CN216053752U - Formation unmanned aerial vehicle's light module quick assembly disassembly part - Google Patents
Formation unmanned aerial vehicle's light module quick assembly disassembly part Download PDFInfo
- Publication number
- CN216053752U CN216053752U CN202122118888.7U CN202122118888U CN216053752U CN 216053752 U CN216053752 U CN 216053752U CN 202122118888 U CN202122118888 U CN 202122118888U CN 216053752 U CN216053752 U CN 216053752U
- Authority
- CN
- China
- Prior art keywords
- bolt
- light module
- unmanned aerial
- aerial vehicle
- connecting column
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model relates to the technical field of unmanned aerial vehicles, and discloses a quick light module dismounting component of a formation unmanned aerial vehicle, which is used for quickly dismounting a machine body and a light module of the unmanned aerial vehicle and comprises a connecting column, and a first bolt and a second bolt which are arranged at two ends of the connecting column; the first bolt comprises first elastic pieces symmetrically arranged at the top end of the connecting column, the second bolt comprises two second elastic pieces symmetrically arranged at the bottom end of the connecting column, and the first elastic pieces and the second elastic pieces can be kneaded or separated relative to the connecting column respectively; the bottom of the machine body is provided with a plurality of first jacks matched with the first bolts, and the light module is provided with a plurality of second jacks matched with the second bolts; and the middle part of the connecting column is provided with a limiting ring along the radial direction in a surrounding manner. The fast assembly and disassembly component for the light module of the formation unmanned aerial vehicle is reasonable in structural design and small in size, and can realize fast assembly of the light module and the unmanned aerial vehicle.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a rapid light module dismounting component of a formation unmanned aerial vehicle.
Background
At present, mainstream formation unmanned aerial vehicle performance is based on light display, and a plurality of unmanned aerial vehicles form light patterns in the air to show performance effects, such as a color screen in the same sky. Since the formation drone performs like a color screen, there may be problems with conventional display screens that are prone to occur after intensive use: bad spots, color cast, color error and the like. And after the above-mentioned problem has appeared, just need to change the light module that corresponding unmanned aerial vehicle assembled.
However, the light modules on the common formation unmanned aerial vehicles are fixed by screws, and if the screws are poor in quality, the screws are easily disassembled and assembled repeatedly and are easy to slip, fine screws are also easily lost, and the workload of replacing the light modules is increased; in addition, if the screw is corroded in the screw hole, the screw can be inconvenient to disassemble and assemble, and the machine body can be damaged.
Therefore, it is actually necessary to provide a light module quick assembly and disassembly part of the formation unmanned aerial vehicle for solving the above problems.
SUMMERY OF THE UTILITY MODEL
The quick disassembling and assembling part for the light modules of the formation unmanned aerial vehicles is mainly used for solving the problems that the light modules of the common formation unmanned aerial vehicles are fixed by screws, the screws are easy to slide after being repeatedly disassembled and assembled, and the screws are also easy to rust in screw holes, so that the disassembly and the assembly are inconvenient.
In order to solve the technical problems, the technical scheme adopted by the utility model is as follows:
a quick assembly and disassembly component for a light module of an unmanned aerial vehicle for formation is used for quickly assembling and disassembling a body and the light module of the unmanned aerial vehicle and comprises a connecting column, a first bolt and a second bolt, wherein the first bolt and the second bolt are arranged at two ends of the connecting column;
the first bolt comprises two first elastic sheets which are symmetrically arranged at the top end of the connecting column in a splayed manner, the second bolt comprises two second elastic sheets which are symmetrically arranged at the bottom end of the connecting column in a splayed manner, the two first elastic sheets and the two second elastic sheets can be kneaded or separated relative to the connecting column respectively, and the first bolt and the second bolt form arrow-shaped structures in opposite directions respectively;
a plurality of first jacks matched with the first bolts are arranged at the bottom of the machine body in a penetrating manner, and a plurality of second jacks which vertically correspond to the first jacks and are matched with the second bolts are arranged on the light module in a penetrating manner;
the middle part of the connecting column is provided with a limiting ring along the radial direction in a surrounding manner, so that the quick assembly disassembly part body can be limited up and down when being connected and assembled with the machine body and the light module.
Furthermore, the outer diameter of the limiting ring is larger than the inner diameters of the first jack and the second jack, the structural design is reasonable, and the limiting function is convenient to realize during assembly.
