CN213594545U - Quick plug installation device of unmanned aerial vehicle auxiliary - Google Patents
Quick plug installation device of unmanned aerial vehicle auxiliary Download PDFInfo
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- CN213594545U CN213594545U CN202021876813.4U CN202021876813U CN213594545U CN 213594545 U CN213594545 U CN 213594545U CN 202021876813 U CN202021876813 U CN 202021876813U CN 213594545 U CN213594545 U CN 213594545U
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- 238000009434 installation Methods 0.000 title claims abstract description 26
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- 238000000034 method Methods 0.000 abstract description 3
- 238000001125 extrusion Methods 0.000 abstract 1
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- 239000000463 material Substances 0.000 description 6
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- 208000035473 Communicable disease Diseases 0.000 description 1
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- 230000008602 contraction Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
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Abstract
The utility model discloses a quick plug installation device of unmanned aerial vehicle auxiliary, including backup pad and fixed plate, the side fixedly connected with installation piece of backup pad, the medial surface fixedly connected with sleeve of fixed plate. This quick plug installation device of unmanned aerial vehicle accessory is provided with the conducting block, the fixed plate, the sleeve, first spring, backing plate and buckle, and the fixed plate, the sleeve, first spring, backing plate and buckle symmetry are provided with two sets ofly in the backup pad, install the device on unmanned aerial vehicle through the bolt that sets up in the through-hole, promote the buckle, at the in-process that promotes the buckle, the first spring in the backing plate extrusion sleeve, be connected accessory equipment and conducting block, the conducting block is provided with two sets ofly in the backup pad, be positive pole and negative pole respectively, and the conducting block passes through outside wire and is connected with the unmanned aerial vehicle power, accessory equipment circular telegram this moment, two sets of buckles inwards move under the effect of first spring, fix accessory equipment, need not use the ribbon to fix, and it is comparatively firm to install.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a quick plug installation device of unmanned aerial vehicle auxiliary.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
At present, unmanned aerial vehicle accessory equipment is mostly the shape equipment alone if according to lamp megaphone etc. installs very inconveniently with the ribbon through installing the fixed plate additional, and when unmanned aerial vehicle carries out high-speed flight, accessory equipment rocks easily, can drop from unmanned aerial vehicle even when serious.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a quick plug installation device of unmanned aerial vehicle auxiliary to solve the unmanned aerial vehicle auxiliary equipment on the existing market that above-mentioned background art provided and mostly be independent shape equipment if according to lamp megaphone etc., install very inconveniently through installing the ribbon for the fixed plate additional, and when unmanned aerial vehicle carries out high-speed flight, auxiliary equipment rocks easily, can follow the problem that unmanned aerial vehicle drops even when serious.
In order to achieve the above object, the utility model provides a following technical scheme: a rapid plugging and unplugging mounting device for an unmanned aerial vehicle accessory comprises a supporting plate and a fixing plate, wherein the side surface of the supporting plate is fixedly connected with a mounting block, the mounting block is provided with a through hole, a conductive block is fixedly connected above the supporting plate, wherein,
the utility model discloses a quick-witted, including the fixed plate, the medial surface fixedly connected with sleeve of fixed plate, the first spring of fixedly connected with in the sleeve, the top fixedly connected with backing plate of first spring, the side fixedly connected with bracing piece of backing plate, the top fixedly connected with buckle of bracing piece, the constant head tank has been seted up in the backup pad, swing joint has the gag lever post in the constant head tank, the terminal fixedly connected with quick detach board of gag lever post, fixedly connected with limiting plate on the quick detach board, it presss from both sides the mouth to have seted up equipment in the limiting plate, the first solid fixed ring of fixedly connected with in the equipment presss from both sides the mouth, fixedly connected with second spring in the first solid fixed ring, the solid.
Preferably, the conducting block is provided with two sets of in the backup pad, is anodal and negative pole respectively, and the conducting block passes through external conductor and is connected with the unmanned aerial vehicle power.
Preferably, the fixed plate, the sleeve, the first spring, the base plate, the support rod and the buckle are symmetrically arranged in two groups on the support plate, and the sum of the lengths of the two groups of sleeves, the first spring, the base plate, the support rod and the buckle is larger than half of the length of the support plate.
Preferably, the outer diameter of the first spring is the same as the inner diameter of the sleeve, and the length of the first spring is less than the depth of the sleeve.
Preferably, the cross section of constant head tank and gag lever post is T shape, and the constant head tank symmetry is provided with two sets ofly in the backup pad, and the gag lever post symmetry is provided with two sets ofly on the quick detach board, constant head tank and gag lever post one-to-one.
Preferably, the first fixing ring, the second spring and the second fixing ring form a clamping mechanism, and the first fixing ring and the second fixing ring are made of rubber.
Compared with the prior art, the beneficial effects of the utility model are that: this quick plug installation device of unmanned aerial vehicle auxiliary:
1. the device is provided with a conductive block, a fixed plate, a sleeve, a first spring, a base plate, a support rod and a buckle, wherein the fixed plate, the sleeve, the first spring, the base plate, the support rod and the buckle are symmetrically provided with two groups on a support plate;
2. the quick-release plate is provided with the positioning grooves and the limiting rods, the positioning grooves are symmetrically provided with two groups on the supporting plate, the limiting rods are symmetrically provided with two groups on the quick-release plate, the positioning grooves and the limiting rods are in one-to-one correspondence, the quick-release plate can be quickly installed on the fixed plate through the matching connection of the positioning grooves and the limiting rods, the quick-release plate is convenient to disassemble, and the cross sections of the positioning grooves and the limiting rods are T-shaped, so that the quick-release plate can be;
3. be provided with equipment and press from both sides the mouth, first solid fixed ring, the solid fixed ring of second spring and second, accomplish the back with the installation of quick detach board, continue to promote the quick detach board, it presss from both sides the mouth to pass equipment until auxiliary equipment, because the solid fixed ring of first solid fixed ring and second material is rubber, through the yielding characteristic of rubber material, can tightly fix auxiliary equipment in the solid fixed ring of second, prevent auxiliary equipment overlength, only lean on the unable condition that makes auxiliary equipment stable installation of buckle, and through the flexible of second spring, to auxiliary equipment's when slowing down unmanned aerial vehicle flight condition, prevent that auxiliary equipment from droing from unmanned aerial vehicle.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the quick release plate structure of the present invention;
fig. 3 is an enlarged view of the part a structure of the present invention.
In the figure: 1. a support plate; 2. mounting blocks; 3. a through hole; 4. a conductive block; 5. a fixing plate; 6. a sleeve; 7. a first spring; 8. a base plate; 9. a support bar; 10. buckling; 11. positioning a groove; 12. a limiting rod; 13. a quick release plate; 14. a limiting plate; 15. a device nip; 16. a first retaining ring; 17. a second spring; 18. a second retaining ring.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-3, the present invention provides a technical solution: a rapid plugging and pulling installation device for an auxiliary of an unmanned aerial vehicle comprises a support plate 1, an installation block 2, a through hole 3, a conductive block 4, a fixing plate 5, a sleeve 6, a first spring 7, a backing plate 8, a support rod 9, a buckle 10, a positioning groove 11, a limiting rod 12, a quick-release plate 13, a limiting plate 14, a device clamping opening 15, a first fixing ring 16, a second spring 17 and a second fixing ring 18, wherein the side surface of the support plate 1 is fixedly connected with the installation block 2, the through hole 3 is formed in the installation block 2, the conductive block 4 is fixedly connected above the support plate 1, the conductive block 4 is provided with two groups on the support plate 1, namely an anode and a cathode, the conductive block 4 is connected with a power supply of the unmanned aerial vehicle through an external lead, the electrified operation of the auxiliary device can be realized without additionally installing an external power supply,
the inner side surface of the fixing plate 5 is fixedly connected with a sleeve 6, a first spring 7 is fixedly connected in the sleeve 6, the outer diameter of the first spring 7 is the same as the inner diameter of the sleeve 6, the length of the first spring 7 is smaller than the depth of the sleeve 6, the situation that the backing plate 8 is popped out of the sleeve 6 and cannot reset due to overlong length of the first spring 7 is prevented, a backing plate 8 is fixedly connected to the top end of the first spring 7, a supporting rod 9 is fixedly connected to the side surface of the backing plate 8, a buckle 10 is fixedly connected above the supporting rod 9, two groups of the fixing plate 5, the sleeve 6, the first spring 7, the backing plate 8, the supporting rod 9 and the buckle 10 are symmetrically arranged on the supporting plate 1, the sum of the lengths of the two groups of the sleeve 6, the first spring 7, the backing plate 8, the supporting rod 9 and the buckle 10 is larger than half of the length of the supporting plate 1, and the, the quick-release auxiliary part device is characterized in that a positioning groove 11 is formed in the supporting plate 1, a limiting rod 12 is movably connected in the positioning groove 11, the cross sections of the positioning groove 11 and the limiting rod 12 are in a T shape, two groups of positioning grooves 11 are symmetrically arranged on the supporting plate 1, two groups of limiting rods 12 are symmetrically arranged on the quick-release plate 13, the positioning grooves 11 and the limiting rods 12 correspond one to one, the quick-release plate 13 is quickly disassembled and installed by matching and connecting the positioning grooves 11 and the limiting rods 12, the installation speed of auxiliary part devices is improved, the tail end of the limiting rod 12 is fixedly connected with the quick-release plate 13, a limiting plate 14 is fixedly connected on the quick-release plate 13, a device clamping opening 15 is formed in the limiting plate 14, a first fixing ring 16 is fixedly connected in the device clamping opening 15, a second spring 17 is fixedly connected in the first fixing ring 16, and a second, first solid fixed ring 16, second spring 17 and the solid fixed ring 18 of second constitute fixture, and the solid fixed ring 16 of first solid fixed ring and the solid fixed ring 18 of second material be rubber, through the yielding characteristics of rubber material, can tightly fix auxiliary equipment in the solid fixed ring 18 of second, prevent auxiliary equipment overlength, only lean on buckle 10 can't make the stable condition of installing of auxiliary equipment.
The working principle is as follows: when the rapid inserting and pulling installation device for the auxiliary part of the unmanned aerial vehicle is used, the device is simply known, firstly, the device is installed on the unmanned aerial vehicle through a bolt arranged in a through hole 3, then a buckle 10 is pushed, in the process of pushing the buckle 10, a first spring 7 in a sleeve 6 is extruded through a backing plate 8, then auxiliary equipment is connected with a conductive block 4, as two groups of conductive blocks 4 are arranged on a support plate 1 and are respectively an anode and a cathode, and the conductive block 4 is connected with a power supply of the unmanned aerial vehicle through an external lead, at the moment, the auxiliary equipment is electrified, then the two groups of buckles 10 are loosened, the two groups of buckles 10 move inwards under the action of the first spring 7 to fix the auxiliary equipment without using a binding tape for installation, and the installation is firmer, secondly, two groups of positioning grooves 11 are symmetrically arranged on the support plate 1, two groups of limiting rods 12 are symmetrically arranged on a quick-release plate 13, the positioning grooves 11 correspond to the limiting rods 12 one by one, the positioning grooves 11 are connected with the limiting rods 12 in a matched mode, the quick-release plate 13 can be rapidly installed on the fixing plate 5, the quick-release plate is convenient to detach, the cross sections of the positioning grooves 11 and the cross sections of the limiting rods 12 are both in a T shape, when the quick-release plate 13 is installed, the quick-release plate 13 can be effectively prevented from shaking, then after the quick-release plate 13 is installed, the quick-release plate 13 is continuously pushed until the auxiliary equipment passes through the equipment clamping opening 15, the auxiliary equipment can be tightly fixed in the second fixing ring 18 through the deformable characteristic of rubber materials due to the fact that the materials of the first fixing ring 16 and the second fixing ring 18 are rubber, the situation that the auxiliary equipment is too long and cannot be stably installed by the buckles 10 is prevented, the impact force on the auxiliary equipment during flying of the unmanned aerial vehicle is relieved through the expansion and contraction of the, those not described in detail in this specification are within the skill of the art.
Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the invention.
Claims (6)
1. The utility model provides a quick plug installation device of unmanned aerial vehicle auxiliary, includes backup pad (1) and fixed plate (5), its characterized in that: the side surface of the supporting plate (1) is fixedly connected with an installation block (2), the installation block (2) is provided with a through hole (3), a conductive block (4) is fixedly connected above the supporting plate (1), wherein,
the inner side surface of the fixing plate (5) is fixedly connected with a sleeve (6), a first spring (7) is fixedly connected in the sleeve (6), a backing plate (8) is fixedly connected to the top end of the first spring (7), a supporting rod (9) is fixedly connected to the side surface of the backing plate (8), a buckle (10) is fixedly connected to the upper portion of the supporting rod (9), a positioning groove (11) is formed in the supporting plate (1), a limiting rod (12) is movably connected in the positioning groove (11), a quick-release plate (13) is fixedly connected to the tail end of the limiting rod (12), a limiting plate (14) is fixedly connected to the quick-release plate (13), an equipment clamping opening (15) is formed in the limiting plate (14), a first fixing ring (16) is fixedly connected in the equipment clamping opening (15), and a second spring (17) is fixedly connected in the first fixing ring (16, the tail end of the second spring (17) is fixedly connected with a second fixing ring (18).
2. The rapid inserting and pulling installation device for auxiliary parts of unmanned aerial vehicles according to claim 1, characterized in that: conducting block (4) are provided with two sets ofly on backup pad (1), are anodal and negative pole respectively, and conducting block (4) are connected with the unmanned aerial vehicle power through external conductor.
3. The rapid inserting and pulling installation device for auxiliary parts of unmanned aerial vehicles according to claim 1, characterized in that: the fixing plate (5), the sleeve (6), the first spring (7), the backing plate (8), the supporting rod (9) and the buckle (10) are symmetrically provided with two groups on the supporting plate (1), and the sum of the lengths of the two groups of sleeves (6), the first spring (7), the backing plate (8), the supporting rod (9) and the buckle (10) is larger than half of the length of the supporting plate (1).
4. The rapid inserting and pulling installation device for auxiliary parts of unmanned aerial vehicles according to claim 1, characterized in that: the outer diameter of the first spring (7) is the same as the inner diameter of the sleeve (6), and the length of the first spring (7) is smaller than the depth of the sleeve (6).
5. The rapid inserting and pulling installation device for auxiliary parts of unmanned aerial vehicles according to claim 1, characterized in that: the cross section of constant head tank (11) and gag lever post (12) is T shape, and constant head tank (11) symmetry is provided with two sets ofly on backup pad (1), and gag lever post (12) symmetry is provided with two sets ofly on quick detach board (13), constant head tank (11) and gag lever post (12) one-to-one.
6. The rapid inserting and pulling installation device for auxiliary parts of unmanned aerial vehicles according to claim 1, characterized in that: the first fixing ring (16), the second spring (17) and the second fixing ring (18) form a clamping mechanism, and the first fixing ring (16) and the second fixing ring (18) are made of rubber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021876813.4U CN213594545U (en) | 2020-09-01 | 2020-09-01 | Quick plug installation device of unmanned aerial vehicle auxiliary |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021876813.4U CN213594545U (en) | 2020-09-01 | 2020-09-01 | Quick plug installation device of unmanned aerial vehicle auxiliary |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213594545U true CN213594545U (en) | 2021-07-02 |
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ID=76585962
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021876813.4U Expired - Fee Related CN213594545U (en) | 2020-09-01 | 2020-09-01 | Quick plug installation device of unmanned aerial vehicle auxiliary |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213594545U (en) |
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2020
- 2020-09-01 CN CN202021876813.4U patent/CN213594545U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210702 |