CN218055648U - Unmanned aerial vehicle rapid disassembly structure - Google Patents
Unmanned aerial vehicle rapid disassembly structure Download PDFInfo
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- CN218055648U CN218055648U CN202222319073.XU CN202222319073U CN218055648U CN 218055648 U CN218055648 U CN 218055648U CN 202222319073 U CN202222319073 U CN 202222319073U CN 218055648 U CN218055648 U CN 218055648U
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Abstract
The utility model discloses an unmanned aerial vehicle rapid disassembly structure, which comprises a slide block and a connecting seat, wherein the outer edge of the slide block is provided with a guide convex edge, and the guide convex edge comprises a body and a flat tongue; the connecting seat is provided with a sliding groove and an insertion hole, the sliding groove is communicated with the insertion hole, and the connecting seat is provided with an elastic bolt; the slider is through leading-in spout of leading positive protruding edge to slide in towards the jack direction, promote flat tongue and insert the jack, the constant head tank grafting of elasticity bolt and slider locks the slider. The utility model discloses a structure of slip assembly to utilize to lead protruding along accurate and quick leading-in to spout, promote flat tongue and insert the jack and peg graft and target in place, the elasticity bolt is pegged graft with the constant head tank of slider and is carried out the locking location, thereby reaches the advantage that the dismouting is quick, accurate, convenient and can assemble great carry, solves the technical problem who exists among the prior art.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle and specifically relates to a quick and convenient unmanned aerial vehicle rapid disassembly structure of dismouting between unmanned aerial vehicle and carry is related to.
Background
The Chinese published patent No. CN215851943U discloses a rotary quick-dismantling device, which is applicable to the conditions of small mounting volume and light weight, and is inconvenient to operate on site if large volume or heavy weight is in charge; china's published patent publication No. CN216805850U states a quick detach structure and unmanned aerial vehicle for unmanned aerial vehicle carry, and it states a sliding connection structure, and it only discloses the structure of slip quick detach, and this structure appears the condition such as counterpoint inaccurate, dislocation installation in the in-service use in-process, and the structural stability after the assembly is not enough.
Therefore, how to design and manufacture a product capable of solving the technical problems of inconvenient operation, limited application, insufficient structural stability and the like in the prior art is one of the technical problems to be solved by the technical personnel in the field.
SUMMERY OF THE UTILITY MODEL
For the technical problem who exists among the above-mentioned prior art of solution, the utility model aims at providing a quick and convenient unmanned aerial vehicle rapid disassembly structure of dismouting.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an unmanned aerial vehicle rapid disassembly structure, its includes slider and connecting seat, wherein:
the outer edge of the sliding block is provided with a guide convex edge which comprises a body and a flat tongue;
the connecting seat is provided with a sliding groove and an insertion hole, the sliding groove is communicated with the insertion hole, and the connecting seat is assembled with an elastic bolt;
the slider is through leading-in spout of leading positive protruding edge to slide in towards the jack direction, promote flat tongue and insert the jack, the constant head tank grafting of elasticity bolt and slider locks the slider.
Further preferably: the guide convex edge is U-shaped and is arranged around the body and the flat tongue.
Further preferably: the guide convex edge is provided with a guide inclined plane.
Further preferred is: the body is provided with a connector male head mounting hole and the positioning groove;
the connector male head mounting hole is matched with the connector female head mounting hole of the connecting seat.
Further preferred is: the two positioning grooves are symmetrically distributed on two sides of the body.
Further preferably: the connecting seat includes seat and lower cover, wherein:
the upper seat is provided with a lower opening groove and a moving groove and is provided with an end wire harness box;
the lower cover is U-shaped and is fixedly locked in the lower opening groove, and the lower cover is provided with a buckle cover which covers the movable groove;
the spout is close to the open end setting of lower cover, the jack is close to the bottom setting of lower cover.
Further preferably: the upper seat is assembled on the unmanned aerial vehicle.
Further preferred is: elastic bolt includes bolt, spring, nut and inserted block, wherein:
the insert block is positioned in the moving groove and is a hollow body, and the nut is assembled in the insert block;
the spring is assembled on the bolt and is positioned between the moving groove and the inserting block;
the bolt penetrates through the movable groove and the inserting block and is in threaded connection with the nut.
Further preferred is: the bolt is provided with two bolt connection sections, one bolt connection section is in bolt connection with the screw hole of the movable groove, and the other bolt connection section is in bolt connection with the nut.
Further preferably: the insert block is provided with a pressing surface matched with the sliding block.
After the technical scheme is adopted, compared with the background art, the utility model, have following advantage:
the utility model discloses a slide assembly's structure to utilize to lead positive protruding edge accurate and quick leading-in to spout, promote flat tongue and insert the jack and peg graft and target in place, the constant head tank grafting of elasticity bolt and slider carries out the locking location, thereby reaches the advantage that the dismouting is quick, accurate, convenient and can assemble great carry, solves the technical problem who exists among the prior art.
Drawings
Fig. 1 is a schematic structural perspective view of the rapid dismounting structure of an unmanned aerial vehicle according to an embodiment of the present invention;
fig. 2 is an exploded view of the rapid dismounting structure of the unmanned aerial vehicle according to the embodiment of the present invention;
fig. 3 is a cross-sectional view of the rapid dismounting structure of the unmanned aerial vehicle along the Y-axis direction in the embodiment of the present invention;
fig. 4 is a cross-sectional view of the rapid dismounting structure of the unmanned aerial vehicle along the X-axis direction in the embodiment of the present invention;
fig. 5 is a schematic view of the slider structure according to the embodiment of the present invention;
fig. 6 is a schematic view of the connection seat structure in the embodiment of the present invention.
The reference numbers in the drawings of the specification are as follows:
100. the connector comprises a sliding block, 110, a body, 111, a positioning groove, 120, a flat tongue, 130, a guide convex edge, 200, a connecting seat, 201, a sliding groove, 202, a jack, 210, an upper seat, 211, a moving groove, 220, a lower cover, 221, a buckle cover, 222, a connector female head mounting hole, 300, an elastic bolt, 310, a bolt, 320, a spring, 330, an inserting block, 340 and a nut.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
In the present invention, it should be noted that the terms "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. are all based on the orientation or position relationship shown in the drawings, and are only for convenience of description, but not for indication or suggestion that the device or element of the present invention must have a specific orientation, and thus cannot be understood as a limitation of the present invention.
Examples
As shown in fig. 1 and fig. 2, an unmanned aerial vehicle rapid disassembly structure includes a sliding block 100 and a connecting seat 200, where the connecting seat 200 is assembled on an unmanned aerial vehicle, and the sliding block 100 is assembled on a mount (the mount is an apparatus such as a video camera, a camera, and a power supply that is hung on the abdomen of an unmanned aerial vehicle body).
As shown in fig. 1 and 2, the connecting socket 200 provides a sliding groove 201 and an insertion hole 202, and the sliding block 100 slides in from the sliding groove 201 and is inserted into the insertion hole 202, and is positioned by an elastic plug 300.
With reference to fig. 1 to 5, the slider 100 is a block-shaped body, and has an L-shaped overall cross section, and the guiding convex edge 130 is U-shaped, that is: the guide convex edge 130 is arranged around the sliding block 100; the pilot ledge 130 has a pilot slope. Specifically, the method comprises the following steps: the slider 100 comprises a body 110 and a flat tongue 120, wherein the body 110 is a rectangular block, the flat tongue 120 is arranged in the short side direction of the body 110, and the thickness of the flat tongue 120 is far smaller than that of the body 110; a connector male mounting hole 112 is formed in a part, close to the flat tongue 120, of the body 110, the connector male mounting hole 112 is matched with an existing connector male, and an opening is formed in the side face, close to the flat tongue 120, of the body 110 and is communicated with the connector male mounting hole 112; the body 110 is further provided with positioning grooves 111, the positioning grooves 111 are located on the side face of the body 110, the positioning grooves 111 are arranged on the side face of the long side direction of the body 110, in order to meet different position requirements, the number of the positioning grooves 111 is preferably two, and the positioning grooves 111 are symmetrically distributed on two sides of the body 110.
It should be noted that: as shown in fig. 5, the guiding ledge 130 is integrally connected to the body 110 and the tongue 120, and the tongue 120 is surrounded by the guiding ledge 130; the guiding ledge 130 is also disposed at a portion corresponding to the positioning groove 111.
Preferably, the following components: as shown in fig. 5, the body 110 has protruding strips, which are arranged along the long side direction of the body 110 and are far away from the tongue 120; the convex strip is located on the guiding convex edge 130 and integrally connected with the guiding convex edge 130.
Referring to fig. 1, 2, 3, 4 and 6, the connecting base 200 has a sliding groove 201 and an insertion hole, the sliding groove 201 is communicated with the insertion hole 202, the sliding groove 201 is disposed near an opening end of the lower cover 220, and the insertion hole 202 is disposed near a bottom end of the lower cover 220. That is to say: the insertion hole 202 needs to be introduced through the sliding groove 201 to realize insertion. Specifically, the method comprises the following steps: the side wall of the sliding groove 201 is matched with the guiding convex edge 130, that is to say: the side wall of the sliding chute 201 is provided with a sliding inclined surface, and the sliding inclined surface is matched with the guide inclined surface and is matched with the sliding guide. The side wall of the insertion hole 202 also has an inclined surface, and the inclined surface is matched with the guide inclined surface.
Referring to fig. 1, 2, 3, 4 and 6, a connector female mounting hole 222 is formed in the connecting base 200, and an opening is formed in a side wall of the sliding groove 201 and is aligned with and communicated with the connector female mounting hole 222; after the connecting seat 200 of the assembly connector female head and the sliding block 100 of the assembly connector male head are inserted, the connector female head and the connector male head are inserted to complete the connection of a mounting power supply or a signal.
As shown in fig. 1, 2, 4 and 6, the connecting base 200 is provided with a moving groove 211, the moving groove 211 is protruded, and the moving groove 211 is communicated with the sliding groove 201.
Specifically, the method comprises the following steps: referring to fig. 1, 2, 3, 4, and 6, the connection seat 200 includes an upper seat 210 and a lower cover 220, the upper seat 210 is fixed to the abdomen of the unmanned aerial vehicle body by screws, and the lower cover 220 is fixed to the upper seat 210. The upper seat 210 is a shell, and has a U-shaped lower opening groove, an end harness box 400 is assembled at one arc-shaped end of the upper seat, and a wire passing hole is formed in the end harness box 400; a moving groove 211 is formed in a side wall of the upper base 210, and the moving groove 211 protrudes from the side wall; the lower cover 220 is U-shaped and is buckled in the lower opening groove, the lower cover 220 has a buckling cover 221, and the buckling cover 221 is arranged corresponding to the moving groove 211 and buckled in the moving groove 211; of course, the upper and lower covers 220 of the connecting socket 200 may be formed as a single body.
As shown in fig. 1, 2, 3, 4 and 6, the elastic latch 300 is assembled in the moving groove 211; specifically, the method comprises the following steps: the elastic bolt 300 comprises a bolt 310, a spring 320, a nut 340 and an insert block 330, wherein the insert block 330 is a hollow body and is positioned in the moving groove 211, and the nut 340 is assembled in the insert block 330; the spring 320 is assembled on the bolt 310; the bolt 310 is threaded with the nut 340 through the sidewall of the moving slot 211 and the insert 330.
As shown in fig. 2 and 4, the bolt 310 includes a head and a screw rod, the head is large in size, the design is convenient for the operator to perform the operation, the screw rod is a stepped rod, and the diameter of the screw rod decreases towards the axial direction away from the head, in this embodiment: the screw rod has major diameter section and path section, the diameter of major diameter section is 6mm, and the diameter of path section is 3mm. The spring 320 is positioned in the movable groove 211 and sleeved on the large-diameter section of the bolt 310, and the small-diameter section passes through the plug and is connected with the nut 340; the bolt 310, i.e., the screw, has two screw coupling sections, one screw coupling section is screw coupled to the screw hole of the moving groove, and the other screw coupling section is screw coupled to the nut, i.e.: one of the screw connection sections is arranged corresponding to the screw hole and is in screw connection with the screw hole, and the other screw connection section is arranged corresponding to the nut and is in screw connection with the nut. The plug is a hollow block body and is provided with an insertion end, the side wall of the plug, which is close to the spring 320, is provided with a yielding hole, and the small-diameter section of the screw rod penetrates through the yielding hole to be in threaded connection with the nut 340; the nut 340 is placed within the plug. It should be noted that: one side surface of the plug facing the guiding convex edge 130 is a pressing surface, the pressing surface is matched with the corresponding position of the sliding block 100, and the insertion end of the plug extends into the positioning groove 111 of the sliding block 100.
As shown in fig. 2, 4 and 6, the screw of the elastic bolt 300 is screwed with the nut 340, the compression spring 320 pushes the plug to insert into the positioning groove 111, the pressing surface of the plug abuts against the slider 100, the position of the slider 100 is positioned, and the installation of the slider 100 and the connecting seat 200 is completed; the screw is in threaded connection with the screw hole of the movable groove 211 and is screwed in the screw for positioning the screw, namely, the screw cannot pop out from the positioning groove 111 due to factors such as the reset force of the spring 320; on the contrary, the screw is screwed out from the screw hole of the moving slot 211, the screw is driven to disengage from the nut 340, the spring 320 is reset, the bolt 310 is pushed to move towards the direction away from the positioning slot 111, at this time, the plug is also pulled out from the positioning slot 111, and the slider 100 can slide and move.
With reference to fig. 1 to 6, the specific dismounting process of the quick release structure of the unmanned aerial vehicle is as follows:
installation: the flat tongue 120 in the sliding block 100 is placed towards the sliding groove 201 and slides into the sliding groove 201, and the purpose of quick and accurate alignment is realized by the matching of the guiding convex edge 130 and the guiding groove; the sliding block 100 slides in from the sliding groove 201 and pushes the flat tongue 120 to be inserted into the insertion hole 202; the plug of the elastic bolt 300 is inserted into the positioning groove 111, so that the sliding block 100 is positioned, and the assembly of the sliding block 100 and the connecting seat 200 is realized;
disassembling: first, the elastic latch 300 is released (i.e., the screw hole of the screw moving groove 211 is screwed out), so that the plug is pulled out from the positioning groove 111; secondly, the sliding block 100 is driven to slide out of the sliding groove 201 and drive the plug to be pulled out of the jack 202, so that the sliding block 100 and the connecting seat 200 are detached.
In summary, the installation and detachment process between the slider 100 and the connecting seat 200 has the advantages of convenient operation and simple operation, and the structural design is utilized to achieve the advantages of accurate and rapid alignment, thereby achieving the purpose of quick detachment and blocking.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any changes or substitutions that can be easily conceived by those skilled in the art within the technical scope of the present invention should be covered by the present invention. Therefore, the protection scope of the present invention shall be subject to the protection scope of the claims.
Claims (10)
1. Unmanned aerial vehicle rapid disassembly structure, its characterized in that: it includes slider and connecting seat, wherein:
the outer edge of the sliding block is provided with a guide convex edge which comprises a body and a flat tongue;
the connecting seat is provided with a sliding groove and an insertion hole, the sliding groove is communicated with the insertion hole, and the connecting seat is assembled with an elastic bolt;
the slider is through leading-in spout of leading positive protruding edge to slide in towards the jack direction, promote flat tongue and insert the jack, the constant head tank grafting of elasticity bolt and slider locks the slider.
2. The fast dismounting structure of unmanned aerial vehicle of claim 1, characterized in that: the guide convex edge is U-shaped and is arranged around the body and the flat tongue.
3. The fast dismounting structure of unmanned aerial vehicle of claim 1 or 2, characterized in that: the guide convex edge is provided with a guide inclined plane.
4. The rapid disassembly structure of unmanned aerial vehicle of claim 1, wherein: the body is provided with a connector male head mounting hole and the positioning groove;
the connector male head mounting hole is matched with the connector female head mounting hole of the connecting seat.
5. The fast dismounting structure of unmanned aerial vehicle of claim 1, characterized in that: the two positioning grooves are symmetrically distributed on two sides of the body.
6. The rapid disassembly structure of unmanned aerial vehicle of claim 1, wherein: the connecting seat includes seat and lower cover, wherein:
the upper seat is provided with a lower opening groove and a moving groove and is provided with an end wire harness box;
the lower cover is U-shaped and is locked in the lower opening groove, and the lower cover is provided with a buckle cover which covers the movable groove;
the spout is close to the open end setting of lower cover, the jack is close to the bottom setting of lower cover.
7. The rapid disassembly structure of unmanned aerial vehicle of claim 6, wherein: the upper seat is assembled on the unmanned aerial vehicle.
8. The fast dismounting structure of unmanned aerial vehicle of claim 6, characterized in that: elastic bolt includes bolt, spring, nut and inserted block, wherein:
the insert block is positioned in the moving groove and is a hollow body, and the nut is assembled in the insert block;
the spring is assembled on the bolt and positioned between the moving groove and the inserting block;
the bolt penetrates through the moving groove and the inserting block and is in threaded connection with the nut.
9. The rapid disassembly structure of unmanned aerial vehicle of claim 8, wherein: the bolt is provided with two bolt connection sections, one bolt connection section is in bolt connection with the screw hole of the moving groove, and the other bolt connection section is in bolt connection with the nut.
10. The rapid disassembly structure of unmanned aerial vehicle of claim 8, wherein: the insert block is provided with a pressing surface matched with the sliding block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222319073.XU CN218055648U (en) | 2022-09-01 | 2022-09-01 | Unmanned aerial vehicle rapid disassembly structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222319073.XU CN218055648U (en) | 2022-09-01 | 2022-09-01 | Unmanned aerial vehicle rapid disassembly structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218055648U true CN218055648U (en) | 2022-12-16 |
Family
ID=84409285
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222319073.XU Active CN218055648U (en) | 2022-09-01 | 2022-09-01 | Unmanned aerial vehicle rapid disassembly structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218055648U (en) |
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2022
- 2022-09-01 CN CN202222319073.XU patent/CN218055648U/en active Active
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Unmanned Aerial Vehicle Quick Demolition Structure Effective date of registration: 20230706 Granted publication date: 20221216 Pledgee: Xiamen Bank Co.,Ltd. Pledgor: XIAMEN TIANYUAN OURUI TECHNOLOGY Co.,Ltd. Registration number: Y2023980047603 |