CN214325370U - Unmanned aerial vehicle machine oar convenient to change - Google Patents
Unmanned aerial vehicle machine oar convenient to change Download PDFInfo
- Publication number
- CN214325370U CN214325370U CN202120047615.5U CN202120047615U CN214325370U CN 214325370 U CN214325370 U CN 214325370U CN 202120047615 U CN202120047615 U CN 202120047615U CN 214325370 U CN214325370 U CN 214325370U
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- unmanned aerial
- aerial vehicle
- fixing seat
- change
- convenient
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Abstract
The utility model relates to a dull and stereotyped shell makes technical field, specifically is an unmanned aerial vehicle machine oar convenient to change, including the unmanned aerial vehicle body, the unmanned aerial vehicle camera has been installed in the front of unmanned aerial vehicle body, the unmanned aerial vehicle horn has been installed to the side of unmanned aerial vehicle body, and installs the grout fixing base on the top of unmanned aerial vehicle horn, the flexible piece of second has been installed to the bottom of unmanned aerial vehicle body, and the flexible piece of first flexible piece has been installed on the surface of second, the descending base has been installed to the bottom of first flexible piece. The utility model discloses be provided with first dismantlement button and second and dismantle the button, dismantle the button through pressing first dismantlement button and second to make fixing pin can't fix in the inside of thick liquid fixing base at the block, can dismantle the change with the thick liquid body through this mode, can cushion the impact force that produces through the fifth spring, can prevent effectively through this mode that the inside of unmanned aerial vehicle body leads to the part impaired because of receiving the impact.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle machine oar convenient to change.
Background
With the continuous progress of modern science and technology, more and more fields begin to use unmanned aerial vehicles to replace people to complete some specific works, and the application of unmanned aerial vehicles provides much convenience.
Usually in order to ensure the stability of unmanned aerial vehicle flight, can install on unmanned aerial vehicle and establish multiunit aircraft thick liquid, and the aircraft thick liquid is mostly fixed through the welded mode, but because unmanned aerial vehicle various accident can appear in difficult the meeting of exempting when using, need change the aircraft thick liquid sometimes, the welded fixed mode leads to the unmanned aerial vehicle aircraft thick liquid to be inconvenient dismantles the change, and when unmanned aerial vehicle when descending bottom and ground contact, inside part can receive the impact in difficult the avoiding, easily cause the damage of internals, consequently, need a unmanned aerial vehicle aircraft oar convenient to change to solve above-mentioned problem urgently.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle machine oar convenient to change to solve the inconvenient problem that dismantles the change and the impact that unmanned aerial vehicle received when descending easily causes the internals to damage of unmanned aerial vehicle machine thick liquid that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle oar convenient to replace comprises an unmanned aerial vehicle body, wherein an unmanned aerial vehicle camera is arranged on the front face of the unmanned aerial vehicle body, an unmanned aerial vehicle arm is arranged on the side face of the unmanned aerial vehicle body, a slurry fixing seat is arranged at the top end of the unmanned aerial vehicle arm, a first disassembly button is inserted into the side face of the slurry fixing seat, a first spring is arranged on the surface of the first disassembly button, a second disassembly button is inserted into the side face of the slurry fixing seat, a second spring is arranged on the surface of the second disassembly button, the top end of the slurry fixing seat is provided with a slurry body, a fixing bolt is arranged at the bottom end of the slurry body, a first fixing clamping block is arranged inside the fixing bolt, a third spring is arranged on the side face of the first fixing clamping block, a second fixing clamping block is arranged inside the fixing bolt, and a fourth spring is arranged on the side face of the second fixing clamping block, the flexible piece of second has been installed to the bottom of unmanned aerial vehicle body, and the flexible piece of first flexible piece has been installed on the surface of second, the fifth spring is installed to the inside of first flexible piece, descending base has been installed to the bottom of first flexible piece.
Preferably, a circular groove is formed in the top end of the machine pulp fixing seat, and the inside of the machine pulp fixing seat and the fixing bolt form a sliding type structure.
Preferably, a circular hole groove is formed in the side face of the machine pulp fixing seat, and the side face of the machine pulp fixing seat and the surface of the first disassembly button form a sliding type structure.
Preferably, a circular hole groove is formed in the side face of the machine pulp fixing seat, and the side face of the machine pulp fixing seat and the surface of the second disassembly button form a sliding type structure.
Preferably, a circular groove is formed in the machine pulp fixing seat, and the inside of the machine pulp fixing seat and the first fixing clamping block form a clamping structure.
Preferably, a circular groove is formed in the machine pulp fixing seat, and the inside of the machine pulp fixing seat and the second fixing clamping block form a clamping structure.
Preferably, the inner diameter of the first telescopic block is larger than the surface diameter of the second telescopic block, and the inner part of the first telescopic block and the surface of the second telescopic block form a sliding structure.
Compared with the prior art, the beneficial effects of the utility model are that: this unmanned aerial vehicle machine oar convenient to change is provided with first dismantlement button and second dismantlement button, dismantles the button through pressing first dismantlement button and second to make fixing pin can't fix in the inside of quick-witted thick liquid fixing base at the block, can dismantle the change with the quick-witted thick liquid body through this mode, can cushion the impact force that produces through the fifth spring, can effectively prevent through this mode that the inside of unmanned aerial vehicle body leads to the part impaired because of receiving the impact.
(1) The device is provided with first dismantlement button and second dismantlement button, dismantles the button through pressing first dismantlement button and second for the fixed fixture block of first fixed fixture block and second can contract toward fixed bolt's inside, thereby makes fixed bolt can't be fixed in the inside of thick liquid fixing base at the block, can dismantle the change with the thick liquid body through this mode.
(2) The device installs the fifth spring through the bottom at the unmanned aerial vehicle body, when the unmanned aerial vehicle body descends to the ground, can cushion the impact force that produces through the fifth spring, can prevent effectively through this mode that the inside of unmanned aerial vehicle body leads to the part impaired because of receiving the impact.
Drawings
FIG. 1 is a schematic sectional view of the front view of the structure of the present invention;
FIG. 2 is a schematic front view of the structure of the present invention;
fig. 3 is a schematic front sectional view of the first, second and fifth spring structures of the present invention;
fig. 4 is an enlarged schematic view of a structure in fig. 1 according to the present invention.
In the figure: 1. an unmanned aerial vehicle body; 101. an unmanned aerial vehicle camera; 102. an unmanned aerial vehicle arm; 2. a machine pulp fixing seat; 201. a first disassembly button; 202. a first spring; 203. a second disassembly button; 204. a second spring; 3. a machine pulp body; 301. fixing the bolt; 302. a first fixed fixture block; 303. a third spring; 304. a second fixed fixture block; 305. a fourth spring; 4. a first telescopic block; 401. a second telescopic block; 402. a fifth spring; 5. and (5) descending the base.
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. 1-4, the present invention provides an embodiment: an unmanned aerial vehicle oar convenient to replace comprises an unmanned aerial vehicle body 1, wherein an unmanned aerial vehicle camera 101 is arranged on the front surface of the unmanned aerial vehicle body 1, an unmanned aerial vehicle arm 102 is arranged on the side surface of the unmanned aerial vehicle body 1, a mortar fixing seat 2 is arranged at the top end of the unmanned aerial vehicle arm 102, a circular groove is formed in the top end of the mortar fixing seat 2, the inside of the mortar fixing seat 2 and a fixing bolt 301 form a sliding structure, a circular hole groove is formed in the side surface of the mortar fixing seat 2, the side surface of the mortar fixing seat 2 and the surface of a first disassembly button 201 form a sliding structure, a circular hole groove is formed in the side surface of the mortar fixing seat 2, the side surface of the mortar fixing seat 2 and the surface of a second disassembly button 203 form a sliding structure, a circular groove is formed in the inside of the mortar fixing seat 2, and the inside of the mortar fixing seat 2 and a first fixing fixture block 302 form a clamping structure, a circular groove is formed inside the machine pulp fixing seat 2, and the inside of the machine pulp fixing seat 2 and the second fixing fixture block 304 form a clamping structure. A first dismounting button 201 is inserted into the side of the machine pulp fixing seat 2, a first spring 202 is arranged on the surface of the first dismounting button 201, a second dismounting button 203 is inserted into the side of the machine pulp fixing seat 2, and a second spring 204 is arranged on the surface of the second dismounting button 203.
The top end of the machine pulp fixing seat 2 is provided with the machine pulp body 3, the bottom end of the machine pulp body 3 is provided with a fixing bolt 301, a first fixing fixture block 302 is arranged inside the fixing bolt 301, a third spring 303 is arranged on the side surface of the first fixing fixture block 302, a second fixing fixture block 304 is arranged inside the fixing bolt 301, a fourth spring 305 is arranged on the side surface of the second fixing fixture block 304, a second telescopic block 401 is arranged at the bottom end of the unmanned aerial vehicle body 1, a first telescopic block 4 is arranged on the surface of the second telescopic block 401, the inner diameter of the first telescopic block 4 is larger than the surface diameter of the second telescopic block 401, a sliding structure is formed by the inner portion of the first telescopic block 4 and the surface of the second telescopic block 401, a fifth spring 402 is arranged inside the first telescopic block 4, and a landing base 5 is arranged at the bottom end of the first telescopic block 4.
The working principle is as follows: during the use, when needing to dismantle the change with quick-witted thick liquid body 3, according to fig. 1, can make it slide in quick-witted thick liquid fixed seat 2's inside through pressing first dismantlement button 201 and second dismantlement button 203, can conflict first fixed fixture block 302 and second fixed fixture block 304 through first dismantlement button 201 and second dismantlement button 203, make first fixed fixture block 302 and second fixed fixture block 304 can contract towards the inside of fixed bolt 301 through the conflict to first fixed fixture block 302 and second fixed fixture block 304 for fixed bolt 301 no longer blocks in the inside of quick-witted thick liquid fixed seat 2, can dismantle quick-witted thick liquid body 3 from the top of quick-witted thick liquid fixed seat 2 through this mode.
When needs prevent that unmanned aerial vehicle body 1 is inside to receive the impact and impaired when descending, according to figure 1, through installing the flexible piece 401 of second in unmanned aerial vehicle body 1's bottom, and install first flexible piece 4 on the surface of the flexible piece 401 of second, through installing fifth spring 402 in the inside at first flexible piece 4, make unmanned aerial vehicle body 1 when descending subaerial, can cushion the impact force that produces through fifth spring 402, can effectively slow down the loss that the impact force led to the fact unmanned aerial vehicle body 1 internals through this mode, can prevent effectively that unmanned aerial vehicle body 1's inside from receiving the damage.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein, and any reference signs in the claims are not intended to be construed as limiting the claim concerned.
Claims (7)
1. The utility model provides an unmanned aerial vehicle oar convenient to change, includes unmanned aerial vehicle body (1), its characterized in that: the front of the unmanned aerial vehicle body (1) is provided with an unmanned aerial vehicle camera (101), the side of the unmanned aerial vehicle body (1) is provided with an unmanned aerial vehicle arm (102), the top end of the unmanned aerial vehicle arm (102) is provided with a mortar fixing seat (2), the side of the mortar fixing seat (2) is inserted with a first disassembly button (201), the surface of the first disassembly button (201) is provided with a first spring (202), the side of the mortar fixing seat (2) is inserted with a second disassembly button (203), the surface of the second disassembly button (203) is provided with a second spring (204), the top end of the mortar fixing seat (2) is provided with a mortar body (3), the bottom end of the mortar body (3) is provided with a fixing bolt (301), the inside of the fixing bolt (301) is provided with a first fixing clamping block (302), and the side of the first fixing clamping block (302) is provided with a third spring (303), fixed fixture block (304) of second have been installed to the inside of dead bolt (301), and fourth spring (305) have been installed to the side of the fixed fixture block of second (304), flexible piece (401) of second have been installed to the bottom of unmanned aerial vehicle body (1), and first flexible piece (4) have been installed on the surface of the flexible piece of second (401), fifth spring (402) are installed to the inside of first flexible piece (4), descending base (5) have been installed to the bottom of first flexible piece (4).
2. The unmanned aerial vehicle oar convenient to change of claim 1, characterized in that: a circular groove is formed in the top end of the machine pulp fixing seat (2), and the inside of the machine pulp fixing seat (2) and the fixing bolt (301) form a sliding type structure.
3. The unmanned aerial vehicle oar convenient to change of claim 1, characterized in that: circular hole grooves are formed in the side face of the machine pulp fixing seat (2), and the side face of the machine pulp fixing seat (2) and the surface of the first disassembling button (201) form a sliding type structure.
4. The unmanned aerial vehicle oar convenient to change of claim 1, characterized in that: a circular hole groove is formed in the side face of the machine pulp fixing seat (2), and the side face of the machine pulp fixing seat (2) and the surface of the second disassembly button (203) form a sliding type structure.
5. The unmanned aerial vehicle oar convenient to change of claim 1, characterized in that: a circular groove is formed in the machine pulp fixing seat (2), and the inside of the machine pulp fixing seat (2) and the first fixing fixture block (302) form a clamping structure.
6. The unmanned aerial vehicle oar convenient to change of claim 1, characterized in that: a circular groove is formed in the machine pulp fixing seat (2), and the inside of the machine pulp fixing seat (2) and the second fixing clamping block (304) form a clamping structure.
7. The unmanned aerial vehicle oar convenient to change of claim 1, characterized in that: the inner diameter of the first telescopic block (4) is larger than the surface diameter of the second telescopic block (401), and the inner part of the first telescopic block (4) and the surface of the second telescopic block (401) form a sliding structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120047615.5U CN214325370U (en) | 2021-01-08 | 2021-01-08 | Unmanned aerial vehicle machine oar convenient to change |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120047615.5U CN214325370U (en) | 2021-01-08 | 2021-01-08 | Unmanned aerial vehicle machine oar convenient to change |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214325370U true CN214325370U (en) | 2021-10-01 |
Family
ID=77905490
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120047615.5U Expired - Fee Related CN214325370U (en) | 2021-01-08 | 2021-01-08 | Unmanned aerial vehicle machine oar convenient to change |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214325370U (en) |
-
2021
- 2021-01-08 CN CN202120047615.5U patent/CN214325370U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20211001 Termination date: 20220108 |
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| CF01 | Termination of patent right due to non-payment of annual fee |