Furthermore, the distance between one end of the first bolt close to the limiting ring and the limiting ring is not smaller than the thickness of the shell of the machine body, namely, after the two first elastic pieces are separated relative to the connecting column, the distance between the separating ends of the first elastic pieces and the limiting ring is not smaller than the thickness of the shell of the machine body, the design is reasonable, and the assembly coordination is good.
Furthermore, the second bolt is close to the one end of spacing ring with interval between the spacing ring is not less than the thickness of light module, two promptly the second flexure strip for the spliced pole separation back, second flexure strip separation end with interval between the spacing ring is not less than the thickness of light module, reasonable in design, the assembly harmony is good.
Furthermore, the connecting column with first bolt, second bolt and spacing ring be integrated into one piece structure, are convenient for process and assemble, labour saving and time saving.
Furthermore, the connecting column, the first bolt, the second bolt and the limiting ring are made of rubber or silica gel materials, so that the connecting column is light in weight, good in elasticity or toughness, capable of being used repeatedly and saving cost.
Furthermore, the connecting column is of a strip-shaped or cylindrical structure.
Furthermore, the width of the periphery of the two first elastic pieces of the first bolt after being kneaded relative to the connecting column is smaller than the inner diameter of the first jack, and the width of the periphery of the two first elastic pieces after being separated relative to the connecting column is larger than the inner diameter of the first jack, so that the assembling coordination is good, and the connection is reliable.
Furthermore, the width of the periphery of the two second elastic pieces of the second bolt after being kneaded relative to the connecting column is smaller than the inner diameter of the second jack, and the width of the periphery of the two second elastic pieces after being separated relative to the connecting column is larger than the inner diameter of the second jack, so that the assembling coordination is good, and the connection is reliable.
Furthermore, the two first elastic pieces of the first bolt are not larger than the outer diameter of the limiting ring relative to the periphery width of the separated connecting column and the two second elastic pieces of the second bolt are not larger than the outer diameter of the limiting ring relative to the periphery width of the separated connecting column, so that the appearance is simple and attractive, the size is reduced, and materials are saved.
Compared with the prior art, the technical scheme of the utility model has the beneficial effects that:
1. the rapid disassembly and assembly part of the light module of the formation unmanned aerial vehicle is simple and reasonable in design, small in size, low in manufacturing cost, easy to machine and assemble, convenient to use, stable and reliable in connection with the unmanned aerial vehicle and the light module, reusable and long in service life;
2. when the quick disassembly and assembly part of the light module is used, the top end of the first bolt is inserted into a first jack of a machine body, the two first elastic pieces are gradually extruded by the inner side of the first jack along with the insertion of the first bolt and are kneaded relatively, when the bottom surface of the machine body contacts a limiting ring, the first bolt completely enters the machine body, the two first elastic pieces recover to deform and automatically bounce open and are matched with the limiting ring, so that the first bolt is integrally fixed on the machine body; then aligning a second jack on the light module with the second plug pin, pushing the light module towards the machine body, extruding and relatively kneading two second elastic sheets of the second plug pin by the inner side of the second jack, and after the second jack and the second plug pin are assembled in place, the two second elastic sheets can restore to deform and automatically bounce open, so that the light module and the machine body are fixedly assembled, the assembly is quick and convenient, the screw fixation is not needed, the phenomena of screw slipping or losing and the like are avoided, the time and the labor are saved, and the light module is suitable for popularization and application;
3. after the rapid assembly and disassembly component of the light module of the formation unmanned aerial vehicle is adopted, the rapid assembly and disassembly of the light module can be completed only by kneading the two second elastic pieces of the second bolt when the light module is disassembled or assembled, a screwdriver is not needed to screw the screws, and if the body of the rapid assembly and disassembly component is damaged, the damaged rapid assembly and disassembly component can be disassembled from the machine body for replacement only by kneading the two first elastic pieces of the first bolt, so that the rapid assembly and disassembly component is simple and convenient.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to the drawings without creative efforts.
Fig. 1 is a perspective view of a light module quick-release component of a formation unmanned aerial vehicle of the present invention;
fig. 2 is a side view of a light module quick-release component of a formation drone of the present invention;
FIG. 3 is a schematic view of the assembly of a formation drone and a lighting module of the present invention by means of quick-release components;
fig. 4 is an enlarged view of fig. 3 at a.
