CN211033000U - Unmanned aerial vehicle with safeguard function - Google Patents
Unmanned aerial vehicle with safeguard function Download PDFInfo
- Publication number
- CN211033000U CN211033000U CN201921435872.5U CN201921435872U CN211033000U CN 211033000 U CN211033000 U CN 211033000U CN 201921435872 U CN201921435872 U CN 201921435872U CN 211033000 U CN211033000 U CN 211033000U
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- China
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- aerial vehicle
- unmanned aerial
- protection
- fixedly connected
- vehicle body
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Abstract
The utility model discloses an unmanned aerial vehicle with safeguard function, including the unmanned aerial vehicle body, the equal fixedly connected with buffer in the left and right sides of unmanned aerial vehicle body bottom, the equal fixedly connected with protector in four corners department at unmanned aerial vehicle body top, buffer includes the mounting panel, the right side fixedly connected with fixed block of mounting panel bottom, the back of fixed block is rotated through the loose axle and is connected with the atress pole. The utility model discloses a mutually supporting between mounting panel, fixed block, loose axle, atress pole, gyro wheel, dead lever, buffer spring, installation pole, bearing, safety cover, central disc, guard slot, slider, fender rod, rubber guard ring and the protection spring has realized an unmanned aerial vehicle with protect function, can follow diversified the device and carry out effectual protection to such as unmanned aerial vehicle's side and bottom, avoid the damage because of accident causes the device itself to the life of this device has been increased.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle with safeguard function.
Background
The unmanned plane is an unmanned plane which is operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, compared with the unmanned plane, the unmanned plane is more suitable for tasks too dull, dirty or dangerous, is provided with no cockpit on the plane, but is provided with an autopilot, a program control device and other devices, and personnel on the ground, a naval vessel or a mother machine remote control station track, position, remotely control, telemeter and digitally transmit the unmanned plane through radar and other devices, can take off like a common plane under the remote control of radio or launch and lift off by using a boosting rocket, and can also take the mother machine to the air to launch and fly.
When the unmanned aerial vehicle is recovered, the unmanned aerial vehicle can automatically land in the same way as a common aircraft in the landing process, and can also be recovered by a parachute or a barrier net through remote control, the existing unmanned aerial vehicle is not particularly expensive, but the unmanned aerial vehicle flying to the sky also needs protective measures, if the unmanned aerial vehicle is not well operated, the unmanned aerial vehicle easily collides with a large building or birds to cause machine damage, or when the unmanned aerial vehicle is out of control, the unmanned aerial vehicle also can cause the machine body to fall down and damage the unmanned aerial vehicle, the existing unmanned aerial vehicle does not have corresponding protective measures, and the occurrence of collision damage is easy to happen.
SUMMERY OF THE UTILITY MODEL
In order to solve the problem the utility model provides an unmanned aerial vehicle with safeguard function.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle with a protection function comprises an unmanned aerial vehicle body, wherein the left side and the right side of the bottom of the unmanned aerial vehicle body are fixedly connected with buffer devices, and the four corners of the top of the unmanned aerial vehicle body are fixedly connected with protection devices;
the buffering device comprises an installation plate, a fixed block is fixedly connected to the right side of the bottom of the installation plate, the back of the fixed block is rotatably connected with a stress rod through a movable shaft, a roller is arranged on one side, away from the fixed block, of the stress rod, a fixed rod is fixedly connected to the bottom of the installation plate and located on the left side of the fixed block, a buffering spring is fixedly connected to the bottom of the right side of the fixed rod, and one side, close to the stress rod, of the buffering spring is fixedly connected with the buffering;
the protection device comprises an installation rod, the top of the installation rod is connected with a protection cover through a bearing in a rotating mode, the protection cover comprises a central disc, the edge of the central disc is provided with a protection groove which is arranged equidistantly, the inner wall of the protection groove is connected with a sliding block matched with the sliding block in a sliding mode, the sliding block is far away from one side of the protection groove, one side of the protection rod far away from the sliding block runs through the protection groove and extends to the outside of the protection groove, one end of the four protection rods far away from the sliding block passes through a rubber protection ring fixed connection, and a protection spring is sleeved on the surface of the protection rod outside the protection groove.
Preferably, the top of mounting panel and the bottom fixed connection of unmanned aerial vehicle body.
Preferably, the top fixed connection of the bottom unmanned aerial vehicle body of installation pole.
Preferably, the number of the protective grooves is four, and the protective grooves are arranged at the edge of the central disk at equal intervals.
Preferably, one side of the protection spring close to the central disk is fixedly connected with the central disk.
Preferably, one side of the protection spring close to the rubber protection ring is fixedly connected with the rubber protection ring.
Compared with the prior art, the beneficial effects of the utility model are as follows:
the utility model discloses an unmanned aerial vehicle body, mounting panel, fixed block, loose axle, atress pole, gyro wheel, dead lever, buffer spring, installation pole, bearing, safety cover, central disc, guard slot, slider, guard bar, mutually supporting between rubber guard ring and the protection spring, realized an unmanned aerial vehicle with protect function, can follow diversified the device and carry out effectual protection such as unmanned aerial vehicle's side and bottom, avoid the damage that causes the device itself because of the accident to the life of this device has been increased.
Drawings
Fig. 1 is a schematic structural view of a front view of the present invention;
fig. 2 is a schematic structural diagram of a top view of the present invention;
fig. 3 is a schematic structural view of a front view of the buffering device of the present invention;
fig. 4 is a schematic structural view of a front view of the protection device of the present invention;
fig. 5 is a schematic structural diagram of a top view of the protective cover of the present invention;
fig. 6 is a structural sectional view of a top view of the protective cover of the present invention;
fig. 7 is a partial enlarged view of a-a in fig. 6 according to the present invention.
In the figure: 1 unmanned aerial vehicle body, 2 buffer, 201 mounting panel, 202 fixed block, 203 loose axle, 204 atress pole, 205 gyro wheel, 206 dead lever, 207 buffer spring, 3 protector, 301 installation pole, 302 bearing, 303 safety cover, 3031 central disc, 3032 guard groove, 3033 slider, 3034 guard bar, 3035 rubber guard ring, 3036 protection spring.
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.
Please refer to fig. 1-2, an unmanned aerial vehicle with a protection function comprises an unmanned aerial vehicle body 1, wherein a buffer device 2 is fixedly connected to the left side and the right side of the bottom of the unmanned aerial vehicle body 1, and a protection device 3 is fixedly connected to the four corners of the top of the unmanned aerial vehicle body 1.
Referring to fig. 1-3, the buffering device 2 includes a mounting plate 201, the top of the mounting plate 201 is fixedly connected to the bottom of the main body 1 of the unmanned aerial vehicle, the right side of the bottom of the mounting plate 201 is fixedly connected to a fixed block 202, the back of the fixed block 202 is rotatably connected to a stress rod 204 through a movable shaft 203, a roller 205 is disposed on one side of the stress rod 204 away from the fixed block 202, the bottom of the mounting plate 201 is fixedly connected to a fixed rod 206 on the left side of the fixed block 202, a buffering spring 207 is fixedly connected to the bottom on the right side of the fixed rod 206, and one side of the buffering spring.
Referring to fig. 1 to 7, the protection device 3 includes a mounting rod 301, the top of the bottom drone body 1 of the mounting rod 301 is fixedly connected to the top of the mounting rod 301, the top of the mounting rod 301 is rotatably connected to a protection cover 303 through a bearing 302, the protection cover 303 includes a central disk 3031, protection grooves 3032 are arranged at the edge of the central disk 3031 at equal intervals, the number of the protection grooves 3032 is four, the protection grooves 3032 are arranged at the edge of the central disk 3031 at equal intervals, a sliding block 3033 adapted to the protection grooves 3032 is slidably connected to the inner wall of the protection grooves 3032, a protection rod 3034 is fixedly connected to one side of the sliding block 3033 far away from the protection groove 3032, one side of the protection rod 3034 far away from the sliding block 3033 penetrates through the protection groove 3032 and extends to the outside of the protection groove 3032, one end of the four protection rods 3034 far away from the sliding block 3035 is fixedly connected to a rubber ring 3035 in a sleeving manner, a, protection spring 3036 is close to one side of rubber protection circle 3035 rather than fixed connection, through unmanned aerial vehicle body 1, mounting panel 201, fixed block 202, loose axle 203, stress rod 204, gyro wheel 205, dead lever 206, buffer spring 207, installation pole 301, bearing 302, safety cover 303, central disc 3031, protective slot 3032, slider 3033, protective rod 3034, mutually support between rubber protection circle 3035 and protection spring 3036, an unmanned aerial vehicle with protect function has been realized, can follow diversified protection to the device such as unmanned aerial vehicle's side and bottom, avoid because of the unexpected damage that leads to the fact itself to the device, thereby the life of this device has been increased.
During the use, this device can effectually reduce the produced impact force of device when vertical direction whereabouts through setting up buffer 2, consequently can effectively protect unmanned aerial vehicle to when unmanned aerial vehicle meets accident and appears turning on one's side, can effectually avoid organism and rotating vane to receive the damage through setting up protector 3, thereby can realize increasing its life to the multi-angle protection of unmanned aerial vehicle body 1.
In summary, the following steps: this unmanned aerial vehicle with safeguard function through setting up unmanned aerial vehicle body 1, mounting panel 201, fixed block 202, loose axle 203, atress pole 204, gyro wheel 205, dead lever 206, buffer spring 207, installation pole 301, bearing 302, safety cover 303, central disc 3031, guard slot 3032, slider 3033, guard bar 3034, rubber guard ring 3035 and guard spring 3036, has solved the problem that the background art mentioned.
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 invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides an unmanned aerial vehicle with safeguard function, includes unmanned aerial vehicle body (1), its characterized in that: the left side and the right side of the bottom of the unmanned aerial vehicle body (1) are both fixedly connected with a buffer device (2), and four corners of the top of the unmanned aerial vehicle body (1) are both fixedly connected with a protective device (3);
the buffer device (2) comprises a mounting plate (201), a fixed block (202) is fixedly connected to the right side of the bottom of the mounting plate (201), the back of the fixed block (202) is rotatably connected with a stress rod (204) through a movable shaft (203), a roller (205) is arranged on one side, away from the fixed block (202), of the stress rod (204), a fixed rod (206) is fixedly connected to the bottom of the mounting plate (201) and located on the left side of the fixed block (202), a buffer spring (207) is fixedly connected to the bottom of the right side of the fixed rod (206), and one side, close to the stress rod (204), of the buffer spring (207) is fixedly connected with the stress rod;
the protection device (3) comprises a mounting rod (301), the top of the mounting rod (301) is rotatably connected with a protection cover (303) through a bearing (302), the protection cover (303) comprises a central disc (3031), protection grooves (3032) are arranged at the edge of the central disc (3031) at equal intervals, a sliding block (3033) matched with the protection groove (3032) is connected to the inner wall of the protection groove (3032) in a sliding mode, one side, far away from the protection groove (3032), of the sliding block (3033) is fixedly connected with protection rods (3034), one side, far away from the sliding block (3033), of the protection rods (3034) penetrates through the protection groove (3032) and extends to the outside of the protection groove, one ends, far away from the sliding block (3033), of the four protection rods (3034) are fixedly connected through rubber protection rings (3035), and a spring (3036) is sleeved on the surface of the protection rods (3034) located outside.
2. The unmanned aerial vehicle with safeguard function of claim 1, characterized in that: the top of mounting panel (201) and the bottom fixed connection of unmanned aerial vehicle body (1).
3. The unmanned aerial vehicle with safeguard function of claim 1, characterized in that: the top fixed connection of bottom unmanned aerial vehicle body (1) of installation pole (301).
4. The unmanned aerial vehicle with safeguard function of claim 1, characterized in that: the number of the protective grooves (3032) is four, and the protective grooves are arranged at the edge of the central disc (3031) at equal intervals.
5. The unmanned aerial vehicle with safeguard function of claim 1, characterized in that: one side of the protection spring (3036) close to the central disc (3031) is fixedly connected with the central disc.
6. The unmanned aerial vehicle with safeguard function of claim 1, characterized in that: one side of the protection spring (3036) close to the rubber protection ring (3035) is fixedly connected with the rubber protection ring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921435872.5U CN211033000U (en) | 2019-08-31 | 2019-08-31 | Unmanned aerial vehicle with safeguard function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921435872.5U CN211033000U (en) | 2019-08-31 | 2019-08-31 | Unmanned aerial vehicle with safeguard function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211033000U true CN211033000U (en) | 2020-07-17 |
Family
ID=71540206
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921435872.5U Expired - Fee Related CN211033000U (en) | 2019-08-31 | 2019-08-31 | Unmanned aerial vehicle with safeguard function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211033000U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112723186A (en) * | 2020-12-16 | 2021-04-30 | 中联重科股份有限公司 | Buffer device, crane boom and crane |
-
2019
- 2019-08-31 CN CN201921435872.5U patent/CN211033000U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112723186A (en) * | 2020-12-16 | 2021-04-30 | 中联重科股份有限公司 | Buffer device, crane boom and crane |
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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: 20200717 Termination date: 20210831 |