CN208947630U - A kind of safeguard structure of unmanned plane camera - Google Patents
A kind of safeguard structure of unmanned plane camera Download PDFInfo
- Publication number
- CN208947630U CN208947630U CN201821751999.3U CN201821751999U CN208947630U CN 208947630 U CN208947630 U CN 208947630U CN 201821751999 U CN201821751999 U CN 201821751999U CN 208947630 U CN208947630 U CN 208947630U
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- China
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- fixedly connected
- bottom end
- unmanned plane
- damping spring
- guard ring
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Abstract
The utility model discloses a kind of safeguard structures of unmanned plane camera, including body and the guard ring for being located at organism bottom, four wing center bottoms are fixedly connected to buffer unit, the internal body of camera shooting both sides of head is opened up there are two groove, the top of two inside grooves is fixedly connected to the second damping spring, and the bottom end of two support columns is respectively fixedly connected with the two sides on guard ring top.The utility model is when body is encountered when barrier is fallen or landing is too fast; reduce certain impact force; remaining impact force passes to buffer unit; connecting column pushes up sliding block and slides in casing and compress the first damping spring; guard ring contacts ground; guard ring moves upwards; push support column; support column pushes limited block to slide in groove; limited block compresses the second damping spring; second damping spring further absorbs impact energy and is converted into elastic potential energy, further protects camera and body injury-free.
Description
Technical field
The utility model relates to a kind of safeguard structure, specially a kind of safeguard structure of unmanned plane camera.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently automatically operated by car-mounted computer.
Currently, unmanned plane using more and more extensive, the common people are usually shot with unmanned plane, unobscured, still
Due to fall or land when unmanned plane may touch barrier in flight it is too fast be easy to make camera and machine due to
With collision on the ground to be damaged, unnecessary damage is caused.Therefore we make improvement to this, propose a kind of unmanned plane camera
Safeguard structure.
Utility model content
To solve defect of the existing technology, the utility model provides a kind of safeguard structure of unmanned plane camera.
In order to solve the above-mentioned technical problem, the utility model provides the following technical solution:
A kind of safeguard structure of unmanned plane camera of the utility model, including body and the guard ring for being located at organism bottom,
The periphery wall of the body is equidistantly spaced there are four wing, and four wing tips are equipped with far from the side of body
Fan blade is gone up and down, is sequentially connected at the rotation center of the lifting fan blade with motor output shaft included inside wing, described in four
Wing center bottom is fixedly connected to buffer unit, and the center bottom of the body is fixedly connected with camera, the camera shooting
The internal body of both sides of head is opened up there are two groove, and the top of two inside grooves is fixedly connected to the second damping bullet
Spring, the bottom end of two second damping springs are elasticly connected with limited block, and the bottom end of two limited blocks is fixed to be connected
It is connected to support column, the bottom end of two support columns is respectively fixedly connected with the two sides on guard ring top.
As a kind of optimal technical scheme of the utility model, the buffer unit includes being fixedly connected with wing bottom end
Casing, the top inside described sleeve pipe are fixedly connected with the first damping spring, and the bottom end of first damping spring is fixedly connected
There is the sliding block to match with internal surface of sleeve pipe, the bottom end of the sliding block is fixedly connected with connecting column.
As a kind of optimal technical scheme of the utility model, the bottom end of the connecting column is fixedly connected with universal wheel.
As a kind of optimal technical scheme of the utility model, the side of the support column, which is embedded, is equipped with LED light, described
The inside of body is equipped with battery, and the LED light is electrically connected by light switch and battery.
As a kind of optimal technical scheme of the utility model, two avris of the guard ring respectively screw thread be plugged with hand twist
Screw, the bottom end of the body are equipped with the threaded hole to match with hand the turn of the screw.
As a kind of optimal technical scheme of the utility model, the outer wall of the body is coated with waterproof coating.
