CN215972081U - Unmanned aerial vehicle with quick detach formula horn structure - Google Patents
Unmanned aerial vehicle with quick detach formula horn structure Download PDFInfo
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- CN215972081U CN215972081U CN202122656290.3U CN202122656290U CN215972081U CN 215972081 U CN215972081 U CN 215972081U CN 202122656290 U CN202122656290 U CN 202122656290U CN 215972081 U CN215972081 U CN 215972081U
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Abstract
The utility model discloses an unmanned aerial vehicle with a quick-dismantling type horn structure, which belongs to the field of unmanned aerial vehicle connection and comprises a horn body and an unmanned aerial vehicle body, wherein the horn body is installed on the unmanned aerial vehicle body, the horn body and the unmanned aerial vehicle body are detachably connected through a clamping device, the clamping device comprises an upper clamping part and a lower clamping part, the upper clamping part is arranged on the upper side and the lower side of the horn body and the unmanned aerial vehicle body by being attached to the lower clamping part, a positioning piece is fixedly connected to one side of the upper clamping part facing downwards, a positioning groove is formed in one side of the lower clamping part facing upwards, the positioning piece is inserted into the positioning groove, a fixing device is connected to the side wall of the lower clamping part, and the fixing device is detachably connected with the positioning piece after penetrating through the groove wall of the positioning groove. The utility model has the advantages that the quick disassembly and assembly mode is adopted to replace the direct fixing modes such as welding and the like to overhaul the horn, thereby reducing the overhaul difficulty and not easily damaging the unmanned aerial vehicle structure.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle connection, in particular to an unmanned aerial vehicle with a quick-release type horn structure.
Background
An unmanned vehicle is an unmanned vehicle operated by a radio remote control device and a self-contained program control device, and is a general name of unmanned vehicles in fact. Unmanned aerial vehicle usage is extensive, is applied to multiple aerial operations, like aerial camera shooting, fire control rescue, military shooting etc.. In the prior art, a connecting pipe of a fuselage part of an unmanned aerial vehicle is directly fixed with a horn by welding and the like.
The above prior art has the following disadvantages: when the damage takes place in the unmanned aerial vehicle and need repair or inspect, because it adopts the mode of direct fixation such as welding, be difficult to directly overhaul it under the condition that does not cause unmanned aerial vehicle structure to damage, this problem is waited for to solve urgently.
SUMMERY OF THE UTILITY MODEL
Aiming at the defects in the prior art, the utility model aims to provide the unmanned aerial vehicle with the quick-disassembly type horn structure, which has the advantages that the horn is overhauled by adopting a quick-disassembly mode to replace a direct fixing mode such as welding and the like, so that the overhauling difficulty is reduced, and the damage to the unmanned aerial vehicle structure is not easy to cause.
The utility model provides an unmanned aerial vehicle with quick detach formula horn structure, includes horn body and unmanned aerial vehicle fuselage, the horn body is installed on the unmanned aerial vehicle fuselage, can dismantle through clamping device between horn body and the unmanned aerial vehicle fuselage and be connected, clamping device includes clamping part and lower clamping part, it is set up in by the laminating of clamping part down in the upper and lower both sides of horn body and unmanned aerial vehicle fuselage to go up the clamping part, go up clamping part one side fixedly connected with setting element down, the constant head tank has been seted up to clamping part one side up down, the setting element is pegged graft in the constant head tank, be connected with fixing device down on the clamping part lateral wall, fixing device can dismantle with the setting element after passing the cell wall of constant head tank and be connected.
The utility model is further configured to: go up the mounting groove of having seted up on the clamping part, the setting element top set up in the mounting groove and with the tank bottom fixed connection of mounting groove, the setting element bottom is stretched out by the notch of mounting groove, be provided with reset spring around the setting element in the mounting groove, reset spring bottom mounting is on the clamping part down, reset spring is under the original length state the setting element bottom is located the notch top of constant head tank.
The utility model is further configured to: the unmanned aerial vehicle comprises an unmanned aerial vehicle body and is characterized in that a first abdicating groove is formed in the unmanned aerial vehicle body, a second abdicating groove is formed in the unmanned aerial vehicle body, the first abdicating groove and the second abdicating groove are spliced together, the upper clamping part and the lower clamping part are positioned in the first abdicating groove and the second abdicating groove when being spliced with each other, and the groove depth of the first abdicating groove and the second abdicating groove is equal to the thickness of the upper clamping part and the lower clamping part.
The utility model is further configured to: the horn body is towards unmanned aerial vehicle fuselage one end fixedly connected with connecting piece, the spread groove has been seted up towards horn body one end to the unmanned aerial vehicle fuselage, the connecting piece is pegged graft in the spread groove.
The utility model is further configured to: the connecting piece is the dovetail piece that sets up along the horizontal direction, the unmanned aerial vehicle fuselage is located the spread groove top and has seted up the cell body of stepping down, the cell body of stepping down communicates with the spread groove, the length, the width and the height and the connecting piece homoenergetic of spread groove equal.
The utility model is further configured to: one end of the fixing device is provided with a handle, and the other end of the fixing device penetrates through the positioning piece and then is in threaded connection with the groove wall of the positioning groove.
The utility model is further configured to: go up clamping part and lower clamping part and horn body and unmanned aerial vehicle fuselage contact department facility and have the rubber pad.
When this body coupling of horn is on the unmanned aerial vehicle fuselage in needs, make the connecting piece on the horn body insert the notch department of the cell body of stepping down, then make it wholly move down, connecting piece embedding spread groove this moment, will go up clamping part and lower clamping part and remove to first groove and the second groove department of stepping down, reset spring is in the original long state this moment, the setting element is located outside the notch of constant head tank, then will go up the clamping part and clamp part pressfitting together down, reset spring is in compression state this moment, the setting element inserts in the constant head tank, it screws up to make fixing device pass setting element and constant head tank opposite side cell wall in proper order after, accomplish the connection process of horn body and unmanned aerial vehicle fuselage. When horn body and unmanned aerial vehicle fuselage were dismantled to needs, loosened fixing device, reset spring resumes original length, and in the setting element shifted out the constant head tank, then will loosen last clamping part and lower clamping part remove on the unmanned aerial vehicle fuselage, make the connecting piece shift out by stepping down the cell body behind the rebound horn body to inspect and repair in the unmanned aerial vehicle fuselage, need not to destroy its structure itself.
In conclusion, the utility model has the following beneficial effects:
1. through the clamping device consisting of the upper clamping part and the lower clamping part, the arm body and the unmanned aerial vehicle body can be simply and conveniently disassembled and assembled so as to conveniently overhaul the interior of the unmanned aerial vehicle;
2. through the arrangement of the mounting groove and the reset spring, the upper clamping part and the lower clamping part are unfolded under the unfixed state and are moved to the unmanned aerial vehicle body;
3. through connecting piece, spread groove and the setting of the cell body of stepping down, can carry out simple and convenient location to horn body and unmanned aerial vehicle fuselage to subsequent with hold the device fixed.
Drawings
FIG. 1 is a schematic structural view for embodying the entirety of the present invention;
FIG. 2 is a schematic structural view of the present invention for showing the fitting relationship between the upper clamping portion and the lower clamping portion;
FIG. 3 is a schematic view of the structure for embodying the coupling member and the coupling groove in the present invention;
fig. 4 is an enlarged view of a portion a in fig. 2.
In the figure, 1, a machine arm body; 11. a first abdicating groove; 12. a connecting member; 2. an unmanned aerial vehicle body; 21. a second abdicating groove; 22. connecting grooves; 23. a yielding groove body; 3. a clamping device; 31. an upper clamping portion; 311. mounting grooves; 312. a positioning member; 313. a return spring; 32. a lower clamping portion; 321. positioning a groove; 322. a fixing device; 323. a handle; 33. and (7) a rubber pad.
Detailed Description
The present invention is further described in detail below with reference to the attached drawings, and other advantages and effects of the present invention will be easily understood by those skilled in the art from the disclosure of the present specification. In the present specification, the terms "upper", "lower", "left", "right" and "middle" are used for clarity of description, and are not intended to limit the scope of the present invention, and changes or modifications in the relative relationship may be made without substantial technical changes and modifications.
Example (b):
as shown in fig. 1 and 2, the unmanned aerial vehicle with the quick-release type horn structure designed in the present invention includes a horn body 1 and an unmanned aerial vehicle body 2, the horn body 1 is installed on the unmanned aerial vehicle body 2, the horn body 1 and the unmanned aerial vehicle body 2 are detachably connected through a clamping device 3, the clamping device 3 includes an upper clamping portion 31 and a lower clamping portion 32, the upper clamping portion 31 is disposed on the upper and lower sides of the horn body 1 and the unmanned aerial vehicle body 2 by being attached to the lower clamping portion 32, a positioning member 312 is fixedly connected to one side of the upper clamping portion 31 facing downward, a positioning groove 321 is disposed on one side of the lower clamping portion 32 facing upward, the positioning member 312 is inserted into the positioning groove 321, a fixing device 322 is connected to a side wall of the lower clamping portion 32, and the fixing device 322 is detachably connected to the positioning member 312 after passing through a groove wall of the positioning groove 321.
As shown in fig. 2 and 4, an installation groove 311 is formed in the upper clamping portion 31, the top end of the positioning element 312 is disposed in the installation groove 311 and is fixedly connected to the bottom of the installation groove 311, the bottom end of the positioning element 312 extends out of the notch of the installation groove 311, a return spring 313 is disposed in the installation groove 311 around the positioning element 312, the bottom end of the return spring 313 is fixed to the lower clamping portion 32, and the bottom end of the positioning element 312 is located above the notch of the positioning groove 321 in the original length state of the return spring 313. When the return spring 313 is compressed, the positioning element 312 is inserted into the positioning slot 321, the fixing device 322 passes through the positioning element 312 and the slot wall of the positioning slot 321, one end of the fixing device 322 is formed with a handle 323, and the other end passes through the positioning element 312 and then is in threaded connection with the slot wall of the positioning slot 321.
As shown in fig. 2 and 3, a first abdicating groove 11 has been provided on the horn body 1, a second abdicating groove 21 has been provided on the unmanned aerial vehicle fuselage 2, the first abdicating groove 11 and the second abdicating groove 21 are spliced together, the upper clamping portion 31 and the lower clamping portion 32 are positioned in the first abdicating groove 11 and the second abdicating groove 21 when being spliced together, and the groove depth of the first abdicating groove 11 and the second abdicating groove 21 is equal to the thickness of the upper clamping portion 31 and the lower clamping portion 32. The horn body 1 has connecting piece 12 towards 2 one end fixedly connected with of unmanned aerial vehicle fuselage, and spread groove 22 has been seted up towards 1 one end of horn body to unmanned aerial vehicle fuselage 2, and connecting piece 12 is pegged graft in spread groove 22. Connecting piece 12 is the forked tail piece that sets up along the horizontal direction, and unmanned aerial vehicle fuselage 2 is located the connecting groove 22 top and has seted up the cell body 23 of stepping down, steps down cell body 23 and connecting groove 22 intercommunication, and the length, the width and the height of connecting groove 22 all equal with connecting piece 12. When connecting horn body 1 and unmanned aerial vehicle fuselage 2, make connecting piece 12 insert in the cell body 23 of stepping down, then make horn body 1 move down, connecting piece 12 imbeds in spread groove 22 to subsequent fixed process who goes up clamping part 31 and lower clamping part 32. Go up clamping part 31 and lower clamping part 32 and horn body 1 and unmanned aerial vehicle fuselage 2 contact department facility and have rubber pad 33, be difficult for causing horn body 1 and unmanned aerial vehicle fuselage 2 surface to produce mar or damage in the centre gripping process.
The implementation principle of the above-mentioned embodiment is for stepping down when needing to connect horn body 1 on unmanned aerial vehicle fuselage 2, make connecting piece 12 on the horn body 1 insert the notch department of the cell body 23 of stepping down, then make it move down wholly, connecting piece 12 imbeds in the spread groove 22 this moment, it moves first groove 11 and the second groove 21 of stepping down to go up clamping part 31 and lower clamping part 32, reset spring 313 is in the primary state this moment, setting element 312 is located outside the notch of constant head tank 321, then it is in the same place with the pressure of lower clamping part 32 with last clamping part 31, reset spring 313 is in compression state this moment, setting element 312 inserts in constant head tank 321, make fixing device 322 pass setting element 312 and screw up behind the constant head tank 321 opposite side cell wall in proper order, accomplish the connection process of horn body 1 and unmanned aerial vehicle fuselage 2. When horn body 1 and unmanned aerial vehicle fuselage 2 are dismantled to needs, loosen fixing device 322, reset spring 313 resumes original length, and setting element 312 shifts out in the constant head tank 321, then will loosen last clamping part 31 and lower clamping part 32 remove to unmanned aerial vehicle fuselage 2 on, make connecting piece 12 shift out by stepping down in the cell body 23 behind the rebound horn body 1 to inspect and repair in the unmanned aerial vehicle fuselage 2, need not to destroy its structure itself.
The present embodiment is only for explaining the present invention, and it is not limited to the present invention, and those skilled in the art can make modifications of the present embodiment without inventive contribution as needed after reading the present specification, but all of them are protected by patent law within the scope of the claims of the present invention.
Claims (7)
1. The utility model provides an unmanned aerial vehicle with quick detach formula horn structure which characterized in that: comprises a horn body (1) and an unmanned aerial vehicle body (2), wherein the horn body (1) is arranged on the unmanned aerial vehicle body (2), the arm body (1) is detachably connected with the unmanned aerial vehicle body (2) through a clamping device (3), the clamping device (3) comprises an upper clamping part (31) and a lower clamping part (32), the upper clamping part (31) is attached to the upper side and the lower side of the arm body (1) and the unmanned aerial vehicle body (2) by the lower clamping part (32), a positioning piece (312) is fixedly connected with the downward side of the upper clamping part (31), a positioning groove (321) is arranged on the upward side of the lower clamping part (32), the positioning piece (312) is inserted in the positioning groove (321), the side wall of the lower clamping part (32) is connected with a fixing device (322), and the fixing device (322) penetrates through the groove wall of the positioning groove (321) and then is detachably connected with the positioning piece (312).
2. The unmanned aerial vehicle with quick detach formula horn structure of claim 1, its characterized in that: go up mounting groove (311) on clamping part (31) seted up, setting element (312) top set up in mounting groove (311) and with the tank bottom fixed connection of mounting groove (311), setting element (312) bottom is stretched out by the notch of mounting groove (311), it is provided with reset spring (313) to surround setting element (312) in mounting groove (311), reset spring (313) bottom mounting is on clamping part (32) down, reset spring (313) are in the original state down setting element (312) bottom is located the notch top of constant head tank (321).
3. The unmanned aerial vehicle with quick detach formula horn structure of claim 2 characterized in that: seted up first groove (11) of stepping down on horn body (1), the second groove (21) of stepping down has been seted up on unmanned aerial vehicle fuselage (2), first groove (11) of stepping down and second groove (21) amalgamation together, go up clamping part (31) and lower clamping part (32) and lie in first groove (11) of stepping down and second groove (21) of stepping down when amalgamation each other, the groove depth of first groove (11) of stepping down and second groove (21) of stepping down equals with the thickness homonymy of last clamping part (31) and lower clamping part (32).
4. The unmanned aerial vehicle with quick detach formula horn structure of claim 1, its characterized in that: the unmanned aerial vehicle is characterized in that the connecting piece (12) is fixedly connected to the arm body (1) towards one end of the unmanned aerial vehicle body (2), the connecting groove (22) is formed in the unmanned aerial vehicle body (2) towards one end of the arm body (1), and the connecting piece (12) is inserted into the connecting groove (22).
5. The unmanned aerial vehicle with quick detach formula horn structure of claim 4, its characterized in that: connecting piece (12) is the dovetail piece that sets up along the horizontal direction, unmanned aerial vehicle fuselage (2) are located spread groove (22) top and have been seted up and have been stepped down cell body (23), step down cell body (23) and spread groove (22) intercommunication, the length, the width and the height and connecting piece (12) homonymy of spread groove (22).
6. The unmanned aerial vehicle with quick detach formula horn structure of claim 2 characterized in that: one end of the fixing device (322) is provided with a handle (323), and the other end of the fixing device penetrates through the positioning piece (312) and then is in threaded connection with the groove wall of the positioning groove (321).
7. The unmanned aerial vehicle with quick detach formula horn structure of claim 4, its characterized in that: go up clamping part (31) and lower clamping part (32) and horn body (1) and unmanned aerial vehicle fuselage (2) contact department and be provided with rubber pad (33).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122656290.3U CN215972081U (en) | 2021-11-02 | 2021-11-02 | Unmanned aerial vehicle with quick detach formula horn structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122656290.3U CN215972081U (en) | 2021-11-02 | 2021-11-02 | Unmanned aerial vehicle with quick detach formula horn structure |
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| Publication Number | Publication Date |
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| CN215972081U true CN215972081U (en) | 2022-03-08 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202122656290.3U Active CN215972081U (en) | 2021-11-02 | 2021-11-02 | Unmanned aerial vehicle with quick detach formula horn structure |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116062169A (en) * | 2022-12-12 | 2023-05-05 | 国网青海省电力公司海北供电公司 | Multipurpose unmanned aerial vehicle spraying device |
-
2021
- 2021-11-02 CN CN202122656290.3U patent/CN215972081U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116062169A (en) * | 2022-12-12 | 2023-05-05 | 国网青海省电力公司海北供电公司 | Multipurpose unmanned aerial vehicle spraying device |
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