CN221294182U - Adjusting part and unmanned aerial vehicle hangar - Google Patents
Adjusting part and unmanned aerial vehicle hangar Download PDFInfo
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- CN221294182U CN221294182U CN202323359233.4U CN202323359233U CN221294182U CN 221294182 U CN221294182 U CN 221294182U CN 202323359233 U CN202323359233 U CN 202323359233U CN 221294182 U CN221294182 U CN 221294182U
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- 238000005096 rolling process Methods 0.000 claims abstract description 15
- 238000007789 sealing Methods 0.000 claims abstract description 15
- 230000003028 elevating effect Effects 0.000 claims description 20
- 230000003014 reinforcing effect Effects 0.000 claims description 10
- 230000033228 biological regulation Effects 0.000 claims description 6
- 238000009434 installation Methods 0.000 claims description 6
- 238000009423 ventilation Methods 0.000 claims description 5
- 238000010030 laminating Methods 0.000 claims description 4
- 238000003780 insertion Methods 0.000 description 6
- 230000037431 insertion Effects 0.000 description 6
- 230000000694 effects Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000011435 rock Substances 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 210000004027 cell Anatomy 0.000 description 1
- 210000005056 cell body Anatomy 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model relates to an adjusting assembly and an unmanned aerial vehicle hangar, which comprises a hangar body, wherein a double-shaft motor is started to drive an adjusting rod to rotate, a movable plate which is arranged on the surface of the adjusting rod in a threaded manner is driven to slide in a groove body, so that a push-to-angle seat is controlled to be close to or far away from each other, the unmanned aerial vehicle body is parked at the top of a lifting platform, meanwhile, the unmanned aerial vehicle body is diagonally oriented to the push-to-angle seat, the push-to-angle seat is used for moving and clamping the unmanned aerial vehicle body, a rolling column which is pushed to the inside of the angle seat is attached to the surface of the unmanned aerial vehicle body, the rolling group rotates to reduce friction force, the two push-to-angle seats are used for clamping and fixing the unmanned aerial vehicle body, the lifting platform is lowered after the unmanned aerial vehicle body is fixed, the unmanned aerial vehicle body is retracted into the hangar body, meanwhile, a connecting plate is driven to move upwards by pulling a pull rod handle to compress a supporting spring, an inserting block is separated from a clamping groove, and a rotating frame is rotated to one side, the inserting block is inserted into a clamping groove on one side of the hangar body, and two sealing covers can be opened.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle equipment, in particular to an adjusting component and an unmanned aerial vehicle hangar.
Background
Along with the development of unmanned aerial vehicle manufacturing technology and control technology, more and more fields have introduced unmanned aerial vehicle's application, for example highway, urban road, security protection warehouse, petroleum pipeline, inspection of coast etc. have all introduced many rotor unmanned aerial vehicle, pack unmanned aerial vehicle into the hangar in, because lack better spacing unmanned aerial vehicle, when leading to unmanned aerial vehicle hangar to remove, unmanned aerial vehicle rocks in inside and easily leads to damaging, lack to unmanned aerial vehicle better fixed effect.
An unmanned aerial vehicle hangar (application number: 202123321919.5) which is convenient for adjusting the distance between a lifting plate and the top end of a hangar main body cavity according to the size of an unmanned aerial vehicle body, is convenient for storing and charging unmanned aerial vehicle bodies with different volumes, and reduces the use limitation of the device; including hangar main part, fixing base, motor, two sets of sprockets, chain, axis of rotation, two sets of first fixed blocks, two sets of gears, two sets of racks, two sets of T type sliders, lifter plate, battery and unmanned aerial vehicle body, the inside cavity that is provided with of hangar main part, the motor passes through the fixing base to be fixed in the bottom of hangar main part cavity, the output and the one set of sprocket of motor are connected, another set of sprocket is fixed in the middle part of axis of rotation, connect through chain drive between two sets of sprockets to the axis of rotation rotates with two sets of first fixed blocks to be connected, and two sets of first fixed blocks are symmetrical respectively and are fixed in the left and right sides of hangar main part cavity bottom.
Above patent packs into the hangar with unmanned aerial vehicle in, owing to lack better spacing unmanned aerial vehicle, leads to unmanned aerial vehicle hangar when removing, and unmanned aerial vehicle rocks in inside and easily leads to damaging, lacks the better fixed effect to unmanned aerial vehicle, consequently we need provide an adjusting part and unmanned aerial vehicle hangar.
Disclosure of utility model
The utility model aims to provide an adjusting component and an unmanned aerial vehicle library, and solve the problems in the background art.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the unmanned aerial vehicle hangar comprises a hangar body, wherein a lifting table is arranged in the hangar body, two sealing covers are hinged to the top of the hangar body, a mounting mechanism for fixing the two sealing covers is arranged on the surface of the hangar body, and a lifting mechanism for adjusting the height of the lifting table is arranged in the hangar body;
The installation mechanism comprises a rotating frame, a pull rod handle, an inserting mechanism and a clamping groove, wherein the rotating frame is installed on the surface of the machine base body in a rotating mode, the pull rod handle is installed in the rotating frame in a sliding mode, the clamping groove is formed in the top of the sealing cover and one side of the machine base body, and the inserting mechanism at the bottom of the pull rod handle is matched with the clamping groove.
Preferably, the insertion mechanism comprises a connecting plate, supporting springs and an insertion block, the bottom of the pull rod handle is fixedly provided with the connecting plate, two supporting springs are clamped between the top of the connecting plate and the rotating frame body, and the insertion block at the bottom of the connecting plate is clamped with the clamping groove.
Preferably, the lifting mechanism comprises a driving motor and a threaded rod, two threaded rods are rotatably arranged in the machine base body, the driving motor is arranged at the lower end of each threaded rod, and the surface of each threaded rod is in threaded installation with the inner part of the lifting table.
Preferably, four balance bars are fixedly arranged in the machine base body, and the surfaces of the four balance bars are slidably arranged in the lifting table.
Preferably, ventilation grooves are formed in two sides of the hangar body.
Preferably, the inner parts of the two supporting springs are movably sleeved with the surface of the pull rod handle.
The utility model provides an adjusting part, includes unmanned aerial vehicle hangar, two spouts have been seted up to the inside of elevating platform, two equal slidable mounting in inside of spout has the movable plate, the bottom fixed mounting of elevating platform has the biax motor, the regulation pole is all installed at the both ends of biax motor, two it keeps away from to adjust the pole the fixed block is all rotated to the one end of biax motor is installed, two the top fixed mounting of fixed block is in the bottom of elevating platform, two the top of movable plate all runs through the top of elevating platform and installs and push away to the mechanism, the top of elevating platform is provided with the unmanned aerial vehicle body, push away to the mechanism and be used for right the unmanned aerial vehicle body promotes the centre gripping.
Preferably, the pushing mechanism comprises a pushing angle seat, a groove body and rolling columns, wherein the pushing angle seat is fixedly arranged at the top of each of the two moving plates, and the groove body for the rolling columns to rotate is formed in the pushing angle seat.
Preferably, the connecting seat rod is installed at the bottom of unmanned aerial vehicle body, connecting seat rod surface with push away to the laminating of mechanism case.
Preferably, the lifting platform further comprises a reinforcing seat, wherein the reinforcing seat is arranged on the surface of the double-shaft motor, and the top of the reinforcing seat is fixedly arranged at the bottom of the lifting platform through bolts.
Compared with the prior art, the utility model has the beneficial effects that:
According to the utility model, the double-shaft motor is started to drive the adjusting rod to rotate, the moving plate which is arranged on the surface of the adjusting rod in a threaded manner is driven to slide in the groove body, so that the push-direction angle seats are controlled to be close to or far away from each other, the unmanned aerial vehicle body is parked at the top of the lifting table, meanwhile, the diagonal direction of the unmanned aerial vehicle body faces the push-direction angle seats, the push-direction angle seats move to clamp the unmanned aerial vehicle body, the rolling columns in the push-direction angle seats are attached to the surface of the unmanned aerial vehicle body, the rolling groups rotate to reduce friction force, the two push-direction angle seats clamp and fix the unmanned aerial vehicle body, the lifting table is lowered after the unmanned aerial vehicle body is fixed, the unmanned aerial vehicle body is retracted into the unmanned aerial vehicle body, meanwhile, the connecting plate is driven to move upwards through pulling the pull rod handle, the supporting spring is compressed, the inserting block is separated from the clamping groove, the rotating frame is rotated to one side, the inserting block is inserted into the clamping groove on one side of the unmanned aerial vehicle body, and two sealing covers can be opened.
Drawings
FIG. 1 is a schematic perspective view of the structure of the present utility model;
FIG. 2 is a perspective view of the lifting mechanism of the present utility model;
FIG. 3 is a partial exploded view of the present utility model;
FIG. 4 is a perspective view of the push mechanism of the present utility model;
fig. 5 is a partial structural perspective view of the present utility model.
In the figure: 1. a hangar body; 2. a lifting table; 3. sealing cover; 4. a mounting mechanism; 41. a rotating frame; 42. a pull rod handle; 43. an insertion mechanism; 431. a connecting plate; 432. a support spring; 433. an insert block; 44. a clamping groove; 5. a lifting mechanism; 51. a drive motor; 52. a threaded rod; 6. a balance bar; 7. a ventilation groove; 8. a chute; 9. a moving plate; 10. a biaxial motor; 11. an adjusting rod; 12. a fixed block; 13. a pushing mechanism; 131. pushing the base to the corner seat; 132. a tank body; 133. a rolling column; 14. an unmanned aerial vehicle body; 15. a connecting seat rod; 16. and (5) reinforcing the seat.
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 present utility model provides a technical solution: the unmanned aerial vehicle hangar comprises a hangar body 1, wherein a lifting table 2 is arranged in the hangar body 1, two sealing covers 3 are hinged to the top of the hangar body 1, a mounting mechanism 4 for fixing the two sealing covers 3 is arranged on the surface of the hangar body 1, and a lifting mechanism 5 for adjusting the height of the lifting table 2 is arranged in the hangar body 1;
The installation mechanism 4 comprises a rotating frame 41, a pull rod handle 42, an inserting mechanism 43 and a clamping groove 44, wherein the rotating frame 41 is rotatably installed on the surface of the machine base body 1, the pull rod handle 42 is slidably installed in the rotating frame 41, the clamping groove 44 is formed in the top of the sealing cover 3 and one side of the machine base body 1, and the inserting mechanism 43 at the bottom of the pull rod handle 42 is matched with the clamping groove 44.
The inserting mechanism 43 comprises a connecting plate 431, supporting springs 432 and an inserting block 433, the bottom of the pull rod handle 42 is fixedly provided with the connecting plate 431, two supporting springs 432 are clamped between the top of the connecting plate 431 and the rotating frame 41, and the inserting block at the bottom of the connecting plate 431 is clamped with the clamping groove 44;
In this embodiment, the connecting plate 431 is driven to move upwards by pulling the pull rod handle 42, the supporting spring 432 is compressed, the insertion block is separated from the clamping groove 44, the rotating frame 41 is rotated to one side, the insertion block is inserted into the clamping groove 44 on one side of the machine base body 1, the two sealing covers 3 can be opened, the above-mentioned movement process moves reversely, and the two sealing covers 3 are limited and fixed, so that the sealing of the machine base body 1 is completed.
The lifting mechanism 5 comprises a driving motor 51 and a threaded rod 52, two threaded rods 52 are rotatably arranged in the machine base body 1, the driving motor 51 is arranged at the lower end of the threaded rod 52, and the surface of the threaded rod 52 is in threaded installation with the interior of the lifting table 2;
Specifically, the two driving motors 51 are synchronous motors, and the driving motors 51 are started to drive the output end threaded rod 52 to rotate, so that the height adjustment of the lifting platform 2 is controlled.
Four balance bars 6 are fixedly arranged in the machine base body 1, and the surfaces of the four balance bars 6 are slidably arranged in the lifting table 2;
It should be noted that, four balance bars 6 are disposed in the hangar body 1, and the height adjustment movement by the lifting platform 2 has better stability.
In order to achieve a certain ventilation and heat dissipation effect in the hangar body 1, ventilation grooves 7 are formed in two sides of the hangar body 1.
In order to avoid bending of the supporting springs 432 in the deformation process and the supporting springs 432 cannot be used, the inner parts of the two supporting springs 432 are movably sleeved with the surface of the pull rod handle 42.
The utility model provides an adjusting part, including unmanned aerial vehicle hangar, two spouts 8 have been seted up to the inside of elevating platform 2, the equal slidable mounting in inside of two spouts 8 has movable plate 9, the bottom fixed mounting of elevating platform 2 has biax motor 10, regulation pole 11 is all installed at biax motor 10's both ends, two regulation poles 11 are kept away from biax motor 10's one end and are all rotated and install fixed block 12, the top fixed mounting of two fixed blocks 12 is in the bottom of elevating platform 2, the top of two movable plate 9 all runs through elevating platform 2's top and installs push away to mechanism 13, elevating platform 2's top is provided with unmanned aerial vehicle body 14, push away to mechanism 13 is used for promoting the centre gripping to unmanned aerial vehicle body 14.
The pushing mechanism 13 comprises a pushing angle seat 131, a groove body 132 and a rolling column 133, wherein the pushing angle seat 131 is fixedly arranged at the top of each of the two moving plates 9, and the groove body 132 for the rolling column 133 to rotate is formed in the pushing angle seat 131;
Further, start biax motor 10 drives and adjusts pole 11 rotation, drive and adjust pole 11 surface screw-thread mounted's movable plate 9 and slide in cell body 132, thereby control pushes away to angle seat 131 and is close to each other or keep away from each other, park unmanned aerial vehicle body 14 at elevating platform 2 top, unmanned aerial vehicle body 14 diagonal orientation pushes away to angle seat 131 simultaneously, push away to angle seat 131 and remove centre gripping unmanned aerial vehicle body 14, it pushes away to the inside rolling post 133 of angle seat 131 and unmanned aerial vehicle body 14 surface laminating, the rolling group rotates and reduces frictional force, two push away to angle seat 131 and carry out centre gripping to unmanned aerial vehicle body 14 fixedly.
In order to facilitate the guiding clamping of the pushing mechanism 13 to the unmanned aerial vehicle body 14, the connecting seat rod 15 at the bottom of the unmanned aerial vehicle body 14 is convenient to push the clamping of the pushing mechanism 13, the connecting seat rod 15 is installed at the bottom of the unmanned aerial vehicle body 14, and the surface of the connecting seat rod 15 is attached to the pushing mechanism 13.
In order to fix the double-shaft motor 10 more firmly, the lifting platform further comprises a reinforcing seat 16, wherein the reinforcing seat 16 is arranged on the surface of the double-shaft motor 10, and the top of the reinforcing seat 16 is fixedly arranged at the bottom of the lifting platform 2 through bolts.
This device starts driving motor 51 and drives output threaded rod 52 rotation to control elevating platform 2 rise, fall unmanned aerial vehicle body 14 at elevating platform 2 top, the corner subtend pushes away to angle seat 131 in when unmanned aerial vehicle body 14 parks, start biax motor 10 and drive regulation pole 11 rotation, drive regulation pole 11 surface screw-mounting's movable plate 9 and slide in cell 132, thereby control push away to angle seat 131 each other and be close to or keep away from each other, park unmanned aerial vehicle body 14 at elevating platform 2 top, unmanned aerial vehicle body 14 diagonal orientation pushes away to angle seat 131 simultaneously, push away to angle seat 131 and remove centre gripping unmanned aerial vehicle body 14, it pushes away to the inside rolling column 133 of angle seat 131 and unmanned aerial vehicle body 14 surface laminating, rolling group rotates and reduces frictional force, two push away to angle seat 131 carry out the centre gripping to unmanned aerial vehicle body 14 fixedly, unmanned aerial vehicle body 14 back will elevating platform 2 decline, unmanned aerial vehicle body 14 is interior, simultaneously drive connecting plate 431 through pulling pull rod handle 42 and move upwards, compress supporting spring 432, make the insert the piece and break away from draw-in groove 44, and rotate frame 41 to one side, insert the piece and insert two sealed lid 1 side, two seal up joint plate 1, two seal 3, two seal up seal 1, and 3.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (10)
1. The utility model provides an unmanned aerial vehicle hangar, includes hangar body (1), its characterized in that: the automatic lifting device is characterized in that a lifting table (2) is arranged inside the machine base body (1), two sealing covers (3) are hinged to the top of the machine base body (1), a mounting mechanism (4) used for fixing the two sealing covers (3) is arranged on the surface of the machine base body (1), and a lifting mechanism (5) used for adjusting the height of the lifting table (2) is arranged inside the machine base body (1);
The installation mechanism (4) comprises a rotating frame (41), a pull rod handle (42), an inserting mechanism (43) and a clamping groove (44), wherein the rotating frame (41) is installed on the surface of the machine base body (1) in a rotating mode, the pull rod handle (42) is installed in the rotating frame (41) in a sliding mode, the clamping groove (44) is formed in the top of the sealing cover (3) and one side of the machine base body (1), and the bottom inserting mechanism (43) of the pull rod handle (42) is matched with the clamping groove (44).
2. A drone hangar according to claim 1, wherein: the inserting mechanism (43) comprises a connecting plate (431), supporting springs (432) and an inserting block (433), the connecting plate (431) is fixedly arranged at the bottom of the pull rod handle (42), two supporting springs (432) are clamped between the top of the connecting plate (431) and the rotating frame (41), and the inserting block at the bottom of the connecting plate (431) is clamped with the clamping groove (44).
3. A drone hangar according to claim 1, wherein: the lifting mechanism (5) comprises a driving motor (51) and a threaded rod (52), two threaded rods (52) are rotatably arranged in the machine base body (1), the driving motor (51) is arranged at the lower end of each threaded rod (52), and the surface of each threaded rod (52) is in threaded installation with the inner part of the lifting table (2).
4. A drone hangar according to claim 3, wherein: four balance bars (6) are fixedly arranged in the machine base body (1), and the surfaces of the four balance bars (6) are slidably arranged in the lifting table (2).
5. A drone hangar according to claim 1, wherein: ventilation grooves (7) are formed in two sides of the hangar body (1).
6. A drone hangar according to claim 2, wherein: the inner parts of the two supporting springs (432) are movably sleeved with the surface of the pull rod handle (42).
7. An adjustment assembly, characterized by: including the unmanned aerial vehicle hangar of any one of claims 1-6, two spouts (8) have been seted up to the inside of elevating platform (2), two equal slidable mounting in inside of spout (8) has movable plate (9), the bottom fixed mounting of elevating platform (2) has biax motor (10), regulation pole (11) are all installed at the both ends of biax motor (10), two adjust pole (11) keep away from the one end of biax motor (10) is all rotated and is installed fixed block (12), two the top fixed mounting of fixed block (12) is in the bottom of elevating platform (2), two the top of movable plate (9) is all run through the top of elevating platform (2) and install push mechanism (13), the top of elevating platform (2) is provided with unmanned aerial vehicle body (14), push mechanism (13) are used for right unmanned aerial vehicle body (14) promotes the centre gripping.
8. An adjustment assembly as set forth in claim 7, wherein: the pushing mechanism (13) comprises a pushing angle seat (131), a groove body (132) and a rolling column (133), wherein the pushing angle seat (131) is fixedly arranged at the top of each moving plate (9), and the groove body (132) used for the rolling column (133) to rotate is formed in the pushing angle seat (131).
9. An adjustment assembly as set forth in claim 7, wherein: the bottom of unmanned aerial vehicle body (14) is installed connecting seat pole (15), connecting seat pole (15) surface with push away to mechanism (13) case laminating.
10. An adjustment assembly as set forth in claim 7, wherein: the lifting platform further comprises a reinforcing seat (16), wherein the reinforcing seat (16) is arranged on the surface of the double-shaft motor (10), and the top of the reinforcing seat (16) is fixedly arranged at the bottom of the lifting platform (2) through bolts.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323359233.4U CN221294182U (en) | 2023-12-11 | 2023-12-11 | Adjusting part and unmanned aerial vehicle hangar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323359233.4U CN221294182U (en) | 2023-12-11 | 2023-12-11 | Adjusting part and unmanned aerial vehicle hangar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221294182U true CN221294182U (en) | 2024-07-09 |
Family
ID=91743189
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323359233.4U Active CN221294182U (en) | 2023-12-11 | 2023-12-11 | Adjusting part and unmanned aerial vehicle hangar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221294182U (en) |
-
2023
- 2023-12-11 CN CN202323359233.4U patent/CN221294182U/en active Active
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