CN209290688U - A kind of camera shooting unmanned plane with protection and landing shock-absorbing function - Google Patents
A kind of camera shooting unmanned plane with protection and landing shock-absorbing function Download PDFInfo
- Publication number
- CN209290688U CN209290688U CN201821697040.6U CN201821697040U CN209290688U CN 209290688 U CN209290688 U CN 209290688U CN 201821697040 U CN201821697040 U CN 201821697040U CN 209290688 U CN209290688 U CN 209290688U
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- CN
- China
- Prior art keywords
- rotor bodies
- buffer disc
- unmanned plane
- buffer
- bottom plate
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Abstract
The utility model discloses a kind of with the camera shooting unmanned plane for protecting and landing shock-absorbing function, including more rotor bodies, and the circumferential direction of the buffer disc is connected with the guard ring of annular by supporting mechanism, and guard ring is socketed in the outside of the wing of more rotor bodies.It is transmitted to buffer disc, and buffer disc is connected by the bottom plate and more rotor bodies of spring and upside, spring just plays the role of damping, buffering in this way, slow down impact, it and is multi-party bit buffering, wing and more rotor bodies are protected well, spring is symmetrically arranged with multiple, balance is compared to the stress of buffer disc in this way, increase stability, when landing, buffer disc contacts ground, the support rod of surrounding is played a supporting role, it prevents from turning on one's side, and at this time, spring plays buffer function, the internal structure of more rotor bodies is protected well, it plays a protective role during flight in this way, play the role of buffer protection in landing again, function is richer, it is more practical.
Description
Technical field
The utility model relates to protect field of shock absorption to camera shooting unmanned plane, and in particular to one kind there is protection and landing to subtract
Shake the camera shooting unmanned plane of function.
Background technique
For unmanned plane shoot, we are very familiar with for this, this is relatively common, for example, clap propaganda film, need to building from
Eminence shooting, also some shoots mountain topography.Also have in the market very much, for example notification number is the patent of CN205707396U,
And for fields such as some forest fire protection security protections, it is also desirable to, in order to improve service life, much add protection mechanism, such as public
Accuse number for CN206679273U " the utility model discloses a kind of collision prevention of unmanned plane during flying devices, including sucker, cross machine
Structure, support tube and shielded closure mechanism, the top of the sucker are equipped with the cross mechanism, and the side of the cross mechanism is equipped with institute
Support tube is stated, one end of the support tube is equipped with the shielded closure mechanism, and the cross mechanism includes link block and the first screw thread
Bar, the link block carry out be bonded with the sucker, and one end of the link block and first threaded rod is welded, described
First threaded rod is threadedly coupled with the support tube.The collision prevention of unmanned plane during flying device, is not only simple in structure, and installs
It is convenient, elastic deformation is occurred in collision by steel ring, unmanned plane is sufficiently protected, convenient for be decomposed into multiple structures into
Row assembling, greatly facilitating the collision prevention of unmanned plane during flying device with this can be mounted on the unmanned plane of different size ", still, it
It can only protect, and cannot accomplish damping of landing, have a single function.
Utility model content
The protection mechanism having the technical problem to be solved by the utility model is to camera shooting unmanned plane in the market only has
Protective action does not have shock-absorbing function, has a single function.
To achieve the goals above, technical solution provided by the utility model is: a kind of have protection and landing damping function
The camera shooting unmanned plane of energy, including more rotor bodies, the upper end of more rotor bodies are fixed with camera, more rotor bodies
Lower end in the middle part of be fixed with bottom plate, and the downside of bottom plate is connected with parallel horizontally disposed buffer disc by buffer gear；
The circumferential direction of the buffer disc is connected with the guard ring of annular by supporting mechanism, and guard ring is socketed in more gyroplanes
The outside of the wing of body.
Preferably, the bottom plate and buffer disc are in disk form, and bottom plate is bonded in the lower end of more rotor bodies.It is preferred that
, the buffer gear includes the spring being fixed between bottom plate and buffer disc, and spring is arranged about the axisymmetrical of bottom plate
Have multiple.
Preferably, the supporting mechanism includes the outside support rod for being fixed on buffer disc circumferential direction at equal intervals, and support rod
Free end be fixedly connected by upward connecting rod with the guard ring of upside.
Preferably, arc transition between the support rod and connecting rod.
The utility model design, when encountering barrier, guard ring contacts first, to protect wing, guard ring contact with
Afterwards, impact force is transmitted to connecting rod, through support rod, is transmitted to buffer disc, and buffer disc passes through the bottom plate and more rotors of spring and upside
Body connection, such spring just play the role of damping, buffering, slow down impact, and be multi-party bit buffering, protect well
Wing and more rotor bodies, spring are symmetrically arranged with multiple, compare balance to the stress of buffer disc in this way, increase stability,
When landing, buffer disc contacts ground, and the support rod of surrounding plays a supporting role, prevents from turning on one's side, and at this point, spring plays buffering
Effect protects the internal structure of more rotor bodies well, plays a protective role during flight in this way, and dropping
Play the role of buffer protection when falling, function is richer, more practical.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the main view of the utility model；
Fig. 3 is the guard ring of the utility model and the connection top view of buffer board.
In figure: more than 1 rotor body, 2 cameras, 21 bottom plates, 22 pass punch plate, 23 guard rings, 24 springs, 25 support rods, 26
Connecting rod.
Specific embodiment
As shown in Figures 1 to 3, a kind of camera shooting unmanned plane with protection and landing shock-absorbing function, including more rotor bodies 1,
Using common multi-rotor unmanned aerial vehicle in the market, the control mechanism of camera 2 and more rotor bodies 1 is electrically connected, this is existing
There is technology, relatively common in the market, the upper end of more rotor bodies 1 is fixed with camera 2, and the lower end middle part of more rotor bodies 1 is solid
Surely there is bottom plate 21, and the downside of bottom plate 21 is connected with parallel horizontally disposed buffer disc 22,21 He of bottom plate by buffer gear
Buffer disc 22 is in disk form, reduces windage, and bottom plate 21 is bonded in the lower end of more rotor bodies 1, is easily installed, buffer gear
Including the spring 24 being fixed between bottom plate 21 and buffer disc 22, and spring 24 be provided with about the axisymmetrical of bottom plate 21 it is more
A, spring 24 is provided with multiple, the stability of guarantee buffer disc 22, stress balance.
The circumferential direction of buffer disc 22 is connected with the guard ring 23 of annular by supporting mechanism, and supporting mechanism includes fixing at equal intervals
In the circumferential outside support rod 25 of buffer disc 22, and the free end of support rod 25 passes through the protection of upward connecting rod 26 and upside
Circle 23 is fixedly connected, and supports guard ring 23, and the quantity of preferred support rod 25 is three here, excessively too heavy, very little uneven, and
Guard ring 23 is socketed in the outside of the wing of more rotor bodies 1, and there are buffer distance, supports between guard ring 23 and wing here
Arc transition between bar 25 and connecting rod 26 is prevented from blocking when landing, is integrated between buffer disc 22, support rod 25 and connecting rod 26
Type structure, it is more solid, also become manufacture, all uses plastic material here, it is relatively lighter.
Working principle: when encountering barrier, guard ring 23 contacts first, so that wing is protected, after guard ring 23 contacts,
Impact force is transmitted to connecting rod 26, through support rod 25, is transmitted to buffer disc 22, and buffer disc 22 passes through the bottom plate 21 of spring 24 and upside
It is connected with more rotor bodies 1, such spring 24 just plays the role of damping, buffering, slows down impact, and is multi-party bit buffering, very
It is good to protect wing and more rotor bodies 1, spring 24 be symmetrically arranged with it is multiple, it is relatively more flat to the stress of buffer disc 22 in this way
Weighing apparatus, increases stability, and when landing, buffer disc 22 contacts ground, and the support rod 24 of surrounding plays a supporting role, prevents from turning on one's side,
And at this point, spring 24 plays buffer function, the internal structure of more rotor bodies 1 is protected well, so i.e. in flight
It plays a protective role in the process, and plays the role of buffer protection in landing, function is richer, more practical.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
Made any modifications, equivalent replacements, and improvements etc., should be included in the utility model within the spirit and principle of utility model
Protection scope within.
Claims (5)
1. a kind of with the camera shooting unmanned plane for protecting and landing shock-absorbing function, including more rotor bodies (1), more rotor bodies
(1) upper end is fixed with camera (2), it is characterised in that: is fixed with bottom plate in the middle part of the lower end of more rotor bodies (1)
(21), and the downside of bottom plate (21) is connected with parallel horizontally disposed buffer disc (22) by buffer gear；
The circumferential direction of the buffer disc (22) is connected with the guard ring (23) of annular by supporting mechanism, and guard ring (23) is socketed in
The outside of the wing of more rotor bodies (1).
2. having the camera shooting unmanned plane for protecting and landing shock-absorbing function according to claim 1, it is characterised in that: the bottom plate
(21) and buffer disc (22) is in disk form, and bottom plate (21) is bonded in the lower end of more rotor bodies (1).
3. having the camera shooting unmanned plane for protecting and landing shock-absorbing function according to claim 2, it is characterised in that: the buffering
Mechanism includes being fixed on spring (24) between bottom plate (21) and buffer disc (22), and axis of the spring (24) about bottom plate (21)
It is symmetrically arranged with multiple.
4. according to claim 1 or 3 is described with the camera shooting unmanned plane for protecting and landing shock-absorbing function, it is characterised in that: described
Outside support rod (25) of the supporting mechanism including being fixed on buffer disc (22) circumferential direction at equal intervals, and the free end of support rod (25)
It is fixedly connected by upward connecting rod (26) with the guard ring (23) of upside.
5. having the camera shooting unmanned plane for protecting and landing shock-absorbing function according to claim 4, it is characterised in that: the support
Arc transition between bar (25) and connecting rod (26).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821697040.6U CN209290688U (en) | 2018-10-19 | 2018-10-19 | A kind of camera shooting unmanned plane with protection and landing shock-absorbing function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821697040.6U CN209290688U (en) | 2018-10-19 | 2018-10-19 | A kind of camera shooting unmanned plane with protection and landing shock-absorbing function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209290688U true CN209290688U (en) | 2019-08-23 |
Family
ID=67652851
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821697040.6U Expired - Fee Related CN209290688U (en) | 2018-10-19 | 2018-10-19 | A kind of camera shooting unmanned plane with protection and landing shock-absorbing function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209290688U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113086179A (en) * | 2021-04-27 | 2021-07-09 | 桂林天经地纬遥感信息技术有限公司 | Double-side anti-collision protection device for aerial photography unmanned aerial vehicle |
-
2018
- 2018-10-19 CN CN201821697040.6U patent/CN209290688U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113086179A (en) * | 2021-04-27 | 2021-07-09 | 桂林天经地纬遥感信息技术有限公司 | Double-side anti-collision protection device for aerial photography 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 |
Granted publication date: 20190823 Termination date: 20201019 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |