CN212829120U - Quick assembly disassembly light weight modularization increases steady cloud platform mechanism - Google Patents
Quick assembly disassembly light weight modularization increases steady cloud platform mechanism Download PDFInfo
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- CN212829120U CN212829120U CN202022003603.0U CN202022003603U CN212829120U CN 212829120 U CN212829120 U CN 212829120U CN 202022003603 U CN202022003603 U CN 202022003603U CN 212829120 U CN212829120 U CN 212829120U
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Abstract
The utility model discloses a quick assembly disassembly light weight modularization increases steady cloud platform mechanism, include shock attenuation module and increase steady cloud platform main part, the spacing portion of one side fixedly connected with fixed subassembly of shock attenuation module lower surface, the fixed subassembly locking portion of opposite side fixedly connected with of shock attenuation module lower surface, increase one side fixedly connected with moving assembly location portion of steady cloud platform main part upper surface, increase the opposite side fixedly connected with moving assembly direction slider of steady cloud platform main part upper surface. This quick assembly disassembly light weight modularization increases steady cloud platform mechanism, through the spacing portion of fixed subassembly, fixed subassembly locking portion, remove subassembly location portion, remove the cooperation setting between subassembly guide slide and the fitting pin jack, can install shock-absorbing module and unmanned aerial vehicle, through removing subassembly location portion, remove subassembly guide slide and increase steady cloud platform main part wholly for the spacing portion of fixed subassembly and fixed subassembly locking portion along predetermineeing the installation direction and remove.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle carries cloud platform technical field, specifically is a quick assembly disassembly light weight modularization increases steady cloud platform mechanism.
Background
With the development of science and technology, the unmanned aerial vehicle technology is mature day by day and is widely applied to monitoring, surveying and mapping, photography and other fields, the successful application of the unmanned aerial vehicle technology has close relation with various mounting devices on an unmanned aerial vehicle, a tripod head is taken as one of the unmanned aerial vehicle mounting devices and is widely applied, generally, a camera and other loads are installed on the tripod head, the tripod head is connected with the unmanned aerial vehicle, the unmanned aerial vehicle obtains specific types of environmental information such as images and the like through the mounting devices when executing tasks, most of the existing tripod head devices are screwed on the unmanned aerial vehicle in a screw connection mode, the tripod head and the unmanned aerial vehicle are separated in the transportation process, the tripod head is installed on the unmanned aerial vehicle after arriving at a specified task site, the flight task can be executed after the installation is completed, the currently adopted screw installation mode needs more time, and the installation and the disassembly are not convenient, the unmanned aerial vehicle can not quickly execute flight tasks, the existing cloud deck is mostly in a single task load mounting mode, the requirement that multiple loads are required to be exchanged for mounting in certain specific operation occasions cannot be met, even if multiple loads can be mounted, the cloud deck state also needs to be readjusted when another type of task load is replaced after one type of task load mounting is finished, the replacement of the loads is long in time, the installation and the disassembly are inconvenient, and the unmanned aerial vehicle is influenced to quickly execute the flight tasks.
The device comprises an upper fixing piece which can be fixed on the unmanned aerial vehicle, a lower fixing piece which can be fixed on the tripod head, and a positioning structure, a locking component and a plurality of groups of clamping structures which are arranged between the upper fixing piece and the lower fixing piece, wherein the clamping structures comprise clamping hooks and clamping holes, the locking component is provided with a telescopic locking part, the clamping hooks of the locking component and the clamping structures are arranged on the upper fixing piece, a jack which is matched with the locking component and the clamping holes of the clamping structures are arranged on the lower fixing piece, when in installation, the lower fixing piece is moved along a preset installation direction to ensure that all the clamping structures are clamped in place, the locking part of the locking component which is positioned on the upper fixing piece is automatically unlocked and inserted into the jack of the lower fixing piece, accomplish the locking, when dismantling, exert external force, make locking Assembly's locking portion slide to the position of relieving locking, make lower mounting remove toward the opposite direction of predetermineeing the installation direction for last mounting again, make all joint structures relieve the block and connect, thereby the dismantlement of mounting under the completion, this technical scheme is compared with the screw connection mode commonly used, need not adopt any instrument, simple to operate has been many, but this kind of scheme structure is comparatively complicated, card hole and the unsafe phenomenon of pothook butt joint can appear in multiunit joint structure, and do not have corresponding pretension structure, there is the fit clearance between mounting and last mounting under leading to easily, the not hard up phenomenon appears, and the structure complicacy can make the whole weight of cloud platform increase, influence unmanned aerial vehicle's flight performance.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Not enough to prior art, the utility model provides a quick assembly disassembly light weight modularization increases steady cloud platform mechanism has solved the problem that proposes in the above-mentioned background art.
