CN208802156U - A kind of unmanned plane phase machine protective cover device - Google Patents
A kind of unmanned plane phase machine protective cover device Download PDFInfo
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- CN208802156U CN208802156U CN201821293703.8U CN201821293703U CN208802156U CN 208802156 U CN208802156 U CN 208802156U CN 201821293703 U CN201821293703 U CN 201821293703U CN 208802156 U CN208802156 U CN 208802156U
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- unmanned plane
- shell
- inner casing
- protective cover
- machine protective
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Abstract
The utility model relates to a kind of unmanned plane phase machine protective cover devices, belong to unmanned plane field.It can solve the problems, such as that unmanned plane camera influences camera properties because of dampness in the long-term use using this device.Unmanned plane phase machine protective cover mounting structure; including shell, camera connecting rod; shell includes shell and inner casing; cavity is formed between shell and inner casing; aperture is provided on inner casing; moisture-proof pearl is provided in cavity, shell is provided with the transparency window opposite with unmanned plane camera lens with inner housing surface relative position.The utility model has the function of moisture-proof, so that unmanned plane camera is in drying regime, will not influence the performance of unmanned plane camera.
Description
Technical field
The utility model relates to air vehicle technique field more particularly to a kind of unmanned plane phase machine protective cover devices.
Background technique
The advantages of with the development of technology with innovation, unmanned plane is easily manipulated with it, compact structure, is widely used in ground
Shape is reconnoitred, in the domestic lifes field such as flight high angle shot.A kind of unmanned plane camera that notification number is CN107697310A protects dress
It sets including shell, shell includes first side, second side, the first fixed device, the second fixed device, for no undercarriage
For the unmanned plane of structure, camera lens is closely easy to damage camera lens by foreign matter with respect to ground distance excessively, when using this device, can provide one
The function that the moment that kind can land when unmanned aircraft parachute descent is fallen avoids camera lens dirty and punctured or hit by foreign matter, but camera is in length
During phase use, when environment biggish in humidity, can make camera dampness influence normal photographing.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane phase machine protective cover device, have prevent unmanned plane camera by
The function of tide.
The above-mentioned purpose of the utility model has the technical scheme that
A kind of unmanned plane phase machine protective cover mounting structure, including shell, camera connecting rod, the shell include shell with it is interior
Shell forms cavity between affiliated shell and inner casing, aperture is provided on the inner casing, moisture-proof pearl is provided in the cavity, outside
Shell is provided with the transparency window opposite with unmanned plane camera lens with inner housing surface relative position.
Implement above-mentioned technical proposal and unmanned plane camera is placed in inner casing in the use process of unmanned plane phase machine protective cover
Inside is placed in the moisture-proof pearl in cavity by the moisture in the aperture absorption shell on inner casing, ensures and be in drying regime in shell, make
The performance of camera will not be influenced because of dampness in the long-term use by obtaining unmanned plane camera, meanwhile, unmanned plane camera is being shot
It can be shot in the process by transparency window.
Further, the shell is opposite with inner casing is equipped with opening, and the open edge raises upward to form connecting cylinder, described
It is bolted to connection between connecting cylinder and camera connecting rod.
Implement above-mentioned technical proposal, connecting cylinder is fixedly connected with camera connecting rod, so that unmanned plane phase machine protective cover is logical
Connecting cylinder is crossed to be fixed in connecting rod.
Further, thermal insulation layer is provided on the outer casing inner wall, the moisture-proof pearl is placed between thermal insulation layer and inner casing.
Implement above-mentioned technical proposal, when unmanned plane camera is in the environment of continuous high temperature, nobody can be reduced by thermal insulation layer
Temperature inside machine protective cover, the case where avoiding the fuselage of unmanned plane camera and camera lens excessively high because of temperature damage appearance.
Further, the inner casing includes upper inner casing and lower inner casing, and the shell includes upper shell and lower casing, it is described it is upper in
Shell and upper shell form first chamber, are provided with upper spacer, the lower inner casing and lower casing in the first chamber open edge
Second chamber is formed, is provided with lower clapboard in the second chamber open edge.
Implement above-mentioned technical proposal, when opening shell, guarantees that the moisture-proof pearl between shell and inner casing will not fall out of cavity
It falls, moisture-proof pearl can also be replaced by opening partition.
Further, the upper case surface is symmetrically arranged with the first link block, and the lower casing surface is symmetrically arranged with the second company
Connect block, first link block and the second link block are set to the junction of upper housing and lower case, first link block and the
Two link blocks are bolted.
Implement above-mentioned technical proposal, makes shell be in closed by tightening bolt, prevent unmanned plane camera from being hit
It hits, shell is opened by bolt, can check unmanned plane camera in inner casing.
Further, the camera connecting rod is partially disposed in the inner casing, is provided with spring shock absorption on the inner casing inner wall
Device, the one end of the spring damper far from inner casing are connect with camera connecting rod.
Implement above-mentioned technical proposal, by the way that spring vibration damper is arranged, so that unmanned plane camera is outside shooting process is encountered
When carrying out object shock, the impulse force that exotic is hit is reduced, unmanned plane can also be reduced in the moment to land, unmanned plane camera is by ground
Impact force.
Further, it is provided with support plate on the upper shell, is provided with rain visor in the support plate.
Implement above-mentioned technical proposal, during shooting the rainy day, can block by rain visor will drip unmanned plane camera
Raindrop on to transparency window, so that the photo shot is more clear.
Further, the edge of rain visor and the edge of support plate are hinged.
Implement above-mentioned technical proposal, can make rain visor unmanned plane phase machine protective cover rain cover by rotating rain visor, not make
When with rain visor, it is rotated towards the position far from transparency window, light when shooting will not be blocked.
In conclusion the utility model has the following beneficial effects:
One, in the use process of unmanned plane phase machine protective cover, unmanned plane camera is placed in inner housing inner, is placed in cavity
Moisture-proof pearl the moisture in shell is absorbed by aperture on inner casing, ensure and be in drying regime in shell, so that unmanned plane camera exists
The performance of camera will not be made moist and influenced in long-term use process, meanwhile, unmanned plane camera in shooting process can be by saturating
Bright window is shot.
Two, in the skyborne shooting process of unmanned plane camera, unmanned plane phase machine protective cover and camera connecting rod can be made logical
Unmanned plane camera can be reduced when on the one hand making shock of the unmanned machine protective cover by exotic by crossing spring damper connection
By the dynamics impacted, the case where taking blurring of photos appearance is avoided, on the other hand the wink in the landing of unmanned plane on the ground
Between, reduce dynamics of the unmanned plane camera by ground struck.
Three, in the use process of unmanned machine protective cover, external temperature reduces the temperature in shell by thermal insulation layer, to make
The environment that unmanned plane camera is in proper temperature is obtained, damage of the temperature to unmanned plane camera properties is reduced.
Four, unmanned plane is unmanned machine protective cover rain cover by rain visor, to avoid unmanned plane when shooting in the rain
Camera occurs the situation for taking pictures fuzzy because of the rainwater on unmanned machine protective cover.
Detailed description of the invention
Fig. 1 is the structural schematic diagram that the utility model embodiment shell is connect with unmanned plane；
Fig. 2 is the perspective view of the explosion of the utility model embodiment shell；
Fig. 3 is the schematic cross-sectional view of the utility model embodiment shell.
Appended drawing reference: 1, shell；11, shell；111, upper shell；112, lower casing；113, the first link block；114, second
Link block；115, thermal insulation layer；116, support plate；117, rain visor；2, camera connecting rod；12, inner casing；121, upper inner casing；122,
Lower inner casing；123, aperture；3, moisture-proof pearl；4, transparency window；5, connecting cylinder；61, upper spacer；62, lower clapboard；7, spring damper.
Specific embodiment
Below in conjunction with attached drawing, the technical solution of the utility model embodiment is described.
As shown in Figure 1, a kind of unmanned plane phase machine protective cover device, including shell 1, camera connecting rod 2, shell 1 include outer
Shell 11 and inner casing 12 are provided with thermal insulation layer 115 on 11 inner wall of shell, aperture 123 are provided on inner casing 12, is provided in cavity anti-
Damp pearl 3, i.e., moisture-proof pearl 3 are placed between thermal insulation layer 115 and inner casing 12, and moisture-proof pearl 3 inside aperture 123 and inner casing 12 by being connected to, outside
Shell 11 is provided with the transparency window 4 opposite with unmanned plane camera lens with 12 surface relative position of inner casing.
Shell 11 and inner casing 12 be opposite is equipped with opening, and open edge raises upward to be formed and protrude into for camera connecting rod
Connecting cylinder 5, the connecting cylinder 5 are bolted to connection with camera connecting rod 2, and cavity is formed between shell 11 and inner casing 12, interior
Spring damper 7 is provided on shell 12, which connect with camera connecting rod 2.
Inner casing 12 is made of upper inner casing 121 and lower inner casing 122, and shell 11 includes upper shell 111 and lower casing 112, upper interior
Shell 121 and upper shell 111 form first chamber, are provided with upper spacer 61, upper spacer 61 and first in first chamber open edge
Chamber opening edge is bolted；Lower inner casing 122 and lower casing 112 form second chamber, in second chamber open edge
It is provided with lower clapboard 62, lower clapboard 62 is bolted with second chamber.I.e. shell 1 is divide into upper part and lower part by partition, on
The symmetrical two sides in 111 surface of shell are equipped with the first link block 113, and the symmetrical two sides in 112 surface of lower casing are equipped with the second link block
114, the first link block 113 and the second connection are bolted to shell 111 and abut place with lower casing 112.Upper shell 111
The top of transparency window 4 is provided with support plate 116, one end of support plate 116 cooperates with unmanned plane phase machine protective cover to be fixed, separately
One end and the end of rain visor 117 are hinged.