Reference numerals: 1-machine body, 11-first jack, 2-light module, 21-second jack, 3-connecting column, 31-limiting ring, 4-first bolt, 41-first elastic sheet, 5-second bolt and 51-second elastic sheet.
Detailed Description
The drawings are for illustrative purposes only and are not to be construed as limiting the patent; for better illustration of the present embodiment, certain elements of the drawings may be omitted, enlarged or reduced, and do not represent diameters of actual products; it will be understood by those skilled in the art that certain well-known structures in the drawings and descriptions thereof may be omitted.
The description of "first", "second", etc. referred to in the embodiments of the present invention is for descriptive purposes only and is not to be construed as indicating or implying any relative importance or implicit indication of the number of technical features indicated, whereby the features defined as "first", "second", etc. may explicitly or implicitly include at least one such feature.
Meanwhile, the terms "upper", "lower", "front", "rear", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience in describing the present invention and simplifying the description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted" and "connected" are to be interpreted broadly, e.g., as being either fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, so to speak, as communicating between the two elements. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
In order to more clearly understand the technical features, objects and effects of the present invention, embodiments of the present invention will now be described in detail with reference to the accompanying drawings, but the embodiments of the present invention are not limited thereto.
The implementation mode is as follows:
as shown in fig. 1 to 4, the quick assembly and disassembly component for the light modules of the formation unmanned aerial vehicles is used for quickly assembling and disassembling the body 1 and the light modules 2 of the unmanned aerial vehicles, and comprises a connecting column 3, and a first bolt 4 and a second bolt 5 which are arranged at two ends of the connecting column 3;
the first bolt 4 comprises two first elastic sheets 41 which are symmetrically arranged at the top end of the connecting column 3 in a splayed manner, the second bolt 5 comprises two second elastic sheets 51 which are symmetrically arranged at the bottom end of the connecting column 3 in a splayed manner, the two first elastic sheets 41 and the two second elastic sheets 51 can be respectively kneaded or separated relative to the connecting column 3, and the first bolt 4 and the second bolt 5 respectively form arrow-shaped structures with opposite directions;
a plurality of first jacks 11 matched with the first bolts 4 are arranged at the bottom of the machine body 1 in a penetrating manner, and a plurality of second jacks 21 which correspond to the first jacks 11 up and down and are matched with the second bolts 5 are arranged on the light module 2 in a penetrating manner;
the middle part of the connecting column 3 is provided with a limiting ring 31 along the radial direction in a surrounding way, and the limiting ring can play a role in limiting the quick assembly disassembly part body up and down when being connected and assembled with the machine body 1 and the light module 2.
The external diameter of spacing ring 31 is greater than the internal diameter of first jack 11 and second jack 21, and structural design is reasonable, is convenient for realize limit function during the assembly.
The interval between the one end that first bolt 4 is close to spacing ring 31 and spacing ring 31 is not less than organism 1's shell thickness, and two first flexure strips 41 are for spliced pole 3 separation back promptly, and the interval between first flexure strip 41 separation end and the spacing ring 31 is not less than organism 1's shell thickness, reasonable in design, and the assembly harmony is good.
The second bolt 5 is close to the one end of spacing ring 31 and the interval between spacing ring 31 is not less than the thickness of light module 2, and two second flexure strips 51 are for spliced pole 3 separation back promptly, and the interval between second flexure strip 51 separation end and the spacing ring 31 is not less than the thickness of light module 2, reasonable in design, and the assembly harmony is good.
The connecting column 3, the first bolt 4, the second bolt 5 and the limiting ring 31 are of an integrated structure, so that the processing and the assembly are convenient, and the time and the labor are saved.
The connecting column 3, the first bolt 4, the second bolt 5 and the limiting ring 31 are made of rubber or silica gel materials, so that the light-weight and high-elasticity or toughness plastic is light in weight and can be used repeatedly, and the cost is saved.
The connecting column 3 is of a strip-shaped structure, is easy to machine and form, and has a simple and attractive structure.
The peripheral width of two first elastic pieces 41 of first bolt 4 after kneading for spliced pole 3 is less than the internal diameter of first jack 11, and the peripheral width of two first elastic pieces 41 after for spliced pole 3 separation is greater than the internal diameter of first jack 11, and the assembly harmony is good, connects reliably.