(II) technical scheme
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: the utility model provides a quick assembly disassembly light weight modularization increases steady cloud platform mechanism, includes shock-absorbing module and increases steady cloud platform main part, the spacing portion of one side fixedly connected with fixed subassembly of shock-absorbing module lower surface, the opposite side fixedly connected with fixed subassembly locking portion of shock-absorbing module lower surface, increase one side fixedly connected with removal subassembly location portion of steady cloud platform main part upper surface, the opposite side fixedly connected with removal subassembly guide slide block of steady cloud platform main part upper surface, the fitting pin jack has been seted up on the surface of removal subassembly guide slide block, one side of increasing steady cloud platform main part is provided with the installation stopper, the installation spout has been seted up on the surface of installation stopper, the inner wall sliding connection of installation spout has the load installing frame, the prefabricated hole has been seted up on the surface of load installing.
Optionally, the fixed assembly limiting part comprises a first electrical connector, a positioning seat, a prefabricated ejecting bead and a positioning pin hole, the first electrical connector is arranged on one side of the fixed assembly limiting part, the positioning seats are arranged at two ends of the fixed assembly limiting part, the prefabricated ejecting bead is movably connected to the inner wall of the positioning seat, the positioning pin hole is formed in the surface of the positioning seat, the moving assembly positioning part comprises a positioning pin and a second electrical connector, the second electrical connector is arranged on one side of the moving assembly positioning part, and the positioning pins are fixedly connected to two ends of the moving assembly positioning part.
Optionally, the surface of the positioning pin is movably connected with the inner wall of the positioning pin hole, and the surface of the first electrical connector is movably connected with the inner wall of the second electrical connector.
Optionally, the fixing component locking portion comprises an L-shaped locking pin and a guide sliding groove, the two ends of the fixing component locking portion are provided with the L-shaped locking pin, and the surface of the fixing component locking portion is provided with the guide sliding groove.
Optionally, the surface of the L-shaped locking pin is movably connected with the inner wall of the locking pin insertion hole.
(III) advantageous effects
The utility model provides a quick assembly disassembly light weight modularization increases steady cloud platform mechanism possesses following beneficial effect:
1. the rapid dismounting light-weight modularized stability-increasing tripod head mechanism can install the damping module and the unmanned aerial vehicle through the matching arrangement between the fixed component limiting part, the fixed component locking part, the moving component positioning part, the moving component guide slide block and the locking pin jack, and can complete the locking after reaching the limiting position by moving the moving component positioning part, the moving component guide slide block and the stability-increasing tripod head main body along the preset installation direction relative to the fixed component limiting part and the fixed component locking part, the scheme has short time, does not need any matched tool in the installation process, has simple operation, solves the problems of long time and inconvenient operation when the current stability-increasing tripod head main body is installed and connected by using screws, and has the functions of guiding, positioning and locking, and the locating pin hole and the prefabricated top pearl that set up on the positioning seat in the fixed subassembly spacing part, can prevent the spacing part of fixed subassembly, fixed subassembly locking portion, it is not hard up to appear after removal subassembly location portion and the butt joint of removal subassembly guide slide block, cloud platform installation reliability has been improved, the unreliable problem of installation that has existing quick assembly disassembly structure at present has been solved, cooperation through between first electrical connector and the second electrical connector sets up, can realize the quick opposite plug of connector when the installation, still need the inconvenience of plug wiring mouth again after having avoided quick assembly disassembly structure to pull down.
2. This quick assembly disassembly light weight module increases steady cloud platform mechanism, through increasing steady cloud platform main part, installation stopper, installation spout, load installing frame and the cooperation setting between the prefabricated hole, can install task load through the prefabricated hole that load installing frame surface set up, can satisfy task load and exchange fast, satisfy multiple task load and exchange, satisfied unmanned aerial vehicle quick assembly disassembly's demand when multiple load is task in turn.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the main structure of the stability-increasing cradle head of the present invention;
FIG. 3 is a schematic structural view of the damping module of the present invention;
FIG. 4 is a schematic view of the locking portion of the fixing assembly of the present invention;
FIG. 5 is a schematic view of the structure of the position-limiting portion of the fixing component of the present invention;
FIG. 6 is a schematic view of the positioning portion of the movable assembly of the present invention;
fig. 7 is the schematic view of the structure of the guiding sliding block of the moving assembly of the present invention.