In the use process of unmanned plane phase machine protective cover, the camera connecting rod 2 on unmanned plane camera is passed through into connecting cylinder 5
It is put into unmanned plane phase machine protective cover, is shot by transparency window 4, moisture-proof pearl 3 is siphoned away in shell by the aperture 123 on inner casing 12
Moisture so that unmanned plane camera is in drying regime, in the long-time service of unmanned plane camera, unmanned plane camera will not because of by
Tide and influence its performance.
When unmanned plane phase machine protective cover is by external impact, by spring damper 7 make unmanned plane camera reduce by
To external impact, thus the case where avoiding unmanned plane camera internal from damaging appearance.
When outdoor temperature is higher, unmanned plane camera reduces its table by the thermal insulation layer 115 on unmanned plane phase machine protective cover
Face temperature, so that unmanned plane camera be made not deform camera body due to expanding with heat and contract with cold because of high temperature.
When shooting in the rain, by rain visor 117 be unmanned machine protective cover rain cover, thus avoid unmanned plane camera because
Rainwater on unmanned machine protective cover and there is the situation for taking pictures fuzzy.
Claims (8)
1. a kind of unmanned plane phase machine protective cover device, including shell (1), camera connecting rod (2), characterized in that the shell (1)
Including shell (11) and inner casing (12), cavity is formed between the shell (11) and inner casing (12), is arranged on the inner casing (12)
Have aperture (123), be provided in the cavity moisture-proof pearl (3), shell (11) and inner casing (12) surface relative position be provided with
The opposite transparency window of unmanned plane camera lens (4).
2. a kind of unmanned plane phase machine protective cover device according to claim 1, characterized in that the shell (11) and inner casing
(12) opposite to be equipped with opening, the open edge raises upward to be formed connecting cylinder (5), the connecting cylinder (5) and camera connecting rod
(2) it is bolted to connection between.
3. a kind of unmanned plane phase machine protective cover device according to claim 1, characterized in that on shell (11) inner wall
It is provided with thermal insulation layer (115), the moisture-proof pearl (3) is placed between thermal insulation layer (115) and inner casing (12).
4. a kind of unmanned plane phase machine protective cover device according to claim 1, characterized in that the inner casing (12) includes upper
Inner casing (121) and lower inner casing (122), the shell (11) includes upper shell (111) and lower casing (112), the upper inner casing
(121) first chamber is formed with upper shell (111), upper spacer (61) is provided in the first chamber open edge, under described
Inner casing (122) and lower casing (112) form second chamber, are provided with lower clapboard (62) in the second chamber open edge.
5. a kind of unmanned plane phase machine protective cover device according to claim 4, characterized in that upper shell (111) table
Face is symmetrically arranged with the first link block (113), and lower casing (112) surface is symmetrically arranged with the second link block (114), and described first
Link block (113) and the second link block (114) are set to the junction of upper housing (1) and lower case (1), first link block
(113) it is bolted with the second link block (114).
6. a kind of unmanned plane phase machine protective cover device according to claim 1, characterized in that the camera connecting rod (2)
It is partially disposed in the inner casing (12), is provided with spring damper (7), the spring damper on inner casing (12) inner wall
(7) one end far from inner casing (12) is connect with camera connecting rod (2).
7. a kind of unmanned plane phase machine protective cover device according to claim 5, characterized in that on the upper shell (111)
It is provided with support plate (116), is provided with rain visor (117) on the support plate (116).
8. a kind of unmanned plane phase machine protective cover device according to claim 7, characterized in that the rain visor (117)
The edge at edge and support plate (116) is hinged.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821293703.8U CN208802156U (en) | 2018-08-10 | 2018-08-10 | A kind of unmanned plane phase machine protective cover device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821293703.8U CN208802156U (en) | 2018-08-10 | 2018-08-10 | A kind of unmanned plane phase machine protective cover device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208802156U true CN208802156U (en) | 2019-04-30 |
Family
ID=66231505
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821293703.8U Expired - Fee Related CN208802156U (en) | 2018-08-10 | 2018-08-10 | A kind of unmanned plane phase machine protective cover device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208802156U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111907726A (en) * | 2020-07-30 | 2020-11-10 | 中国航天空气动力技术研究院 | High-speed aircraft outward vision camera heat protection device |
-
2018
- 2018-08-10 CN CN201821293703.8U patent/CN208802156U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111907726A (en) * | 2020-07-30 | 2020-11-10 | 中国航天空气动力技术研究院 | High-speed aircraft outward vision camera heat protection device |
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| 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: 20190430 Termination date: 20200810 |
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| CF01 | Termination of patent right due to non-payment of annual fee |