CN213473529U - Unmanned aerial vehicle cargo hold - Google Patents

Unmanned aerial vehicle cargo hold Download PDF

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Publication number
CN213473529U
CN213473529U CN202022138971.6U CN202022138971U CN213473529U CN 213473529 U CN213473529 U CN 213473529U CN 202022138971 U CN202022138971 U CN 202022138971U CN 213473529 U CN213473529 U CN 213473529U
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CN
China
Prior art keywords
aerial vehicle
unmanned aerial
threaded rod
groove
fixture block
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CN202022138971.6U
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Chinese (zh)
Inventor
陆东明
张金宝
郑超
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Anhui Zhitian Intelligent Technology Co Ltd
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Anhui Zhitian Intelligent Technology Co Ltd
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Priority to CN202022138971.6U priority Critical patent/CN213473529U/en
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Publication of CN213473529U publication Critical patent/CN213473529U/en
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Abstract

The utility model discloses an unmanned aerial vehicle cargo hold, including the cabin body, connecting plate and fixed block, cabin body front end has the hatch door through hinge swing joint, and hatch door upper end swing joint has electric telescopic handle, electric telescopic handle upper end and cabin internal wall swing joint, cabin body upside is equipped with the drive case, and drive case upper end is equipped with the connecting plate, and drives the incasement and be equipped with the threaded rod, and the threaded rod runs through both ends about the drive case. The utility model discloses during the use, through locking bolt with connecting plate and unmanned aerial vehicle fixed connection, starter motor drives pivot, bevel gear two, bevel gear and threaded rod and rotates, and the threaded rod drives slider one and the motion is kept away from each other to the fixture block, and when the fixture block got into the draw-in groove, the fixture block promoted baffle, limiting plate downstream, when the one end that the fixture block is close to each other left the baffle upper end, made fixture block and fixed block joint, the baffle upward movement under the effect that the spring resets to it is spacing to carry out the fixture block.

Description

Unmanned aerial vehicle cargo hold
Technical Field
The utility model relates to an unmanned aerial vehicle accessory technical field specifically is an unmanned aerial vehicle cargo hold.
Background
A drone is an unmanned aircraft that is operated with a radio remote control device and self-contained program control, or is operated autonomously, either completely or intermittently, by an onboard computer.
Unmanned aerial vehicle is equipped with the unmanned aerial vehicle cargo hold usually in the use, and present traditional unmanned aerial vehicle cargo hold often is fixed mounting on unmanned aerial vehicle, and it is inconvenient to dismantle, and wastes time and energy. Therefore, the utility model provides an unmanned aerial vehicle cargo hold to solve the above-mentioned problem that proposes.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle cargo hold to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme:
an unmanned aerial vehicle cargo hold comprises a cabin body, a connecting plate and a fixed block, wherein the front end of the cabin body is movably connected with a cabin door through a hinge, the upper end of the cabin door is movably connected with an electric telescopic rod, the upper end of the electric telescopic rod is movably connected with the inner wall of the cabin body, a driving box is arranged on the upper side of the cabin body, the connecting plate is arranged on the upper end of the driving box, a threaded rod is arranged in the driving box and penetrates through the left end and the right end of the driving box, first sliding blocks are symmetrically arranged on the threaded rod by taking the driving box as the center, a clamping block is arranged at the lower end of each sliding block, the fixed blocks are symmetrically arranged on the upper end of the cabin body in a clamping way, a groove is arranged at the upper end of each fixed block and corresponds to the, the lower end of the fixed pulley is fixedly connected with the bottom end of the groove, the right end of the rope penetrates through the through groove, and the right end of the rope is provided with a pull block.
As a further scheme of the utility model, the four corners is equipped with the bolt hole on the connecting plate, the right locking bolt of bolt hole female connection.
As the utility model discloses scheme further again, be equipped with bevel gear one on the threaded rod, bevel gear one goes up meshing right bevel gear two, and two lower extremes of bevel gear are equipped with the pivot, and the pivot lower extreme is equipped with the motor, motor lower extreme and the bottom end fixed connection of driving box.
As the utility model discloses scheme further again, both ends all are equipped with the slide bar about the motor, and the one end that the slide bar was kept away from each other all runs through drive box and slider one, and slide bar and a slider sliding connection.
As the utility model discloses scheme further again, both ends all are equipped with slider two about the limiting plate, and both ends correspond slider two and are equipped with the spout, limiting plate and recess sliding connection about the recess.
As the utility model discloses further scheme again, the limiting plate lower extreme is equipped with the spring, spring lower extreme and recess bottom end fixed connection.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model discloses during the use, through locking bolt with connecting plate and unmanned aerial vehicle fixed connection, starter motor drives pivot, bevel gear two, bevel gear and threaded rod and rotates, and the threaded rod drives slider one and the motion is kept away from each other to the fixture block, and when the fixture block got into the draw-in groove, the fixture block promoted baffle, limiting plate downstream, when the one end that the fixture block is close to each other left the baffle upper end, made fixture block and fixed block joint, the baffle upward movement under the effect that the spring resets to it is spacing to carry out the fixture block.
2. The utility model discloses during the use, when the cabin body needs to be dismantled, keep away from the pulling each other and draw the piece, draw the piece to drive the rope motion, the rope drives limiting plate and baffle downstream, the reverse function of restart motor can, easy to assemble and dismantlement start electric telescopic handle simultaneously and can open the hatch door from the top down, the convenience is to internal transportation goods in cabin, easy operation, labour saving and time saving.
Drawings
Fig. 1 is a schematic structural diagram of a cargo hold of an unmanned aerial vehicle.
Fig. 2 is a schematic diagram of the internal structure of a driving box in a cargo hold of an unmanned aerial vehicle.
Fig. 3 is an enlarged schematic structure diagram of a position A in a cargo hold of an unmanned aerial vehicle.
In the figure: 1. a cabin body; 2. a hinge; 3. a cabin door; 4. an electric telescopic rod; 5. a slide bar; 6. a first sliding block; 7. a threaded rod; 8. a drive box; 9. a connecting plate; 10. locking the bolt; 11. a clamping block; 12. a first bevel gear; 13. a second bevel gear; 14. a rotating shaft; 15. a motor; 16. a fixed block; 17. a card slot; 18. a groove; 19. a through groove; 20. a baffle plate; 21. a limiting plate; 22. a spring; 23. a second sliding block; 24. a chute; 25. a fixed pulley; 26. a rope; 27. and (5) pulling the block.
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.
Referring to fig. 1 to 3, in the embodiment of the present invention, an unmanned aerial vehicle cargo compartment includes a cabin body 1, a connecting plate 9 and a fixing block 16, wherein a cabin door 3 is movably connected to the front end of the cabin body 1 through a hinge 2, an electric telescopic rod 4 is movably connected to the upper end of the cabin door 3, the upper end of the electric telescopic rod 4 is movably connected to the inner wall of the cabin body 1, a driving box 8 is disposed on the upper side of the cabin body 1, the connecting plate 9 is disposed on the upper end of the driving box 8, bolt holes are disposed at four corners of the connecting plate 9, right locking bolts 10 are threadedly connected to the bolt holes, a threaded rod 7 is disposed in the driving box 8, the threaded rod 7 penetrates through the left and right ends of the driving box 8, a bevel gear 12 is disposed on the threaded rod 7, a right bevel gear 13 is engaged on the bevel gear 12, a rotating shaft 14 is disposed, the end, far away from each other, of each sliding rod 5 penetrates through the driving box 8 and the first sliding block 6, the sliding rods 5 are connected with the first sliding blocks 6 in a sliding manner, the first sliding blocks 6 are symmetrically arranged on the threaded rod 7 by taking the driving box 8 as a center, the lower ends of the first sliding blocks 6 are provided with the clamping blocks 11, the upper end of the cabin body 1 is symmetrically provided with the fixed blocks 16 at left and right sides, the end, close to each other, of each fixed block 16 is provided with a clamping groove 17 corresponding to the corresponding clamping block 11, the upper end of the fixed block 16 is provided with a groove rail corresponding to the first sliding block 6, the lower end of the clamping groove 17 is provided with a groove 18, the right end of the groove 18 is provided with a through groove 19, a baffle 20 is arranged in the groove 18, the lower end of the baffle 20 is provided with a limiting plate 21, the left and right ends of the limiting plate 21 are, a fixed pulley 25 is arranged on the rope 26, the lower end of the fixed pulley 25 is fixedly connected with the bottom end of the groove 18, the right end of the rope 26 penetrates through the through groove 19, and a pulling block 27 is arranged at the right end of the rope 26.
The utility model discloses a theory of operation is:
when the utility model is used, the connecting plate 9 is fixedly connected with the unmanned aerial vehicle through the locking bolt 10, the starting motor 15 drives the rotating shaft 14, the bevel gear 13, the bevel gear 12 and the threaded rod 7 to rotate, the threaded rod 7 drives the slider 6 and the fixture block 11 to move away from each other, when the fixture block 11 enters the clamping groove 17, the fixture block 11 pushes the baffle 20 and the limiting plate 21 to move downwards, when the end, which is close to each other, of the fixture block 11 leaves the upper end of the baffle 20, the fixture block 11 is clamped with the fixing block 16, the baffle 20 moves upwards under the reset action of the spring 22, thereby limiting the fixture block 11, when the cabin body 1 needs to be disassembled, the pulling block 27 is away from each other, the pulling block 27 drives the rope 26 to move, the rope 26 drives the limiting plate 21 and the baffle 20 to move downwards, the restarting motor 15 operates reversely, the installation and disassembly are convenient, the cabin door, the goods are conveniently transported in the cabin body 1, the operation is simple, and the time and the labor are saved.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims (6)