In the figure: 1. a shock-absorbing module; 2. a stability augmentation holder main body; 3. a fixed component limiting part; 301. a first electrical connector; 302. positioning seats; 303. prefabricating a top bead; 304. a positioning pin hole; 4. a fixed assembly locking portion; 401. an L-shaped locking pin; 402. a guide chute; 5. a moving assembly positioning part; 501. positioning pins; 502. a second electrical connector; 6. a moving assembly guide slide block; 7. a locking pin jack; 8. installing a limiting block; 9. installing a chute; 10. a load mounting frame; 11. and (6) hole prefabrication.
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.
Referring to fig. 1 to 7, the present invention provides a technical solution: a quick-dismounting light-weight modular stability-increasing tripod head mechanism comprises a damping module 1 and a stability-increasing tripod head main body 2, wherein one side of the lower surface of the damping module 1 is fixedly connected with a fixed component limiting part 3;
in order to solve the problems of long time and inconvenient operation when the prior stability augmentation tripod head main body 2 is installed and connected by using screws, the utility model is characterized in that a fixed component locking part 4 is fixedly connected to the other side of the lower surface of a damping module 1, a moving component positioning part 5 is fixedly connected to one side of the upper surface of the stability augmentation tripod head main body 2, a moving component guide slide block 6 is fixedly connected to the other side of the upper surface of the stability augmentation tripod head main body 2, a locking pin jack 7 is arranged on the surface of the moving component guide slide block 6, the damping module 1 and an unmanned aerial vehicle can be installed by the matching arrangement between the fixed component limiting part 3, the fixed component locking part 4, the moving component positioning part 5, the moving component guide slide block 6 and the locking pin jack 7, the whole stability augmentation tripod head main body 2 moves along the preset installation direction relative to the fixed component limiting part 3 and the fixed component locking part 4, the locking is completed after the position is limited, the scheme is short in time consumption, no matched tool is needed in the installation process, the operation is simple, and the problems that the existing stability-increasing tripod head main body 2 is long in time consumption and inconvenient to operate when being connected through a screw in the installation process are solved;
in order to facilitate the rapid disassembly and assembly of the utility model when multi-load alternate tasks, an installation limiting block 8 is arranged on one side of the stability-increasing cradle head main body 2, an installation chute 9 is arranged on the surface of the installation limiting block 8, the inner wall of the installation chute 9 is connected with a load installation frame 10 in a sliding way, a prefabricated hole 11 is arranged on the surface of the load installation frame 10, the task load can be rapidly exchanged through the matching arrangement of the stability-increasing cradle head main body 2, the installation limiting block 8, the installation chute 9, the load installation frame 10 and the prefabricated hole 11 arranged on the surface of the load installation frame 10, the requirement of rapid disassembly and assembly of the unmanned aerial vehicle when multi-load alternate tasks is met, the fixing component limiting part 3 comprises a first electrical connector 301, a positioning seat 302, a prefabricated top bead 303 and a positioning pin hole 304, one side of the fixed component limiting part 3 is provided with a first electrical connector 301, two ends of the fixed component limiting part 3 are both provided with positioning seats 302, the inner wall of each positioning seat 302 is movably connected with a prefabricated ejector bead 303, the surface of each positioning seat 302 is provided with a positioning pin hole 304, the movable component positioning part 5 comprises a positioning pin 501 and a second electrical connector 502, one side of the movable component positioning part 5 is provided with the second electrical connector 502, through the matching arrangement between the first electrical connector 301 and the second electrical connector 502, the rapid opposite insertion of the connectors can be realized during the installation, the inconvenience that the wiring port needs to be inserted and pulled after the rapid disassembly structure is disassembled is avoided, two ends of the movable component positioning part 5 are both fixedly connected with the positioning pins 501, the surface of each positioning pin 501 is movably connected with the inner wall of the positioning pin hole 304, the surface of the first electrical connector 301 is movably connected with the inner, fixed subassembly locking portion 4 includes L type fitting pin 401 and direction spout 402, and the both ends of fixed subassembly locking portion 4 all are provided with L type fitting pin 401, and the surface of fixed subassembly locking portion 4 is provided with direction spout 402, the surface of L type fitting pin 401 and the inner wall swing joint of fitting pin jack 7.
To sum up, this quick assembly disassembly light weight modularization increases steady cloud platform mechanism, the use step is as follows:
1. the device connects a fixed component limiting part 3 and a fixed component locking part 4 on a damping module 1, and connects a moving component positioning part 5 and a moving component guide slide block 6 on a stability augmentation holder main body 2;
2. the device can be used for plugging a positioning pin hole 304 formed in the limiting part 3 of the fixing component with a positioning pin 501 arranged on the surface of the positioning part 5 of the moving component, the prefabricated top bead 303 is arranged at the top end of the positioning pin hole 304 by utilizing threads, and the locking effect is achieved after the positioning pin 501 is inserted into the positioning pin hole 304;
3. the unmanned aerial vehicle comprises a damping module 1, a fixing component limiting part 3, a fixing component locking part 4, a moving component positioning part 5, a moving component guide slide block 6, a cradle head main body and a control module, wherein the damping module 1 is directly fixed on the unmanned aerial vehicle;
4. the fixing component locking part 4 comprises an L-shaped locking pin 401, the L-shaped locking pin 401 is provided with a telescopic bolt part, when locking is not needed, the telescopic bolt of the locking pin is pushed and pulled to a non-locking position, and when locking is needed, the telescopic bolt is released to be inserted into the locking pin jack 7;
5. when the unmanned aerial vehicle needs to execute multi-task flight, quick exchange of task loads needs to be carried out, firstly, the task loads and the corresponding load switching blocks slide into the load mounting frame 10 together, the task loads slide to the limiting positions, quick-release bolts are screwed down to complete quick mounting of the loads, after flight of one task load is completed, the quick-release bolts are screwed down to dismount the task loads, the other loads and the corresponding load connecting blocks slide into the load mounting frame 10 together, the task loads slide to the limiting positions, the quick-release bolts are screwed down to complete quick mounting of the loads, and therefore quick exchange of the task loads is achieved.
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 (5)
1. The utility model provides a quick assembly disassembly light weight modularization increases steady cloud platform mechanism, includes shock-absorbing module (1) and increases steady cloud platform main part (2), its characterized in that: one side of the lower surface of the shock absorption module (1) is fixedly connected with a fixed component limiting part (3), the other side of the lower surface of the shock absorption module (1) is fixedly connected with a fixed component locking part (4), one side of the upper surface of the stability-increasing cradle head main body (2) is fixedly connected with a moving component positioning part (5), the other side of the upper surface of the stability-increasing cradle head main body (2) is fixedly connected with a moving component guide slide block (6), the surface of the moving component guide slide block (6) is provided with a locking pin jack (7), one side of the stability augmentation holder main body (2) is provided with an installation limiting block (8), installation spout (9) have been seted up on the surface of installation stopper (8), the inner wall sliding connection of installation spout (9) has load installing frame (10), prefabricated hole (11) have been seted up on the surface of load installing frame (10).
2. The quick-assembly, disassembly and assembly lightweight modular stability-enhancing pan-tilt mechanism of claim 1, wherein: the fixing component limiting part (3) comprises a first electrical connector (301), a positioning seat (302), prefabricated ejecting beads (303) and positioning pin holes (304), one side of the fixing component limiting part (3) is provided with the first electrical connector (301), the two ends of the fixing component limiting part (3) are provided with the positioning seats (302), the inner wall of each positioning seat (302) is movably connected with the prefabricated ejecting beads (303), the positioning pin holes (304) are formed in the surface of the positioning seat (302), the moving component positioning part (5) comprises positioning pins (501) and second electrical connectors (502), one side of the moving component positioning part (5) is provided with the second electrical connectors (502), and the two ends of the moving component positioning part (5) are fixedly connected with the positioning pins (501).
3. The quick-assembly, disassembly and assembly lightweight modular stability-enhancing pan-tilt mechanism of claim 2, wherein: the surface of the positioning pin (501) is movably connected with the inner wall of the positioning pin hole (304), and the surface of the first electrical connector (301) is movably connected with the inner wall of the second electrical connector (502).
4. The quick-assembly, disassembly and assembly lightweight modular stability-enhancing pan-tilt mechanism of claim 1, wherein: fixed subassembly locking portion (4) include L type locking pin (401) and direction spout (402), the both ends of fixed subassembly locking portion (4) all are provided with L type locking pin (401), the surface of fixed subassembly locking portion (4) is provided with direction spout (402).
5. The quick-assembly, disassembly and assembly lightweight modular stability-enhancing pan-tilt mechanism of claim 4, wherein: the surface of the L-shaped locking pin (401) is movably connected with the inner wall of the locking pin jack (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022003603.0U CN212829120U (en) | 2020-09-14 | 2020-09-14 | Quick assembly disassembly light weight modularization increases steady cloud platform mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022003603.0U CN212829120U (en) | 2020-09-14 | 2020-09-14 | Quick assembly disassembly light weight modularization increases steady cloud platform mechanism |
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| CN212829120U true CN212829120U (en) | 2021-03-30 |
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| CN202022003603.0U Active CN212829120U (en) | 2020-09-14 | 2020-09-14 | Quick assembly disassembly light weight modularization increases steady cloud platform mechanism |
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