CN208947627U - A kind of unmanned plane of camera energy fast assembling-disassembling - Google Patents
A kind of unmanned plane of camera energy fast assembling-disassembling Download PDFInfo
- Publication number
- CN208947627U CN208947627U CN201821424424.0U CN201821424424U CN208947627U CN 208947627 U CN208947627 U CN 208947627U CN 201821424424 U CN201821424424 U CN 201821424424U CN 208947627 U CN208947627 U CN 208947627U
- Authority
- CN
- China
- Prior art keywords
- fuselage
- attachment base
- mentioned
- unmanned plane
- shock
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Accessories Of Cameras (AREA)
Abstract
A kind of unmanned plane of camera energy fast assembling-disassembling described in the utility model, including fuselage, the horn being symmetrically distributed on the fuselage and the paddle components being installed on the horn, its main feature is that: the photographic device of energy fast assembling-disassembling is additionally provided on the fuselage.The camera that the photographic device includes attachment base, is installed below attachment base, the photographic device is realized by rotation engaging connection structure and is connected and fixed with fuselage bottom, and the attachment base is equipped with shock-damping structure.The utility model is not needed by extraneous tool, and photographic device is that direct turn-knob is connected on fuselage, be not necessarily to threaded fastener, do not have to worry screw lose or damage and can not completed knocked down products, photographic device dismounting it is very convenient, fast；In addition shock-damping structure is increased in whole device, wherein shock-damping structure is used to offset the rolling power of unmanned plane during flying generation, improves the measurement accuracy of CCD camera assembly.
Description
Technical field
The utility model relates to unmanned plane field, especially a kind of unmanned plane of camera energy fast assembling-disassembling.
Background technique
Unmanned plane is widely used, at low cost, and efficiency-cost ratio is good；Risk that no one was injured；Survival ability is strong, and mobility is good,
It is easy to use, aerial survey, take photo by plane, navigating flies field and has good prospect, but since it need to carry various Aerial Electronic Equipments, as camera shooting is set
It is standby, keep package size often bigger, it is heavy.During transportation with need to dismantle picture pick-up device in maintenance process, and tear open
Process is unloaded to need to need to reinstall threaded fastener again when in use by tool ejector threaded fastener.Sometimes in other places
When operation, leaving behind tool or screw loss causes equipment that can not assemble, and causes to be unable to operation.And it disassembles and installs repeatedly
Both it wasted time, and also accelerated the abrasion of part, so being difficult to meet the requirement of the majority of consumers.
Summary of the invention
The purpose of this utility model is that there are problem and shortage for above-mentioned, one kind is provided and is not needed by extraneous work
Tool, and non-threaded fastener, camera dismounting is very convenient quickly, and the simple unmanned plane of structure.
The technical solution of the utility model is achieved in that
Unmanned plane described in the utility model including fuselage, the horn being symmetrically distributed on the fuselage and is installed on institute
The paddle components on horn are stated, its main feature is that: the photographic device of energy fast assembling-disassembling is additionally provided on the fuselage.The photographic device
Including attachment base, the camera being installed below attachment base, the photographic device is realized by rotation engaging connection structure and machine
Body bottom is connected and fixed, and the attachment base is equipped with shock-damping structure.The shock-damping structure is for offsetting or buffering unmanned plane
The rolling power generated when flight or land reduces the influence that vibration images camera.
To keep its structure simple, above-mentioned rotation engaging connection structure includes the circular rotating for being set to the attachment base top surface
Connector, the periphery of the rotary joint are equipped with buckle, and above-mentioned fuselage bottom is equipped with can be with the circle of the rotary joint adapting device
Block set, the edge that can be set with the hook that is clasped is equipped on the internal chamber wall of the block set accordingly, and the attachment base passes through rotation
Connector turn-knob with fuselage fast assembling-disassembling into linking together in the fuselage bottom block set.
For the very stiff and demanding connection for avoiding photographic device and fuselage, to ensure photographic effect, the shock-damping structure is including being arranged
Shock-damping structure one between above-mentioned attachment base and fuselage bottom, the shock-damping structure one are multiple retractable spring needles, institute
Spring needle is stated to be set at the top of attachment base.
Further to ensure that photographic effect, above-mentioned attachment base are formed by connecting by upper and lower seat board, above-mentioned shock-damping structure is also wrapped
The shock-damping structure two being clipped between upper and lower seat board is included, the shock-damping structure two is elastic component.The periphery of above-mentioned upper and lower seat board
Have multiple outwardly directed extended legs, above-mentioned elastic component be between the extended leg of upper and lower seat board and both ends respectively with phase
The connected elastic rubber column gel column of the extended leg (upper and lower layer) answered.In order to more preferably realize that damping effect, the elastic component include at least two
More than, it is respectively arranged at the outer end region of the extended leg, is capable of the rolling power of more balanced unmanned plane during flying generation in this way.
Above-mentioned camera is connected on above-mentioned attachment base in which can be removably mounted by bracket.To take the photograph the utility model not increasing
As under conditions of head, the range of monitoring is wider, and more efficient, the camera can rotate on bracket under the control of remote controler
Adjust camera angle.
Photographic device in the utility model is that direct turn-knob is connected on fuselage, when installing and removing, do not need by
Extraneous tool, be not necessarily to threaded fastener, do not have to worry screw lose or damage and can not completed knocked down products, photographic device dismounting ten
Divide convenient, fast；In addition multiple shock-damping structures are increased in whole device, shock-damping structure is used to offset unmanned plane during flying generation
Power is shaken, the measurement accuracy of CCD camera assembly is improved.
The utility model will be further described below with reference to the accompanying drawings.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the structural schematic diagram after the utility model takes out photographic device；
Fig. 3 is the structural schematic diagram of photographic device；
Fig. 4 is the assembling structure schematic diagram of Fig. 3.
Specific embodiment
As Figure 1-Figure 4, the unmanned plane of camera energy fast assembling-disassembling described in the utility model, including fuselage 1, symmetrical point
The horn 2 being distributed on the fuselage 1 and the paddle components 3 being installed on the horn 2, the fuselage 1 are equipped with and can quickly tear open
The photographic device 4 of dress.The photographic device includes attachment base 41, the camera 43 for being installed on 41 lower section of attachment base, the connection
Seat 41 is realized by rotation engaging connection structure and is connected and fixed with 1 bottom of fuselage, and the attachment base 41 is equipped with damping knot
Structure.Wherein, above-mentioned rotation engaging connection structure includes the circular rotating connector 44 for being set to 41 top surface of attachment base, the rotation
The periphery of connector 44 be equipped with buckle, above-mentioned 1 bottom of fuselage be equipped with can with the round block set 10 of 44 adapting device of rotary joint,
The edge that can be set with the hook that is clasped is equipped on the internal chamber wall of the block set 10 accordingly, the attachment base 41 is connect by rotation
First 44 turn-knob with 1 fast assembling-disassembling of fuselage into linking together in the 1 bottom block set 10 of fuselage.In order to effectively offset or delay
The rolling power that unmanned plane during flying is generated and landed is rushed, the shock-damping structure includes being set to above-mentioned attachment base 41 and 1 bottom of fuselage
Between shock-damping structure one.The shock-damping structure one is multiple retractable spring needles 42, and the spring needle 42 is set to connection
41 top of seat.To keep its structure simpler, above-mentioned attachment base 41 is formed by connecting by upper and lower seat board, and above-mentioned spring needle 42 is connected to
On upper base plate.Further to reinforce its bradyseism effect, above-mentioned shock-damping structure further includes the damping being clipped between upper and lower seat board
Structure two.There are multiple outwardly directed extended legs on the periphery of above-mentioned upper and lower seat board, and above-mentioned shock-damping structure two is positioned at upper and lower
The elastic rubber column gel column 46 that between the extended leg of seat board and both ends are connected with corresponding upper and lower layer extended leg respectively.To make its installation more
Convenient, the outer end of each extended leg is equipped with the installing port of band opening, the both ends of above-mentioned elastic rubber column gel column 46 be respectively equipped with can with it is described
The annular slot of installing port adapting device.More convenient to install the utility model and using, above-mentioned camera 43 passes through bracket
45 are connected on above-mentioned attachment base 41 in which can be removably mounted, and the camera 43 can be rotated on bracket 45 under the control of remote controler and be adjusted
Save camera angle.To adjust the monitoring range of camera 43, under conditions of not increasing camera, monitoring according to real-time condition
Range is wider, more efficient.The utility model structure is simple, when camera is mounted on fuselage, does not need by extraneous tool,
Non-threaded fastener, dismounting is very convenient quickly, and good camera shooting effect, monitoring range are wide.
Although the utility model is to be described with reference to specific embodiments, this description is not meant to the utility model
It is construed as limiting.Referring to the description of the utility model, other variations of the disclosed embodiments are all for those skilled in the art
It is anticipated that, this variation should belong in appended claims limited range.
Claims (9)
1. a kind of unmanned plane of camera energy fast assembling-disassembling, including fuselage (1), the horn being symmetrically distributed on the fuselage (1)
(2) and the paddle components (3) that are installed on the horn (2), it is characterised in that: the fuselage (1) is equipped with can fast assembling-disassembling
Photographic device (4), the photographic device includes attachment base (41), the camera (43) being installed below attachment base (41), institute
It states attachment base (41) and is realized by rotation engaging connection structure and is connected and fixed with fuselage (1) bottom, and the attachment base (41)
It is equipped with shock-damping structure.
2. unmanned plane according to claim 1, it is characterised in that: above-mentioned rotation engaging connection structure is described including being set to
The periphery of the circular rotating connector (44) of attachment base (41) top surface, the rotary joint (44) is equipped with buckle, above-mentioned fuselage (1) bottom
Equipped with can be equipped with accordingly on the internal chamber wall of the block set (10) with the round block set (10) of the rotary joint (44) adapting device
The edge that can be set with the hook that is clasped, the attachment base (41) pass through rotary joint (44) turn-knob into the fuselage (1) bottom
It links together in portion's block set (10) with fuselage (1) fast assembling-disassembling.