1. The unmanned aerial vehicle cargo compartment comprises a compartment body (1), a connecting plate (9) and a fixing block (16), and is characterized in that the front end of the compartment body (1) is movably connected with a compartment door (3) through a hinge (2), the upper end of the compartment door (3) is movably connected with an electric telescopic rod (4), the upper end of the electric telescopic rod (4) is movably connected with the inner wall of the compartment body (1), a driving box (8) is arranged on the upper side of the compartment body (1), the connecting plate (9) is arranged on the upper end of the driving box (8), a threaded rod (7) is arranged in the driving box (8), the threaded rod (7) penetrates through the left end and the right end of the driving box (8), first sliding blocks (6) are symmetrically arranged on the driving box (8) as the center, clamping blocks (11) are arranged at the lower ends of the first sliding blocks (6), the fixing blocks (16) are symmetrically arranged on the left end, fixed block (16) upper end corresponds slider one (6) and is equipped with the groove rail, and draw-in groove (17) lower extreme is equipped with recess (18), and recess (18) right-hand member is equipped with logical groove (19), be equipped with baffle (20) in recess (18), baffle (20) lower extreme is equipped with limiting plate (21), limiting plate (21) lower extreme is equipped with rope (26), is equipped with fixed pulley (25) on rope (26), and fixed pulley (25) lower extreme and recess (18) bottom fixed connection, and rope (26) right-hand member runs through logical groove (19), and rope (26) right-hand member is equipped with and draws piece (27).
2. The unmanned aerial vehicle cargo hold of claim 1, wherein bolt holes are formed in four corners of the connecting plate (9), and a right locking bolt (10) is connected in the bolt holes in a threaded mode.
3. The cargo compartment of the unmanned aerial vehicle as claimed in claim 1, wherein the threaded rod (7) is provided with a first bevel gear (12), the first bevel gear (12) is meshed with a second right bevel gear (13), the lower end of the second bevel gear (13) is provided with a rotating shaft (14), the lower end of the rotating shaft (14) is provided with a motor (15), and the lower end of the motor (15) is fixedly connected with the bottom end of the driving box (8).
4. The unmanned aerial vehicle cargo hold of claim 3, wherein both ends about motor (15) are equipped with slide bar (5), and the one end that slide bar (5) kept away from each other all runs through drive box (8) and slider (6), and slide bar (5) and slider (6) sliding connection.
5. The unmanned aerial vehicle cargo hold of claim 1, wherein the left and right ends of the limiting plate (21) are provided with a second sliding block (23), the left and right ends of the groove (18) are provided with sliding grooves (24) corresponding to the second sliding block (23), and the limiting plate (21) is slidably connected with the groove (18).
6. An unmanned aerial vehicle cargo compartment according to claim 1 or 5, wherein the lower end of the limiting plate (21) is provided with a spring (22), and the lower end of the spring (22) is fixedly connected with the bottom end of the groove (18).
CN202022138971.6U 2020-09-25 2020-09-25 Unmanned aerial vehicle cargo hold Active CN213473529U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202022138971.6U CN213473529U (en) 2020-09-25 2020-09-25 Unmanned aerial vehicle cargo hold

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202022138971.6U CN213473529U (en) 2020-09-25 2020-09-25 Unmanned aerial vehicle cargo hold

Publications (1)

Publication Number Publication Date
CN213473529U true CN213473529U (en) 2021-06-18

Family

ID=76362955

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202022138971.6U Active CN213473529U (en) 2020-09-25 2020-09-25 Unmanned aerial vehicle cargo hold

Country Status (1)

Country Link
CN (1) CN213473529U (en)

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