The peripheral width of the two second elastic sheets 51 of the second bolt 5 kneaded relative to the connecting column 3 is smaller than the inner diameter of the second insertion hole 21, the peripheral width of the two second elastic sheets 51 separated relative to the connecting column 3 is larger than the inner diameter of the second insertion hole 21, the assembling coordination is good, and the connection is reliable.
Two first flexure strips 41 of first bolt 4 are for the periphery width after the spliced pole 3 separation and two second flexure strips 51 of second bolt 5 are for the external diameter that the periphery width after the spliced pole 3 separation all is not greater than spacing ring 31, and the appearance is brief pleasing to the eye, is favorable to dwindling the volume, material saving.
The utility model relates to an installation and use steps of a quick disassembly and assembly part of a formation unmanned aerial vehicle light module, which are as follows:
firstly, the top end of a first bolt 4 is inserted into a first jack 11 of a machine body 1, two first elastic sheets 41 are gradually extruded by the inner side of the first jack 11 along with the insertion of the first bolt 4 and are kneaded relatively, when the bottom surface of the machine body 1 contacts a limit ring 31, the first bolt 4 completely enters the machine body 1, the two first elastic sheets 41 can restore to deform and automatically bounce open to be matched with the limit ring 31, and the first bolt 4 is integrally fixed on the machine body 1;
aligning the second jack 21 on the light module 2 to the second plug pin 5, pushing the light module 2 towards the machine body, and extruding and relatively kneading the two second elastic sheets 51 of the second plug pin 5 by the inner side of the second jack 21, wherein when the second jack 21 and the second plug pin 5 are assembled in place, the two second elastic sheets 51 can restore to deform and automatically bounce open, so that the light module 2 and the machine body 1 are fixedly assembled;
when light module 2 need be dismantled, press two second flexure strips 51 of second bolt 5 gently, lift up light module 2 gently simultaneously, make two second flexure strips 51 all imbed in light module 2's second jack 21, adopt same mode, confirm that second flexure strip 51 on all second bolts 5 all imbeds corresponding second jack 21 in the back, drop-down light module 2 gently, make all second bolts 5 break away from light module 2 completely, can accomplish light module 2's dismantlement work.
In the drawings, the positional relationship is described for illustrative purposes only and is not to be construed as limiting the present patent; it should be understood that the above-described embodiments of the present invention are merely examples for clearly illustrating the present invention, and are not intended to limit the embodiments of the present invention. Other variations and modifications will be apparent to persons skilled in the art in light of the above description. And are neither required nor exhaustive of all embodiments. Any modification, equivalent replacement, and improvement made within the spirit and principle of the present invention should be included in the protection scope of the claims of the present invention.
Claims (10)
1. A quick assembly and disassembly component for a light module of a formation unmanned aerial vehicle is used for quickly assembling and disassembling a machine body and the light module and is characterized by comprising a connecting column, a first bolt and a second bolt, wherein the first bolt and the second bolt are arranged at two ends of the connecting column;
the first bolt comprises two first elastic sheets which are symmetrically arranged at the top end of the connecting column in a splayed manner, the second bolt comprises two second elastic sheets which are symmetrically arranged at the bottom end of the connecting column in a splayed manner, and the first elastic sheets and the second elastic sheets can be kneaded or separated relative to the connecting column respectively;
a plurality of first jacks matched with the first bolts are arranged at the bottom of the machine body in a penetrating manner, and a plurality of second jacks which vertically correspond to the first jacks and are matched with the second bolts are arranged on the light module in a penetrating manner;
and the middle part of the connecting column is provided with a limiting ring along the radial direction in a surrounding manner.
2. The light module quick assembly disassembly part of formation unmanned aerial vehicle of claim 1, characterized in that, the external diameter of spacing ring is greater than the internal diameter of first jack and second jack.
3. The formation unmanned aerial vehicle's light module quick assembly disassembly part of claim 2, characterized in that, the first bolt is close to the spacing ring one end and the interval between the spacing ring is not less than the shell thickness of organism.
4. The formation unmanned aerial vehicle's light module quick assembly disassembly part of claim 3, characterized in that, the second bolt is close to the spacing ring one end and the interval between the spacing ring is not less than the thickness of light module.
5. The light module quick assembly disassembly part of formation unmanned aerial vehicle of claim 1, characterized in that, the spliced pole with first bolt, second bolt and spacing ring are integrated into one piece structure.
6. The formation unmanned aerial vehicle's light module quick assembly disassembly part of claim 5, characterized in that, the spliced pole with first bolt, second bolt and spacing ring all adopt rubber or silica gel material to make.