3. unmanned plane according to claim 1 or 2, it is characterised in that: the shock-damping structure includes being set to above-mentioned connection
Shock-damping structure one between seat (41) and fuselage (1) bottom.
4. unmanned plane according to claim 3, it is characterised in that: the shock-damping structure one is multiple retractable spring needles
(42), the spring needle (42) is set at the top of attachment base (41).
5. unmanned plane according to claim 4, it is characterised in that: above-mentioned attachment base (41) is formed by connecting by upper and lower seat board,
Above-mentioned spring needle (42) is connected on upper base plate.
6. unmanned plane according to claim 3, it is characterised in that: above-mentioned attachment base (41) is formed by connecting by upper and lower seat board,
Above-mentioned shock-damping structure further includes the shock-damping structure two being clipped between upper and lower seat board.
7. unmanned plane according to claim 6, it is characterised in that: the periphery of above-mentioned upper and lower seat board has multiple to overhanging
Extended leg out, above-mentioned shock-damping structure two be between the extended leg of upper and lower seat board and both ends respectively with corresponding extended leg
Connected elastic rubber column gel column (46).
8. unmanned plane according to claim 7, it is characterised in that: the outer end of each extended leg is equipped with the installing port with opening,
The both ends of above-mentioned elasticity rubber column gel column (46) are respectively equipped with can be with the annular slot of the installing port adapting device.
9. unmanned plane according to claim 1, it is characterised in that: above-mentioned camera (43) can be removably mounted ground by bracket (45)
It is connected on above-mentioned attachment base (41), the camera (43) can rotation adjusting be taken the photograph on bracket (45) under the control of remote controler
Image angle degree.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821424424.0U CN208947627U (en) | 2018-08-31 | 2018-08-31 | A kind of unmanned plane of camera energy fast assembling-disassembling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821424424.0U CN208947627U (en) | 2018-08-31 | 2018-08-31 | A kind of unmanned plane of camera energy fast assembling-disassembling |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208947627U true CN208947627U (en) | 2019-06-07 |
Family
ID=66736428
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821424424.0U Active CN208947627U (en) | 2018-08-31 | 2018-08-31 | A kind of unmanned plane of camera energy fast assembling-disassembling |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208947627U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112722298A (en) * | 2021-01-06 | 2021-04-30 | 广州市赛皓达智能科技有限公司 | Multispectral remote sensing aerial photography machine |
-
2018
- 2018-08-31 CN CN201821424424.0U patent/CN208947627U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112722298A (en) * | 2021-01-06 | 2021-04-30 | 广州市赛皓达智能科技有限公司 | Multispectral remote sensing aerial photography machine |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| WO2020200008A1 (en) | Plant protection unmanned aerial vehicle | |
| CN208947627U (en) | A kind of unmanned plane of camera energy fast assembling-disassembling | |
| CN206914659U (en) | Aircraft and its cradle head connection device | |
| CN207045661U (en) | Eight rotor plant protection unmanned planes and its flying wing arm knob are disassembled | |
| CN205440846U (en) | Unmanned aerial vehicle and horn folding mechanism thereof | |
| GB2559018A8 (en) | Assembly for an aircraft comprising an engine of the "open rotor puller" type and means for attaching the latter to the rigid structure of an attachment pylon | |
| CN107472546A (en) | A kind of unmanned plane photoelectric nacelle | |
| CN208868306U (en) | A kind of unmanned plane fast insert-pull carry platform | |
| CN205029490U (en) | A motor cabinet for having more rotor unmanned aerial vehicle | |
| CN207826532U (en) | Electric power patrols line unmanned aerial vehicle undercarriage | |
| CN208165744U (en) | A kind of anti-blocking blanking device of Feed Manufacturing | |
| CN212605799U (en) | Unmanned aerial vehicle with shock attenuation ball area increases steady function | |
| CN206797754U (en) | A kind of damping device of unmanned machine equipment installation | |
| CN205341247U (en) | Screen cloth pendulous device of concrete sprayer tool hand | |
| CN203439270U (en) | Aircraft | |
| CN205427433U (en) | Panoramic photography device | |
| CN209861479U (en) | Multifunctional full-angle plug-in machine head plug-in mechanism | |
| CN208233383U (en) | A kind of unmanned plane | |
| CN207191391U (en) | The unmanned plane of threaded interconnection system horn | |
| CN205633088U (en) | Pesticide sprays unmanned aerial vehicle's carry device | |
| CN208036648U (en) | A kind of holder of taking photo by plane of large size gyroplane | |
| CN204674824U (en) | The aircraft of collapsible hold-down arm | |
| CN211501863U (en) | Quick installing support for electric proportional valve | |
| CN209129860U (en) | A kind of fixation device convenient for water ring vacuum pump disassembly installation | |
| CN205596451U (en) | A adsorption equipment for circuit board |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |