CN206734651U - Marine unmanned plane landing platform - Google Patents
Marine unmanned plane landing platform Download PDFInfo
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- CN206734651U CN206734651U CN201720464557.XU CN201720464557U CN206734651U CN 206734651 U CN206734651 U CN 206734651U CN 201720464557 U CN201720464557 U CN 201720464557U CN 206734651 U CN206734651 U CN 206734651U
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- landing platform
- pedestal
- unmanned plane
- universal joint
- platform
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Abstract
The utility model provides a kind of marine unmanned plane landing platform, it is characterised in that：Including landing platform, balanced component and pedestal, the balanced component is arranged between landing platform and pedestal, the balanced component includes three driving cylinders and universal joint, one end of three driving cylinders is respectively connected with universal joint, the other end of universal joint is connected with landing platform, the other end of driving cylinder is fixed in pedestal, and the pedestal is provided with motion sensor.The beneficial effects of the utility model are：The attitude data provided by the Attitute detecting device of pedestal, the action that the motor driven support bar of three driving cylinders is elongated or shortened, landing platform is remained the posture of suitable unmanned plane landing, the purpose of the safe landing of unmanned plane is allowed on yo-yo sea level so as to reach.
Description
Technical field
Stabilized platform is the utility model is related to, refers in particular to a kind of marine unmanned plane landing platform.
Background technology
With the development of unmanned air vehicle technique, unmanned plane product is gradually popularized, and can be run into and be held on sea using unmanned plane auxiliary
The situation of row multiple-task, due to heave of sea, cause unmanned plane landing difficult, limited to unmanned plane to a certain extent
Landing site's advantage, it is therefore necessary to invent the unmanned plane landing platform that a kind of marine vessel uses.
Utility model content
Technical problem to be solved in the utility model is：Offer one kind can emotionally condition carries out feedback control according to surface wave
The device that landing platform keeps relative stability.
In order to solve the above-mentioned technical problem, the technical solution adopted in the utility model is：A kind of marine unmanned plane landing is put down
Platform, including landing platform, balanced component and pedestal, the balanced component are arranged between landing platform and pedestal, the balance
Component includes three driving cylinders and universal joint, and one end of three driving cylinders is respectively connected with universal joint, and the other end of universal joint is with rising
Platform connection is dropped, and the other end of driving cylinder is fixed in pedestal, and the pedestal is provided with motion sensor.
Further, the universal joint includes bearing, the first articulated section, the second articulated section and pin, and the of the bearing
One movable part and landing platform are affixed, and the second movable part of bearing and one end of the first articulated section are affixed, the first articulated section and
Two articulated sections are connected by pin, and the other end of the second articulated section and one end of driving cylinder are affixed.
Further, three driving cylinders are distributed in equilateral triangle.
Further, the projection at the center of the platform and the center of the pedestal coincides.
Further, the driving cylinder is electric cylinder.
The beneficial effects of the utility model are：The attitude data provided by the motion sensor of pedestal, drives to three
The action that the support bar of dynamic cylinder is retracted or stretched out, coordinate general-purpose section that landing platform can be made to remain that suitable unmanned plane rises
The posture of drop, the purpose of the safe landing of unmanned plane is allowed on yo-yo sea level so as to reach.
Brief description of the drawings
Concrete structure of the present utility model is described in detail below in conjunction with the accompanying drawings：
Fig. 1 is the overall structure diagram of marine unmanned plane landing platform of the present utility model；
Fig. 2 is the structural representation of the universal joint of marine unmanned plane landing platform of the present utility model；
1- platforms；2- balanced components；21- universal joints；The movable parts of 211- first；The movable parts of 212- second；213- first is cut with scissors
Socket part；The articulated sections of 214- second；215- pins；22- support bars；23- motors；3- pedestals.
Embodiment
To describe technology contents of the present utility model, construction feature, the objects and the effects in detail, below in conjunction with implementation
Mode simultaneously coordinates accompanying drawing to be explained in detail.
Fig. 1 and Fig. 2, a kind of marine unmanned plane landing platform, including landing platform, balanced component and pedestal are referred to,
The balanced component is arranged between landing platform and pedestal, and the balanced component includes three driving cylinders and universal joint, driving
Cylinder includes support bar and motor, and motor controls support bar to elongate or shorten by leading screw, and one end of three driving cylinders is respectively connected with
Universal joint, the other end of universal joint are connected with landing platform, and the other end of driving cylinder is fixed in pedestal, and the pedestal is provided with posture
Detection means, Attitute detecting device include attitude transducer and looped system, and attitude transducer can perceive pedestal X-axis, Y-axis
With the corner of Z axis, attitude signal is generated in real time and is output to looped system, looped system generates according to attitude signal
Control signal, motor make pose adjustment action.
It was found from foregoing description, the beneficial effects of the utility model are：There is provided by the Attitute detecting device of pedestal
Attitude data, the action that the motor driven support bars of three driving cylinders is elongated or shortened, makes landing platform remain suitable
The posture of unmanned plane landing is closed, the purpose of the safe landing of unmanned plane is allowed on yo-yo sea level so as to reach.
Embodiment 1
A kind of marine unmanned plane landing platform, including landing platform, balanced component and pedestal, the balanced component are arranged at
Between landing platform and pedestal, the balanced component includes three driving cylinders and universal joint, and one end of three driving cylinders respectively connects
One end of universal joint, the other end of universal joint are connected with landing platform, and the other end of driving cylinder is fixed in pedestal, and the pedestal is set
There is attitude transducer, the universal joint includes bearing, the first articulated section, the second articulated section and pin, and the first of the bearing lives
Moving part and landing platform are affixed, and the second movable part of bearing and one end of the first articulated section are affixed, the first articulated section and the second hinge
Socket part is connected by pin, and the other end of the second articulated section and one end of driving cylinder are affixed.
Universal joint can offset between support bar because different in size and caused by translate pulling force, be advantageous to the stability of system,
The first movable part and the second movable part of the bearing of universal joint can relative level rotations.
Embodiment 2
On the basis of embodiment 1, three driving cylinders are distributed in equilateral triangle.
Three driving cylinders support three directions of landing platform respectively, and the strong point is alternate 120 degree, are advantageous to the stabilization of system
Property.
Embodiment 3
On the basis of embodiment 2, the projection at the center of the platform and the center of the pedestal coincides.
The specific size of platform can adjust according to the size of unmanned plane, the center of platform and the center of the pedestal
Projection coincides, it is ensured that the mechanics of whole system is stable.
Embodiment 4
On the basis of embodiment 3, the driving cylinder is electric cylinder.
Driving cylinder is also an option that hydraulic cylinder, and this case preferred scheme is is quick on the draw using electric cylinder, electric cylinder, precision
It is controllable, it is more suitable for fine-tuning.
Embodiment of the present utility model is the foregoing is only, not thereby limits the scope of the claims of the present utility model, it is every
The equivalent structure or equivalent flow conversion made using the utility model specification and accompanying drawing content, or be directly or indirectly used in
Other related technical areas, similarly it is included in scope of patent protection of the present utility model.
Claims (5)
- A kind of 1. marine unmanned plane landing platform, it is characterised in that：Including landing platform, balanced component and pedestal, the balance Component is arranged between landing platform and pedestal, and the balanced component includes three driving cylinders and universal joint, three driving cylinders One end of each universal-joint in one end, the other end of universal joint are connected with landing platform, and the other end of driving cylinder is fixed in pedestal, The pedestal is provided with attitude transducer.
- 2. marine unmanned plane landing platform as claimed in claim 1, it is characterised in that：The universal joint includes bearing, first Articulated section, the second articulated section and pin, the first movable part and landing platform of the bearing are affixed, the second movable part of bearing with One end of first articulated section is affixed, and the first articulated section is connected with the second articulated section by pin, the other end of the second articulated section with One end of driving cylinder is affixed.
- 3. marine unmanned plane landing platform as claimed in claim 2, it is characterised in that：Three driving cylinders are in equilateral triangle point Cloth.
- 4. marine unmanned plane landing platform as claimed in claim 3, it is characterised in that：The center of the platform and the pedestal The projection at center coincide.
- 5. the marine unmanned plane landing platform as described in claim 1-4 any one, it is characterised in that：The driving cylinder is electricity Dynamic cylinder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720464557.XU CN206734651U (en) | 2017-04-28 | 2017-04-28 | Marine unmanned plane landing platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720464557.XU CN206734651U (en) | 2017-04-28 | 2017-04-28 | Marine unmanned plane landing platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206734651U true CN206734651U (en) | 2017-12-12 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720464557.XU Active CN206734651U (en) | 2017-04-28 | 2017-04-28 | Marine unmanned plane landing platform |
Country Status (1)
| Country | Link |
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| CN (1) | CN206734651U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108263633A (en) * | 2018-03-20 | 2018-07-10 | 广州亿航智能技术有限公司 | A kind of method for plane posture of landing from steady landing platform and its holding |
| CN108263631A (en) * | 2017-12-26 | 2018-07-10 | 中国科学院长春光学精密机械与物理研究所 | A kind of unmanned plane guiding and landing system |
| CN108415442A (en) * | 2018-01-23 | 2018-08-17 | 歌尔股份有限公司 | Unmanned plane adjusts test device |
| CN111007866A (en) * | 2019-12-26 | 2020-04-14 | 桂林航天工业学院 | Marine unmanned aerial vehicle take-off and landing platform and working method thereof |
-
2017
- 2017-04-28 CN CN201720464557.XU patent/CN206734651U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108263631A (en) * | 2017-12-26 | 2018-07-10 | 中国科学院长春光学精密机械与物理研究所 | A kind of unmanned plane guiding and landing system |
| CN108415442A (en) * | 2018-01-23 | 2018-08-17 | 歌尔股份有限公司 | Unmanned plane adjusts test device |
| CN108415442B (en) * | 2018-01-23 | 2021-04-13 | 歌尔股份有限公司 | Unmanned aerial vehicle adjusts testing arrangement |
| CN108263633A (en) * | 2018-03-20 | 2018-07-10 | 广州亿航智能技术有限公司 | A kind of method for plane posture of landing from steady landing platform and its holding |
| CN111007866A (en) * | 2019-12-26 | 2020-04-14 | 桂林航天工业学院 | Marine unmanned aerial vehicle take-off and landing platform and working method thereof |
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