CN216332724U - Unmanned aerial vehicle is with frame that plays convenient to installation - Google Patents
Unmanned aerial vehicle is with frame that plays convenient to installation Download PDFInfo
- Publication number
- CN216332724U CN216332724U CN202122538163.3U CN202122538163U CN216332724U CN 216332724 U CN216332724 U CN 216332724U CN 202122538163 U CN202122538163 U CN 202122538163U CN 216332724 U CN216332724 U CN 216332724U
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- Prior art keywords
- block
- unmanned aerial
- aerial vehicle
- landing gear
- groove
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- 238000009434 installation Methods 0.000 title claims abstract description 20
- 230000000087 stabilizing effect Effects 0.000 claims abstract description 13
- 238000007789 sealing Methods 0.000 claims description 22
- 230000003014 reinforcing effect Effects 0.000 claims description 9
- 238000000034 method Methods 0.000 claims description 8
- 239000002184 metal Substances 0.000 claims description 3
- 238000011900 installation process Methods 0.000 abstract description 3
- 230000002035 prolonged effect Effects 0.000 abstract description 3
- 238000005457 optimization Methods 0.000 description 5
- 230000008569 process Effects 0.000 description 5
- 239000000428 dust Substances 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a landing frame convenient to install for an unmanned aerial vehicle, which comprises the unmanned aerial vehicle, wherein the two sides of the bottom of the unmanned aerial vehicle are respectively provided with an undercarriage, the front side and the rear side of the top of the surface of the undercarriage are respectively and fixedly connected with a connecting block, four corners of the bottom of the unmanned aerial vehicle are respectively and fixedly connected with a fixed block, the back of each fixed block is provided with a fixed groove in sliding connection with the corresponding connecting block, the top and the bottom of the inner wall of each fixed groove are respectively provided with a stabilizing groove, and the front side of the inner wall of each stabilizing groove is provided with a fastening groove. According to the utility model, by arranging the unmanned aerial vehicle, the landing gear, the connecting block, the fixing groove, the stabilizing groove, the fastening groove and the fastening sleeve, the problems that the existing landing gear is complicated in the installation process with the unmanned aerial vehicle, a user needs to fix a plurality of bolts and the bottom of the unmanned aerial vehicle through a tool, the installation time of the user is greatly prolonged, and the convenience of the user in installation is reduced are solved.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a landing frame for an unmanned aerial vehicle, which is convenient to install.
Background
The undercarriage is the buffering support that unmanned aerial vehicle takes off and falls, but current undercarriage is comparatively loaded down with trivial details at the process of installing with unmanned aerial vehicle, needs the user to fix a plurality of bolt and unmanned aerial vehicle's bottom through the instrument, and such operation greatly increased user's installation time, convenience when having reduced the user installation.
SUMMERY OF THE UTILITY MODEL
In order to solve the problems in the background art, the utility model aims to provide a landing gear for an unmanned aerial vehicle, which is convenient to install, has the advantage of convenience in installation, and solves the problems that the existing landing gear is complicated in the installation process with the unmanned aerial vehicle, and a user needs to fix a plurality of bolts with the bottom of the unmanned aerial vehicle through tools, so that the installation time of the user is greatly prolonged, and the convenience of the user in installation is reduced.
In order to achieve the purpose, the utility model provides the following technical scheme: a landing frame for an unmanned aerial vehicle convenient to install comprises the unmanned aerial vehicle;
the both sides of unmanned aerial vehicle bottom all are provided with the undercarriage, the front side and the equal fixedly connected with connecting block in rear side at undercarriage surperficial top, the equal fixedly connected with fixed block in four corners of unmanned aerial vehicle bottom, the fixed slot with connecting block sliding connection is seted up at the back of fixed block, the stable groove has all been seted up to the top and the bottom of fixed slot inner wall, the fastening groove has been seted up to the front side of stable inslot wall, the inner wall fixedly connected with adapter sleeve in fastening groove, the back of fixed block is provided with the grip block, the front of grip block and the equal fixedly connected with fastening block in front side of fixed slot inner wall, the front and the back of connecting block all set up with fastening block swing joint's spread groove, the opening has all been seted up to the front and the back of undercarriage, the front of grip block pass the opening and with the inner wall contact of adapter sleeve.
Preferably, the surface of the clamping block is sleeved with a reinforcing block, and one side of the reinforcing block, which is close to the undercarriage, is fixedly connected with the surface of the undercarriage.
Preferably, a sealing gasket is fixedly connected to the surface of the clamping block, and the front surface of the sealing gasket is in contact with the back surface of the fixing block.
Preferably, a buffer sleeve is fixedly connected to the surface of the landing gear, and the thickness of the buffer sleeve is one centimeter.
Preferably, the fastening block is made of metal, and the side of the fastening block close to the landing gear is in a circular arc shape.
Preferably, the front side and the rear side of the top of the surface of the landing gear are fixedly connected with sealing rings, and the bottoms of the fixing blocks and the bottoms of the sealing gaskets are in contact with the tops of the sealing rings.
Compared with the prior art, the utility model has the following beneficial effects:
1. according to the utility model, by arranging the unmanned aerial vehicle, the landing gear, the connecting block, the fixing groove, the stabilizing groove, the fastening groove and the fastening sleeve, the problems that the existing landing gear is complicated in the installation process with the unmanned aerial vehicle, a user needs to fix a plurality of bolts and the bottom of the unmanned aerial vehicle through a tool, the installation time of the user is greatly prolonged, and the convenience of the user in installation is reduced are solved.
2. According to the utility model, the stability of the clamping block and the undercarriage can be improved by arranging the reinforcing block, so that the clamping block and the undercarriage are connected more tightly.
3. According to the utility model, the sealing gasket is arranged, so that the back surface of the fixing block can be sealed, and external dust is prevented from entering the fixing groove.
4. According to the utility model, the bottom of the undercarriage can be buffered by arranging the buffer sleeve, so that the bottom of the undercarriage is prevented from directly contacting with the ground, and the stability of the undercarriage is improved.
5. According to the utility model, one side of the fastening block, which is close to the undercarriage, is set to be in the shape of a circular arc, so that the fastening block can be stably clamped into the connecting groove, and the fastening block and the connecting block are stably connected.
6. According to the utility model, the bottom of the fixing block can be sealed by arranging the sealing ring, so that external dust is prevented from entering the fixing groove from the stabilizing groove, and the sealing property of the stabilizing groove is improved.
Drawings
FIG. 1 is a schematic front view of the structure of the present invention;
FIG. 2 is a right side view of the fixing block of the present invention;
FIG. 3 is a right side sectional view of the structural mounting block of the present invention;
fig. 4 is a perspective view of a structural clamping block of the present invention.
In the figure: 1. an unmanned aerial vehicle; 2. a landing gear; 3. connecting blocks; 4. a fixed block; 5. fixing grooves; 6. a stabilizing slot; 7. a fastening groove; 8. fastening sleeves; 9. a clamping block; 10. a fastening block; 11. connecting grooves; 12. a port; 13. a reinforcing block; 14. a gasket; 15. a buffer sleeve; 16. and (5) sealing rings.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
As shown in fig. 1 to 4, the landing frame for the unmanned aerial vehicle, provided by the utility model, comprises an unmanned aerial vehicle 1;
the both sides of 1 bottom of unmanned aerial vehicle all are provided with undercarriage 2, the front side and the equal fixedly connected with connecting block 3 in rear side at 2 surperficial tops of undercarriage, the equal fixedly connected with fixed block 4 in four corners of 1 bottom of unmanned aerial vehicle, fixed slot 5 with 3 sliding connection of connecting block is seted up at the back of fixed block 4, stable groove 6 has all been seted up with the bottom at the top of fixed slot 5 inner wall, fastening groove 7 has been seted up to the front side of stable groove 6 inner wall, the inner wall fixedly connected with adapter sleeve 8 of fastening groove 7, the back of fixed block 4 is provided with grip block 9, the front of grip block 9 and the equal fixedly connected with anchor block 10 in front side of fixed slot 5 inner wall, connecting groove 11 with anchor block 10 swing joint is all seted up at the front and the back of connecting block 3, opening 12 has all been seted up at undercarriage 2's front and the back, grip block 9 openly pass opening 12 and with the inner wall contact of adapter sleeve 8.
Referring to fig. 3, the surface of the clamping block 9 is sleeved with a reinforcing block 13, and one side of the reinforcing block 13 close to the undercarriage 2 is fixedly connected with the surface of the undercarriage 2.
As a technical optimization scheme of the utility model, the stability of the clamping block 9 and the undercarriage 2 can be improved by arranging the reinforcing block 13, so that the clamping block 9 and the undercarriage 2 are connected more tightly.
Referring to fig. 2, a sealing gasket 14 is fixedly connected to a surface of the clamping block 9, and a front surface of the sealing gasket 14 is in contact with a back surface of the fixing block 4.
As a technical optimization scheme of the present invention, the sealing gasket 14 is provided to seal the back surface of the fixing block 4, thereby preventing external dust from entering the fixing groove 5.
Referring to fig. 1, a cushion sleeve 15 is fixedly attached to the surface of the landing gear 2, and the thickness of the cushion sleeve 15 is one centimeter.
As a technical optimization scheme of the utility model, the bottom of the undercarriage 2 can be buffered by arranging the buffer sleeve 15, so that the bottom of the undercarriage 2 is prevented from directly contacting the ground, and the stability of the undercarriage 2 is improved.
Referring to fig. 3, the side of the fastening block 10 close to the landing gear 2 is in the shape of a circular arc, the fastening block 10 being made of metal.
As a technical optimization scheme of the utility model, one side of the fastening block 10 close to the undercarriage 2 is set to be in a circular arc shape, so that the fastening block 10 can be stably clamped into the connecting groove 11, and the fastening block 10 and the connecting block 3 are stably connected.
Referring to fig. 3, the front side and the rear side of the top of the surface of the landing gear 2 are fixedly connected with a sealing ring 16, and the bottom of the fixing block 4 and the bottom of the sealing gasket 14 are in contact with the top of the sealing ring 16.
As a technical optimization scheme of the utility model, the bottom of the fixing block 4 can be sealed by arranging the sealing ring 16, so that external dust is prevented from entering the fixing groove 5 from the stabilizing groove 6, and the sealing property of the stabilizing groove 6 is improved.
The working principle and the using process of the utility model are as follows: when the landing gear fixing device is used, a user firstly plugs the connecting block 3 into the fixing groove 5 from the fixing groove 5 on the back of the fixing block 4, then the surface of the landing gear 2 slides forwards in the stabilizing groove 6, the connecting groove 11 on the front side of the connecting block 3 is rigidly connected with the fastening block 10 on the front side of the inner wall of the fixing groove 5, the connecting block 3 is contacted with the front side of the inner wall of the fixing groove 5, meanwhile, the front side of the landing gear 2 is contacted with the front side of the inner wall of the stabilizing groove 6, then, after the user aligns the fastening block 10 on the front side of the clamping block 9 with the connecting groove 11 on the back side of the connecting block 3, the clamping block 9 is pressed, the clamping block 9 pushes the fastening block 10 to be clamped into the connecting groove 11, the clamping block 9 is connected with the connecting block 3, meanwhile, the front side of the clamping block 9 can penetrate through the through hole 12 to enter the inside of the fastening groove 7, and the landing gear 2 is limited by the clamping block 9, and then the front of the clamping block 9 is extruded with the inner wall of the fastening sleeve 8, so that the surface of the clamping block 9 is connected with the inner wall of the fastening sleeve 8, thereby achieving the effect of convenient installation.
In summary, the following steps: this unmanned aerial vehicle is with frame that rises convenient to installation, through setting up unmanned aerial vehicle 1, undercarriage 2, connecting block 3, fixed block 4, fixed slot 5, stable groove 6, fastening groove 7 and adapter sleeve 8's cooperation is used, it is comparatively loaded down with trivial details at the process of installing with unmanned aerial vehicle to have solved current undercarriage, it is fixed with a plurality of bolt and unmanned aerial vehicle's bottom to need the user to pass through the instrument, such operation greatly increased user's installation time, the problem of convenience when having reduced the user installation.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. A landing gear for an unmanned aerial vehicle, which is convenient to install, comprises an unmanned aerial vehicle (1);
the method is characterized in that: the unmanned aerial vehicle is characterized in that both sides of the bottom of the unmanned aerial vehicle (1) are provided with landing gears (2), the front side and the rear side of the top of the surface of each landing gear (2) are fixedly connected with a connecting block (3), four corners of the bottom of the unmanned aerial vehicle (1) are fixedly connected with fixing blocks (4), the back of each fixing block (4) is provided with a fixing groove (5) in sliding connection with the corresponding connecting block (3), the top and the bottom of the inner wall of each fixing groove (5) are provided with stabilizing grooves (6), the front side of the inner wall of each stabilizing groove (6) is provided with a fastening groove (7), the inner wall of each fastening groove (7) is fixedly connected with a fastening sleeve (8), the back of each fixing block (4) is provided with a clamping block (9), the front of each clamping block (9) and the front side of the inner wall of each fixing groove (5) are fixedly connected with a fastening block (10), the front and the back of each connecting block (3) are provided with connecting grooves (11) movably connected with the fastening blocks (10), opening (12) have all been seted up to the front and the back of undercarriage (2), the front of grip block (9) passes opening (12) and contacts with the inner wall of adapter sleeve (8).
2. The landing gear for unmanned aerial vehicle convenient to installation of claim 1, wherein: the surface cover of grip block (9) is equipped with reinforcing block (13), one side that reinforcing block (13) are close to undercarriage (2) is connected with the fixed surface of undercarriage (2).
3. The landing gear for unmanned aerial vehicle convenient to installation of claim 1, wherein: the surface of the clamping block (9) is fixedly connected with a sealing gasket (14), and the front surface of the sealing gasket (14) is in contact with the back surface of the fixing block (4).
4. The landing gear for unmanned aerial vehicle convenient to installation of claim 1, wherein: the surface of the landing gear (2) is fixedly connected with a buffer sleeve (15), and the thickness of the buffer sleeve (15) is one centimeter.
5. The landing gear for unmanned aerial vehicle convenient to installation of claim 1, wherein: one side, close to the landing gear (2), of the fastening block (10) is arc-shaped, and the fastening block (10) is made of metal.
6. The landing gear for unmanned aerial vehicle convenient to installation of claim 3, wherein: the landing gear is characterized in that a sealing ring (16) is fixedly connected to the front side and the rear side of the top of the surface of the landing gear (2), and the bottom of the fixing block (4) and the bottom of the sealing gasket (14) are in contact with the top of the sealing ring (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122538163.3U CN216332724U (en) | 2021-10-21 | 2021-10-21 | Unmanned aerial vehicle is with frame that plays convenient to installation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122538163.3U CN216332724U (en) | 2021-10-21 | 2021-10-21 | Unmanned aerial vehicle is with frame that plays convenient to installation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216332724U true CN216332724U (en) | 2022-04-19 |
Family
ID=81178376
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122538163.3U Expired - Fee Related CN216332724U (en) | 2021-10-21 | 2021-10-21 | Unmanned aerial vehicle is with frame that plays convenient to installation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216332724U (en) |
-
2021
- 2021-10-21 CN CN202122538163.3U patent/CN216332724U/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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220419 |