The beneficial effects of the utility model are: the safeguard structure of this kind of unmanned plane camera, encounters barrier when body and falls
When falling or when landing is too fast, universal wheel reduces certain impact force along ground taxi, and remaining impact force passes to buffer unit, even
It connects column and pushes up sliding block and the first damping spring is slided and compressed in casing, impact energy is converted elasticity by the first damping spring
Potential energy, to reduce body injury caused by impact, when impacting excessive, guard ring contacts ground, and guard ring is moved upwards, pushed away
Dynamic support column, support column push limited block to slide in groove, and limited block compresses the second damping spring, and the second damping spring is into one
Step absorbs impact energy and is converted into elastic potential energy, further protects camera and body injury-free.
Detailed description of the invention
Attached drawing is used to provide a further understanding of the present invention, and constitutes part of specification, practical with this
Novel embodiment is used to explain the utility model together, does not constitute limitations of the present invention.In the accompanying drawings:
Fig. 1 is a kind of structural schematic diagram of the safeguard structure of unmanned plane camera of the utility model；
Fig. 2 is a kind of buffer unit the schematic diagram of the section structure of the safeguard structure of unmanned plane camera of the utility model；
Fig. 3 is a kind of body the schematic diagram of the section structure of the safeguard structure of unmanned plane camera of the utility model；
Fig. 4 is a kind of guard ring structural schematic diagram of the safeguard structure of unmanned plane camera of the utility model；
Fig. 5 is a kind of electrical connection schematic diagram of the safeguard structure of unmanned plane camera of the utility model.
In figure: 1, body；2, wing；3, buffer unit；301, casing；302, the first damping spring；303, sliding block；304,
Connecting column；4, guard ring；5, camera；6, fan blade is gone up and down；7, universal wheel；8, support column；9, LED light；10, limited block；11, hand
The turn of the screw；12, the second damping spring；13, groove.
Specific embodiment
It is illustrated below in conjunction with preferred embodiment of the attached drawing to the utility model, it should be understood that described herein excellent
It selects embodiment to be only used for describing and explaining the present invention, is not used to limit the utility model.
Embodiment: shown in as shown in Figure 1, Figure 2, Fig. 3, Fig. 4 and Fig. 5, a kind of protection knot of unmanned plane camera of the utility model
Structure, including body 1 and the guard ring 4 for being located at 1 bottom of body, the periphery wall of body 1 is equidistantly spaced there are four wing 2,
Four 2 tops of wing are equipped with lifting fan blade 6 far from the side of body 1, go up and down at the rotation center of fan blade 6 and inside wing 2
Included motor output shaft transmission connection, four 2 center bottoms of wing are fixedly connected to buffer unit 3, in the bottom end of body 1
Portion is fixedly connected with camera 5, is opened up inside the body 1 of 5 two sides of camera there are two groove 13, the top inside two grooves 13
End is fixedly connected to the second damping spring 12, and the bottom end of two the second damping springs 12 is elasticly connected with limited block 10, and two
The bottom end of a limited block 10 is fixedly connected to support column 8, and the bottom end of two support columns 8 is respectively fixedly connected with pushes up in guard ring 4
The two sides at end.
Wherein, buffer unit 3 includes the casing 301 being fixedly connected with 2 bottom end of wing, and the top inside casing 301 is fixed
It is connected with the first damping spring 302, the bottom end of the first damping spring 302 is fixedly connected with the cunning to match with 301 inner wall of casing
Block 303, the bottom end of sliding block 303 are fixedly connected with connecting column 304, and when device is fallen, connecting column 304 receives impact, push up
Movable slider 303 compresses the first damping spring 302, and impact energy is converted elastic potential energy by the first damping spring 302, to reduce punching
The damage of body 1 caused by hitting.
Wherein, the bottom end of connecting column 304 is fixedly connected with universal wheel 7, facilitates landing.
Wherein, the side of support column 8, which is embedded, is equipped with LED light 9, and the inside of body 1 is equipped with battery, and LED light 9 passes through photograph
Bright switch is electrically connected with battery, makes to shoot apparent.
Wherein, screw thread is plugged with hand the turn of the screw 11 to two avris of guard ring 4 respectively, and the bottom end of body 1, which is equipped with, twists spiral shell with hand
The threaded hole that silk 11 matches pushes guard ring 4 to move to body 1, the second damping spring 12 is compressed, support column 8 is taken in
In machine groove 13, hand the turn of the screw 11 is rotated, guard ring 4 is fixed on to the bottom end of body 1, it is convenient for collecting.
Wherein, the outer wall of body 1 is coated with waterproof coating, and body 1 is avoided to make moist.
When work, the included motor driven lifting fan blade 6 when 1 flight of body inside wing 2 is rotated, and keeps body 1 flat
Steady flight, when body 1 is encountered when barrier is fallen or landing is too fast, universal wheel 7 reduces certain impact along ground taxi
Power, remaining impact force pass to buffer unit 3, and connecting column 304 pushes up sliding block 303 and slides in casing 301 and compress first
Impact energy is converted elastic potential energy by damping spring 302, the first damping spring 302, so that body injury caused by impact is reduced,
When impacting excessive, guard ring 4 contacts ground, and guard ring 4 moves upwards, and pushes support column 8, and support column 8 pushes limited block 10
It is slided in groove 13, limited block 10 compresses the second damping spring 12, and the second damping spring 12 further absorbs impact energy and turns
Elastic potential energy is turned to, further protects camera 5 and body 1 injury-free, the LED light 9 on support column 8 can be in light environment
It illumination is provided after when darker, is more clear the picture of shooting, the bottom end of body 1 is equipped with to match with hand the turn of the screw 11
Threaded hole pushes guard ring 4 to move to body 1, the second damping spring 12 is compressed, and support column 8 is taken in machine groove 13, turns
It starts the turn of the screw 11, guard ring 4 is fixed on to the bottom end of body 1, it is convenient for collecting.
Finally, it should be noted that the above descriptions are merely preferred embodiments of the present invention, it is not limited to this
Utility model, although the utility model is described in detail with reference to the foregoing embodiments, for those skilled in the art
For, it is still possible to modify the technical solutions described in the foregoing embodiments, or to part of technical characteristic
It is equivalently replaced.Within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on,
It should be included within the scope of protection of this utility model.
Claims (6)
1. a kind of safeguard structure of unmanned plane camera, which is characterized in that including body (1) and be located at the anti-of body (1) bottom
Guard ring (4), the periphery wall of the body (1) are equidistantly spaced there are four wing (2), and four wing (2) tops are remote
The disembark side of body (1) is equipped with lifting fan blade (6), at the rotation center of lifting fan blade (6) with it is included inside wing (2)
Motor output shaft transmission connection, four wing (2) center bottoms are fixedly connected to buffer unit (3), the body
(1) center bottom is fixedly connected with camera (5), opens up that there are two grooves inside the bodies (1) of camera (5) two sides
(13), two internal tops of the groove (13) are fixedly connected to the second damping spring (12), two second dampings
The bottom end of spring (12) is elasticly connected with limited block (10), and the bottom end of two limited blocks (10) is fixedly connected to support
Column (8), the bottom end of two support columns (8) are respectively fixedly connected in the two sides on guard ring (4) top.
2. a kind of safeguard structure of unmanned plane camera according to claim 1, which is characterized in that the buffer unit
It (3) include the casing (301) being fixedly connected with wing (2) bottom end, the internal top of described sleeve pipe (301) is fixedly connected with first
Damping spring (302), the bottom end of first damping spring (302) are fixedly connected with the cunning to match with casing (301) inner wall
The bottom end of block (303), the sliding block (303) is fixedly connected with connecting column (304).
3. a kind of safeguard structure of unmanned plane camera according to claim 2, which is characterized in that the connecting column
(304) bottom end is fixedly connected with universal wheel (7).
4. a kind of safeguard structure of unmanned plane camera according to claim 1, which is characterized in that the support column (8)
Side be embedded and be equipped with LED light (9), the inside of the body (1) is equipped with battery, and the LED light (9) passes through light switch
It is electrically connected with battery.
5. a kind of safeguard structure of unmanned plane camera according to claim 1, which is characterized in that the guard ring (4)
Two avris screw thread is plugged with hand the turn of the screw (11) respectively, the bottom end of the body (1) is equipped with to match with hand the turn of the screw (11)
Threaded hole.