7. The formation unmanned aerial vehicle's light module quick assembly disassembly part of claim 1, characterized in that, the spliced pole is strip slice or cylindric structure.
8. The fast assembly and disassembly component of light modules of unmanned aerial vehicles for formation in formation according to any one of claims 1 to 7, wherein the width of the outer periphery of the two first elastic pieces of the first bolt after being kneaded is smaller than the inner diameter of the first insertion hole, and the width of the outer periphery of the two first elastic pieces after being separated is larger than the inner diameter of the first insertion hole.
9. The fast assembly and disassembly component of light module of formation unmanned aerial vehicle of claim 8, wherein the relative outer circumferential width of kneading of two second elastic pieces of the second bolt is less than the inside diameter of the second jack, and the relative outer circumferential width of separating of two second elastic pieces is greater than the inside diameter of the second jack.
10. The formation unmanned aerial vehicle's light module quick assembly disassembly part of claim 9, characterized in that, the relative peripheral width after-separating of two first elastic pieces of first bolt and the relative peripheral width after-separating of two second elastic pieces of second bolt are all not greater than the external diameter of spacing ring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122118888.7U CN216053752U (en) | 2021-09-03 | 2021-09-03 | Formation unmanned aerial vehicle's light module quick assembly disassembly part |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122118888.7U CN216053752U (en) | 2021-09-03 | 2021-09-03 | Formation unmanned aerial vehicle's light module quick assembly disassembly part |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216053752U true CN216053752U (en) | 2022-03-15 |
Family
ID=80535406
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122118888.7U Active CN216053752U (en) | 2021-09-03 | 2021-09-03 | Formation unmanned aerial vehicle's light module quick assembly disassembly part |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216053752U (en) |
-
2021
- 2021-09-03 CN CN202122118888.7U patent/CN216053752U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN216053752U (en) | Formation unmanned aerial vehicle's light module quick assembly disassembly part | |
| US7570317B2 (en) | Flat panel display with wire fixing structure | |
| CN207278632U (en) | Curved surface mounting structure, display screen, combined type display screen | |
| CN210183430U (en) | Assembled liquid crystal display television back plate structure and liquid crystal display television | |
| CN215245581U (en) | Photovoltaic board dust detection device based on many rotor unmanned aerial vehicle | |
| CN201438284U (en) | Computer casing | |
| CN201697052U (en) | Lamp frame structure and clamping piece thereof | |
| CN212156744U (en) | U type structure lamp strip convenient to installation | |
| CN220829792U (en) | Quick detach formula direction sign subassembly | |
| CN211548404U (en) | Hollow sunshine board of PC convenient to concatenation | |
| CN218431767U (en) | Unmanned aerial vehicle protection machanism convenient to dismouting | |
| CN212510814U (en) | Ceiling lamp support mounting structure | |
| CN113175137B (en) | Aluminum veneer wall curtain | |
| CN213920323U (en) | Coding machine for zipper strip processing | |
| CN220481739U (en) | Thoracic cavity control structure and robot | |
| CN221101614U (en) | Vehicle-mounted curved surface screen structure | |
| CN2681609Y (en) | Combined frame of combined wardrobes | |
| CN220895182U (en) | Assembled acoustic metamaterial sound insulation module | |
| CN214513815U (en) | Hollow fiber membrane filtering component convenient to mount and dismount | |
| CN210069745U (en) | Light-transmitting cover for lamp | |
| CN210777698U (en) | Lamp box fixing assembly and lamp box with same | |
| CN219199451U (en) | Shell assembly and air purifier | |
| CN212715765U (en) | Mechanically-installed wall body plate fixing structure | |
| CN218317361U (en) | Lighting device and unmanned aerial vehicle | |
| CN215399349U (en) | A light-duty simple and easy gun rack for unmanned aerial vehicle strikes system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: Room 737, No. 1256, 1258, Wanrong Road, Jing'an District, Shanghai, 200000 Patentee after: Shanghai Qianji Innovation Culture and Tourism Technology Group Co., Ltd. Address before: 510000 room 310-j002, No. 1, Mingzhu 1st Street, Hengli Town, Nansha District, Guangzhou City, Guangdong Province Patentee before: Guangzhou crossing Qianji Innovation Technology Co.,Ltd. |
|
| CP03 | Change of name, title or address |