CN205574296U - Unmanned aerial vehicle mission equipment's tranquilizer - Google Patents
Unmanned aerial vehicle mission equipment's tranquilizer Download PDFInfo
- Publication number
- CN205574296U CN205574296U CN201620307505.7U CN201620307505U CN205574296U CN 205574296 U CN205574296 U CN 205574296U CN 201620307505 U CN201620307505 U CN 201620307505U CN 205574296 U CN205574296 U CN 205574296U
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- Prior art keywords
- dynamic mount
- shock attenuation
- upper plate
- attenuation frame
- tranquilizer
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- 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.)
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Abstract
The utility model discloses an unmanned aerial vehicle mission equipment's tranquilizer, including installing in the tranquilizer of unmanned aerial vehicle main part lower extreme, the tranquilizer includes first shock attenuation frame, second shock attenuation frame and bumper shock absorber, first shock attenuation frame is including first shock attenuation frame upper plate and first shock attenuation frame hypoplastron, second shock attenuation frame is including second shock attenuation frame upper plate and second shock attenuation frame hypoplastron, first shock attenuation frame upper plate is installed in the up end of second shock attenuation frame upper plate, and the screw more than is installed to the lower extreme of first shock attenuation frame upper plate, and first shock attenuation frame hypoplastron is installed in the lower terminal surface of second shock attenuation frame upper plate. The utility model discloses a stacked structure, shock attenuation frame go up the hypoplastron and connect through the steel wire bumper shock absorber, and mission equipment connects on first shock attenuation frame hypoplastron, and the spring of steel wire bumper shock absorber is in the stress, and most high -frequency vibration that the aircraft produced not only can be eliminated to this kind of mode, and it is reliable to install simple structure in addition, increases surely effectually.
Description
Technical field
This utility model relates to the tranquilizer of a kind of unmanned plane task device.
Background technology
Along with the gradually maturation of unmanned air vehicle technique, the especially rapid decrease of SUAV price, it is in boat
The advantage in bat field is the most obvious.Use many rotor unmanned aircrafts carry out taking photo by plane photography have safety high,
Flexibility ratio is good, attitude stabilization, with low cost, up to advantages such as danger areas.
Owing to SUAV quality is little, inertia is little, and power fully relies on the down thrust of propeller own and carried
The retroaction lift come.And the high frequency motion of properller itself brings the vibration of whole fuselage, therefore without
Man-machine itself have the strongest high dither energy, and task device cannot accomplish that precise synchronization offsets disturbance；In addition
The windage brought during unmanned plane motion is the maximum external force in addition to gravity.Irregular and the flight of aircraft configuration
During irregular movement locus all can bring a large amount of irregular high dither.And the speed of aircraft own is more
This shake energy that time fast, windage produces is the biggest.
Generally use The Cloud Terrace, as support platform, the task device such as video camera, photographing unit is installed.At present, exist
Following problems is there is in actually used:
1. The Cloud Terrace stability is the highest, and aircraft is affected by various factors in flight course easily causes The Cloud Terrace
Shake, although The Cloud Terrace increases stability in upgrading and can be strengthened, but the most not ideal enough, impact
Shooting effect；
2. structure is not quite reasonable, and existing The Cloud Terrace framework is relatively big, and insufficient strength is high, is highly prone to damage,
The load of The Cloud Terrace is the most not ideal enough, affects aircraft cruising time；
3. be not suitable for using under low temperature, hot weather environment with the The Cloud Terrace of silicone rubber material shock-damping structure.
Summary of the invention
Technical problem to be solved in the utility model is to provide a kind of tranquilizer, in order to solve prior art
The problem that present in middle tranquilizer, application scenario is limited or operation easier is bigger.
This utility model is achieved through the following technical solutions: the increasing of a kind of unmanned plane task device surely fills
Put, including being installed on the tranquilizer of unmanned plane main body lower end, described tranquilizer include the first dynamic mount,
Second dynamic mount and amortisseur, described first dynamic mount includes the first dynamic mount upper plate and the first dynamic mount lower plate；
Described second dynamic mount includes the second dynamic mount upper plate and the second dynamic mount lower plate, described first dynamic mount
Upper plate is installed on the upper surface of the second dynamic mount upper plate, and the lower end of the first dynamic mount upper plate is provided with more than one
Screw, the first dynamic mount lower plate is installed on the lower surface of the second dynamic mount upper plate；
Second dynamic mount lower plate is installed on the upper end of the first dynamic mount lower plate, the position, lower end of the screw of more than
Putting the lower surface through the second dynamic mount lower plate Yu the first dynamic mount lower plate to the first dynamic mount lower plate, task sets
For being connected in the first dynamic mount lower plate.
As preferred technical scheme, described amortisseur is installed under the second dynamic mount upper plate and the first dynamic mount
Between plate.
As preferred technical scheme, it is provided with between described second dynamic mount upper plate and the first dynamic mount lower plate
With the inclination mounting blocks at oblique angle, tilting and all offer pre-determined bit hole on mounting blocks, the upper and lower side of amortisseur is installed
In pre-determined bit hole.
As preferred technical scheme, described amortisseur is damper wire.
As preferred technical scheme, by connecting between described first dynamic mount upper plate and the first dynamic mount lower plate
Post is fixed according to position, hole screw locking, by connecting between described second dynamic mount upper plate and the second dynamic mount lower plate
Post is fixed according to position, hole screw locking.
The beneficial effects of the utility model are: this utility model uses stepped construction, and dynamic mount upper and lower plates passes through
Damper wire connects, and task device is connected in the first dynamic mount lower plate, at the spring of damper wire
In stress, this kind of mode is possible not only to eliminate the most high-frequency vibration that aircraft produces, and fills
Put simple and reliable for structure, increase the most effective.
Accompanying drawing explanation
In order to be illustrated more clearly that this utility model embodiment or technical scheme of the prior art, below by right
In embodiment or description of the prior art, the required accompanying drawing used is briefly described, it should be apparent that below,
Accompanying drawing in description is only embodiments more of the present utility model, for those of ordinary skill in the art,
On the premise of not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings.
Fig. 1 is cross section view of the present utility model；
Fig. 2 is the partial structurtes schematic diagram of this utility model carry image capturing apparatus main body；
Fig. 3 is overall structure schematic diagram of the present utility model.
Detailed description of the invention
All features disclosed in this specification, or disclosed all methods or during step, except mutually
Beyond the feature repelled mutually and/or step, all can combine by any way.
Any feature disclosed in this specification (including any accessory claim, summary and accompanying drawing), removes
Non-specifically describes, all can be by other equivalences or have the alternative features of similar purpose and replaced.That is, unless
Narration especially, each feature is an example in a series of equivalence or similar characteristics.
As shown in Figure 1-Figure 3, the tranquilizer of a kind of unmanned plane task device of the present utility model, including peace
Being loaded on the tranquilizer of unmanned plane main body 9 lower end, described tranquilizer includes the first dynamic mount, the second damping
Frame and amortisseur 7, described first dynamic mount includes the first dynamic mount upper plate 1 and the first dynamic mount lower plate 2；
Described second dynamic mount includes the second dynamic mount upper plate 3 and the second dynamic mount lower plate 4, described first damping
Frame upper plate 3 is installed on the upper surface of the second dynamic mount upper plate 3, and the lower end of the first dynamic mount upper plate 1 is provided with
The screw 5 of more than one, the first dynamic mount lower plate 2 is installed on the lower surface of the second dynamic mount upper plate 3；
Second dynamic mount lower plate 4 is installed on the upper end of the first dynamic mount lower plate 2, the screw 5 of more than
Lower end position is through the second dynamic mount lower plate 4 and the first dynamic mount lower plate 2 to the first dynamic mount lower plate 2 times
End face, task device 6 is connected in the first dynamic mount lower plate 2.
Wherein, amortisseur 7 is installed between the second dynamic mount upper plate 3 and the first dynamic mount lower plate 2；Second
It is provided with the inclination mounting blocks 8 at band oblique angle between dynamic mount upper plate 3 and the first dynamic mount lower plate 2, tilts to install
All offering pre-determined bit hole on block 8, the upper and lower side of amortisseur 7 is installed in pre-determined bit hole.
In the present embodiment, amortisseur 7 is damper wire；Under first dynamic mount upper plate 1 and the first dynamic mount
Fixed according to position, hole screw locking by connection post between plate 2, described second dynamic mount upper plate 3 and the second damping
Being fixed according to position, hole screw locking by connection post between frame lower plate 4, task device 6 is connected to the first dynamic mount
In lower plate 2, the spring of damper wire is in stress, is now possible not only to eliminate what aircraft produced
Most high-frequency vibration, and apparatus structure is simple and reliable, increases the most effective.
The above, detailed description of the invention the most of the present utility model, but protection domain of the present utility model is also
It is not limited to this, any change expected without creative work or replacement, all should contain in this practicality new
Within the protection domain of type.Therefore, protection domain of the present utility model should be limited with claims
Protection domain is as the criterion.
Claims (5)
1. the tranquilizer of a unmanned plane task device, it is characterised in that: include being installed on unmanned plane main body
The tranquilizer of lower end, described tranquilizer includes the first dynamic mount, the second dynamic mount and amortisseur, described
First dynamic mount includes the first dynamic mount upper plate and the first dynamic mount lower plate；
Described second dynamic mount includes the second dynamic mount upper plate and the second dynamic mount lower plate, described first dynamic mount
Upper plate is installed on the upper surface of the second dynamic mount upper plate, and the lower end of the first dynamic mount upper plate is provided with more than one
Screw, the first dynamic mount lower plate is installed on the lower surface of the second dynamic mount upper plate；
Second dynamic mount lower plate is installed on the upper end of the first dynamic mount lower plate, the position, lower end of the screw of more than
Putting the lower surface through the second dynamic mount lower plate Yu the first dynamic mount lower plate to the first dynamic mount lower plate, task sets
For being connected in the first dynamic mount lower plate.
The tranquilizer of unmanned plane task device the most according to claim 1, it is characterised in that: described
Amortisseur is installed between the second dynamic mount upper plate and the first dynamic mount lower plate.
The tranquilizer of unmanned plane task device the most according to claim 2, it is characterised in that: described
It is provided with the inclination mounting blocks at band oblique angle between second dynamic mount upper plate and the first dynamic mount lower plate, tilts to install
All offering pre-determined bit hole on block, the upper and lower side of amortisseur is installed in pre-determined bit hole.
The tranquilizer of unmanned plane task device the most according to claim 2, it is characterised in that: described
Amortisseur is damper wire.
The tranquilizer of unmanned plane task device the most according to claim 1, it is characterised in that: described
Fixed according to position, hole screw locking by connection post between the first dynamic mount upper plate and the first dynamic mount lower plate, described
Fixed according to position, hole screw locking by connection post between the second dynamic mount upper plate and the second dynamic mount lower plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620307505.7U CN205574296U (en) | 2016-04-13 | 2016-04-13 | Unmanned aerial vehicle mission equipment's tranquilizer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620307505.7U CN205574296U (en) | 2016-04-13 | 2016-04-13 | Unmanned aerial vehicle mission equipment's tranquilizer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205574296U true CN205574296U (en) | 2016-09-14 |
Family
ID=56861802
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620307505.7U Expired - Fee Related CN205574296U (en) | 2016-04-13 | 2016-04-13 | Unmanned aerial vehicle mission equipment's tranquilizer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205574296U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108469887A (en) * | 2018-06-13 | 2018-08-31 | 郑州云海信息技术有限公司 | A kind of server fan damper |
| CN108521775A (en) * | 2017-08-28 | 2018-09-11 | 深圳市大疆创新科技有限公司 | Damping device and head assembly, unmanned plane with the damping device |
| CN109131918A (en) * | 2018-10-19 | 2019-01-04 | 北京清航紫荆装备科技有限公司 | A kind of intersection DCB Specimen unmanned helicopter and its damped platform |
| CN111998212A (en) * | 2020-07-22 | 2020-11-27 | 酷景传媒(上海)有限公司 | High-stability structure of aircraft hanging panoramic camera |
| WO2021217462A1 (en) * | 2020-04-28 | 2021-11-04 | 深圳市大疆创新科技有限公司 | Gimbal assembly, mobile platform, shock absorption layout method and device, and storage medium |
-
2016
- 2016-04-13 CN CN201620307505.7U patent/CN205574296U/en not_active Expired - Fee Related
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108521775A (en) * | 2017-08-28 | 2018-09-11 | 深圳市大疆创新科技有限公司 | Damping device and head assembly, unmanned plane with the damping device |
| WO2019041096A1 (en) * | 2017-08-28 | 2019-03-07 | 深圳市大疆创新科技有限公司 | Damping device, pan-tilt assembly having same, and unmanned aerial vehicle |
| CN108521775B (en) * | 2017-08-28 | 2021-08-31 | 深圳市大疆创新科技有限公司 | Damping device and have this damping device's cloud platform subassembly, unmanned aerial vehicle |
| CN113700793A (en) * | 2017-08-28 | 2021-11-26 | 深圳市大疆创新科技有限公司 | Unmanned plane |
| CN108469887A (en) * | 2018-06-13 | 2018-08-31 | 郑州云海信息技术有限公司 | A kind of server fan damper |
| CN108469887B (en) * | 2018-06-13 | 2023-09-26 | 郑州云海信息技术有限公司 | Server fan shock absorber |
| CN109131918A (en) * | 2018-10-19 | 2019-01-04 | 北京清航紫荆装备科技有限公司 | A kind of intersection DCB Specimen unmanned helicopter and its damped platform |
| CN109131918B (en) * | 2018-10-19 | 2024-01-30 | 北京清航紫荆装备科技有限公司 | Cross double-rotor unmanned helicopter and damping platform thereof |
| WO2021217462A1 (en) * | 2020-04-28 | 2021-11-04 | 深圳市大疆创新科技有限公司 | Gimbal assembly, mobile platform, shock absorption layout method and device, and storage medium |
| CN111998212A (en) * | 2020-07-22 | 2020-11-27 | 酷景传媒(上海)有限公司 | High-stability structure of aircraft hanging panoramic camera |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170316 Address after: 518000 Guangdong Province, Shenzhen City Shilong Baoan District Shiyan Street Community Yihe Road No. 1 Corbett aviation science and Technology Park Building 3 (Yuan Jin Dahua Industrial Zone) Patentee after: SHENZHEN MICROMULTICOPTER Co.,Ltd. Address before: 518000 A District, R2 District, Nanshan District high tech park, Guangdong, Shenzhen, China Patentee before: Liu Wei |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20171010 Address after: Jiaxing City, Zhejiang province Jiashan County 314100 street to Luoxing Valley Park Business Center D block 4 Building Patentee after: ZHEJIANG KEBITE TECHNOLOGY CO.,LTD. Address before: 518000 Guangdong Province, Shenzhen City Shilong Baoan District Shiyan Street Community Yihe Road No. 1 Corbett aviation science and Technology Park Building 3 (Yuan Jin Dahua Industrial Zone) Patentee before: SHENZHEN MICROMULTICOPTER Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160914 |
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| CF01 | Termination of patent right due to non-payment of annual fee |