52 and be connected with dwang 53, fixedly connected with connecting rod 54 on the periphery of dwang 53, the side fixedly connected with stock 55 of base 51, sliding connection has fixed block 56 on the periphery of stock 55, the one end fixed connection that the connecting rod 54 kept away from dwang 53 is at the top of fixed block 56, the side fixedly connected with spring 57 of fixed block 56, the one end fixed connection that the spring 57 kept away from fixed block 56 is on the periphery of stock 55, such design is favorable to alleviateing vibration and impact's effect.
The connector 52, the rotating rod 53, the connecting rod 54 and the fixing block 56 are arranged in two, and are mutually symmetrical along the vertical central axis of the long rod 55, and the fixing block 56 is made of metal, so that the design is beneficial to long-term use and is not easy to damage.
The base 51 is provided with two, and damping device 5 is located the bottom of placing board 2, and base 51 sets up to the metal material, and such design is favorable to making the absorbing effect better.
The placing plate 2 is located on the displacement track of the clamping rod 49, and one end of the clamping rod 49 away from the gear strip 48 penetrates through the side face of the transfer box 1, so that the clamping rod 49 can clamp the placing plate 2.
One specific application of this embodiment is: the application drives the worm 44 to rotate through the rotation of the motor 43, the worm 44 is meshed with the worm wheel 46, when the worm 44 rotates, the worm wheel 46 is driven to rotate, the worm wheel 46 is meshed with the gear strip 48, therefore, when the worm wheel 46 forwards, the gear strip 48 is driven to move, the gear strip 48 is fixedly connected with the round rod 47, the round rod 47 is connected with the inner wall of the control box 41 in a sliding way, the gear strip 48 moves left and right on the inner wall of the control box 41 through the worm wheel 46, the sliding groove 410 is positioned on the displacement track of the gear strip 48, when the gear strip 48 moves left and right, the clamping rod 49 at the bottom is driven to move, the clamping rod 49 penetrates through the side surface of the transfer box 1 and is connected with the inner wall of the transfer box 1 in a sliding way, the unmanned aerial vehicle is placed on the placing plate 2 which is connected with the inner wall of the transfer box 1 in a sliding way, the worm 44, the worm wheel 46, the gear bars 48 and the clamping rods 49 are respectively arranged at two, when the worm wheel 46 rotates from right to left, the two gear bars 48 and the clamping rods 49 are driven to move in opposite directions, a clamping effect is achieved, the two clamping rods 49 clamp the placing plate 2, then an unmanned aerial vehicle placed on the placing plate 2 is clamped, a displacement preventing effect is achieved, displacement, jolt or collision in the transportation and carrying processes is prevented, damage risks are reduced, when the unmanned aerial vehicle is stored on the placing plate 2, in case of loose clamping in the transportation process, the placing plate 2 is difficult to clamp, the placing plate 2 moves downwards, the connector 52 and the rotating rod 53 move downwards, the rotating rod 53 moves downwards, the two connecting rods 54 push the fixing blocks 56 to displace, the two fixing blocks 56 are pushed simultaneously, the spring 57 on the middle long rod 55 is pushed by the two fixing blocks 56 relatively, so that the impact force and vibration force can be reduced when the placing plate 2 is displaced downwards, the vibration and impact effects are reduced, the key systems such as complex electronic equipment, sensors and communication equipment in the middle are effectively protected, and the fuselage structure of the aircraft is protected.
In the description of the present specification, the descriptions of the terms "one embodiment," "example," "specific example," and the like, 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 present utility model. In this specification, schematic representations of the above terms do not necessarily refer to the same embodiments or examples. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The preferred embodiments of the utility model disclosed above are intended only to assist in the explanation of the utility model. The preferred embodiments are not exhaustive or to limit the utility model to the precise form disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the utility model and the practical application, to thereby enable others skilled in the art to best understand and utilize the utility model. The utility model is limited only by the claims and the full scope and equivalents thereof.
Claims (7)
1. The utility model provides an oversized span unmanned aerial vehicle assembly transfer device, includes transfer box (1), its characterized in that: the inside sliding connection of transfer case (1) has place board (2), the side fixedly connected with bracing piece (3) of transfer case (1), the side of transfer case (1) is provided with fixing device (4);
Fixing device (4) are including control box (41), the bottom of side fixed connection at bracing piece (3) of control box (41), the top fixedly connected with branch (42) of control box (41), the one end fixedly connected with motor (43) of control box (41) are kept away from to branch (42), fixedly connected with worm (44) on the output shaft of motor (43), rotate on the inner wall of control box (41) and be connected with bull stick (45), fixedly connected with worm wheel (46) on the periphery of bull stick (45), rotate on the inner wall of control box (41) and be connected with round bar (47), fixedly connected with gear bar (48) on the periphery of round bar (47), the bottom fixedly connected with clamping lever (49) of gear bar (48), the notch has been seted up at the top of control box (41).
2. The oversized span unmanned aerial vehicle assembly transfer device according to claim 1, wherein the worm (44) and the worm wheel (46) are meshed with each other, the worm (44), the worm wheel (46) and the gear strip (48) are arranged in two and are symmetrical with each other along the vertical central axis of the control box (41), a sliding groove (410) is formed in the side face of the control box (41), and the sliding groove (410) is located on the displacement track of the gear strip (48).
3. The oversized wing unmanned aerial vehicle assembly transfer device according to claim 2, wherein two clamping rods (49), supporting rods (42) and supporting rods (3) are arranged and are symmetrical to each other along the vertical central axis of the control box (41), and two groups of fixing devices (4) are arranged and are symmetrical to each other along the vertical central axis of the transfer box (1).
4. The oversized span unmanned aerial vehicle final assembly transfer device according to claim 3, wherein the damping device (5) is arranged on the inner wall of the transfer box (1), the damping device (5) comprises a base (51), the bottom of the base (51) is fixedly connected to the inner wall of the transfer box (1), the bottom of the placement plate (2) is fixedly connected with a connector (52), a rotating rod (53) is rotationally connected to the inner wall of the connector (52), a connecting rod (54) is fixedly connected to the circumferential surface of the rotating rod (53), a long rod (55) is fixedly connected to the side surface of the base (51), a fixed block (56) is slidingly connected to the circumferential surface of the long rod (55), one end of the connecting rod (54) away from the rotating rod (53) is fixedly connected to the top of the fixed block (56), a spring (57) is fixedly connected to the side surface of the fixed block (56), and one end of the spring (57) away from the fixed block (56) is fixedly connected to the circumferential surface of the long rod (55).
5. The oversized span unmanned aerial vehicle assembly transfer device of claim 4, wherein two connectors (52), rotating rods (53), connecting rods (54) and fixing blocks (56) are arranged and are symmetrical to each other along the vertical central axis of the long rod (55), and the fixing blocks (56) are made of metal.
6. The oversized span unmanned aerial vehicle assembly transfer device according to claim 5, wherein two bases (51) are arranged, the damping device (5) is arranged at the bottom of the placing plate (2), and the bases (51) are made of metal.
7. The oversized wing unmanned aerial vehicle assembly transfer device according to claim 6, wherein the placing plate (2) is located on a displacement track of a clamping rod (49), and one end of the clamping rod (49) away from the gear strip (48) penetrates through the side face of the transfer box (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323033951.2U CN221114411U (en) | 2023-11-10 | 2023-11-10 | Super-large span unmanned aerial vehicle final assembly transfer device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323033951.2U CN221114411U (en) | 2023-11-10 | 2023-11-10 | Super-large span unmanned aerial vehicle final assembly transfer device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221114411U true CN221114411U (en) | 2024-06-11 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323033951.2U Active CN221114411U (en) | 2023-11-10 | 2023-11-10 | Super-large span unmanned aerial vehicle final assembly transfer device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221114411U (en) |
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2023
- 2023-11-10 CN CN202323033951.2U patent/CN221114411U/en active Active
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