6. a kind of safeguard structure of unmanned plane camera according to claim 1, which is characterized in that the body (1)
Outer wall is coated with waterproof coating.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821751999.3U CN208947630U (en) | 2018-10-29 | 2018-10-29 | A kind of safeguard structure of unmanned plane camera |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821751999.3U CN208947630U (en) | 2018-10-29 | 2018-10-29 | A kind of safeguard structure of unmanned plane camera |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208947630U true CN208947630U (en) | 2019-06-07 |
Family
ID=66743192
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821751999.3U Expired - Fee Related CN208947630U (en) | 2018-10-29 | 2018-10-29 | A kind of safeguard structure of unmanned plane camera |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208947630U (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110375881A (en) * | 2019-09-03 | 2019-10-25 | 国网河北能源技术服务有限公司 | A kind of distributed fiber temperature measuring device and its temp measuring system |
| CN110879056A (en) * | 2019-12-04 | 2020-03-13 | 山东省国土测绘院 | Unmanned aerial vehicle mapping system |
| CN111994294A (en) * | 2020-09-10 | 2020-11-27 | 赣州毫厘测绘信息技术有限公司 | Unmanned aerial vehicle measures camera protective structure |
| CN112591127A (en) * | 2021-01-27 | 2021-04-02 | 杭州优旗贸易有限公司 | Safety landing device for protecting camera during unmanned aerial vehicle fault |
| CN112706914A (en) * | 2021-01-25 | 2021-04-27 | 北京中联国成科技有限公司 | Helicopter undercarriage with protection function |
| CN113148151A (en) * | 2021-03-11 | 2021-07-23 | 江西水星勘测院有限公司 | Survey and use unmanned aerial vehicle with safety cover structure |
| CN113479322A (en) * | 2021-08-24 | 2021-10-08 | 浙江迪澳普地理信息技术有限公司 | Environment monitoring unmanned aerial vehicle |
| CN113566990A (en) * | 2021-08-24 | 2021-10-29 | 鑫国集团有限公司 | Stabilize intelligent temperature transmitter of low-power consumption |
-
2018
- 2018-10-29 CN CN201821751999.3U patent/CN208947630U/en not_active Expired - Fee Related
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110375881A (en) * | 2019-09-03 | 2019-10-25 | 国网河北能源技术服务有限公司 | A kind of distributed fiber temperature measuring device and its temp measuring system |
| CN110879056A (en) * | 2019-12-04 | 2020-03-13 | 山东省国土测绘院 | Unmanned aerial vehicle mapping system |
| CN110879056B (en) * | 2019-12-04 | 2022-01-07 | 山东省国土测绘院 | Unmanned aerial vehicle mapping system |
| CN111994294A (en) * | 2020-09-10 | 2020-11-27 | 赣州毫厘测绘信息技术有限公司 | Unmanned aerial vehicle measures camera protective structure |
| CN112706914A (en) * | 2021-01-25 | 2021-04-27 | 北京中联国成科技有限公司 | Helicopter undercarriage with protection function |
| CN112591127A (en) * | 2021-01-27 | 2021-04-02 | 杭州优旗贸易有限公司 | Safety landing device for protecting camera during unmanned aerial vehicle fault |
| CN113148151A (en) * | 2021-03-11 | 2021-07-23 | 江西水星勘测院有限公司 | Survey and use unmanned aerial vehicle with safety cover structure |
| CN113479322A (en) * | 2021-08-24 | 2021-10-08 | 浙江迪澳普地理信息技术有限公司 | Environment monitoring unmanned aerial vehicle |
| CN113566990A (en) * | 2021-08-24 | 2021-10-29 | 鑫国集团有限公司 | Stabilize intelligent temperature transmitter of low-power consumption |
| CN113479322B (en) * | 2021-08-24 | 2024-04-09 | 浙江迪澳普地理信息技术有限公司 | Environment monitoring unmanned aerial vehicle |
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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: 20190607 Termination date: 20201029 |