CN207225605U - A kind of unmanned plane stopping platform - Google Patents
A kind of unmanned plane stopping platform Download PDFInfo
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- CN207225605U CN207225605U CN201721170895.9U CN201721170895U CN207225605U CN 207225605 U CN207225605 U CN 207225605U CN 201721170895 U CN201721170895 U CN 201721170895U CN 207225605 U CN207225605 U CN 207225605U
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Abstract
It the utility model is related to a kind of unmanned plane stopping platform, including being installed on for stopping the platform body, support base, inclination of unmanned plane on support base and for multiple supporting rods of support platform body, supporting rod is flexibly connected with support base, is used for realization supporting rod along the diametric swing of support base；Supporting rod is flexibly connected with platform body so that platform body can be moved along supporting rod；Further include the motor for being placed in the flywheel of platform body inner cavity, driving the high-speed rotating rotation axis of flywheel, power being provided for rotation axis, several balls are equipped between the inner wall of platform body and the outer wall of flywheel, connecting shaft is provided with the center of flywheel, connecting shaft is pierced by after the bottom wall of platform body and is connected with rotation axis by universal joint.The unmanned plane stopping platform of the utility model is simple in structure, easy to use.
Description
Technical field
The utility model belongs to unmanned plane auxiliary body field, and in particular to a kind of unmanned plane stopping platform.
Background technology
UAV abbreviation unmanned plane, is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently independently operated by car-mounted computer, compared with manned aircraft, nobody
Machine is often more suitable for those dangerous tasks.Unmanned plane can be divided into dual-use by application field.
In military field, the tasks such as army is largely carried out investigations using unmanned plane, searched and rescued, still, due to marine stormy waves
The reason for big, unmanned plane sea landing platform cannot keep horizontal, cause unmanned plane can not stop and charge across the sea, to nothing
Man-machine use brings significant limitation.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane stopping platform, to overcome current unmanned plane landing platform to exist
The problem of can not being stopped on sea.
For this reason, the technical solution of the utility model is as follows：
A kind of unmanned plane stopping platform, including platform body, support base, inclination for stopping unmanned plane are installed on support
It is flexibly connected on seat and for multiple supporting rods of support platform body, the supporting rod with support base, is used for realization the branch
Strut is along the diametric swing of the support base；
The supporting rod is flexibly connected with platform body so that platform body can be moved along supporting rod；
Further include the flywheel for being placed in platform body inner cavity, the high-speed rotating rotation axis of the drive flywheel, be the rotation
Axis provides the motor of power, several balls are equipped between the inner wall of the platform body and the outer wall of flywheel, the flywheel
Connecting shaft is provided with center, the connecting shaft is pierced by after the bottom wall of platform body and is connected with rotation axis by universal joint.
A kind of above-mentioned unmanned plane stopping platform, is equipped with sliding slot on multiple supporting rods, is set on the platform body
There are multiple fixture blocks for being used to be caught in sliding slot, which can slide along sliding slot；
The supporting rod and support seat hinge so that supporting rod can inwardly or outwardly be swung along hinged place, so as to fulfill card
Downslide of the block in sliding slot moves up.A kind of above-mentioned unmanned plane stopping platform, the motor are fixed on the lower end of support base, institute
State after rotation axis passes through support base and couple with connecting shaft.
A kind of above-mentioned unmanned plane stopping platform, the connecting shaft are equipped with universal joint with rotation axis connection place.
A kind of above-mentioned unmanned plane stopping platform, the platform body are equipped with permanent magnet.
A kind of above-mentioned unmanned plane stopping platform, the platform body are equipped with two electromagnetism suction for unmanned plane charging
Disk, described two magnechucks charge unmanned plane by charging system.
A kind of above-mentioned unmanned plane stopping platform, the charging system include charge controller, power circuit, sucker control
Circuit, charging control circuit, the power circuit are electrically connected with charge controller, for providing needed for charge controller work
Electric energy；The charge controller is electrically connected with sucker control circuit, for controlling the work of magnechuck by sucker control circuit
Make state；The charge controller is also electrically connected with charging control circuit, for controlling the charged state to unmanned plane.
A kind of above-mentioned unmanned plane stopping platform, the charge controller are DPS digitial controllers, its model
TMS320。
A kind of above-mentioned unmanned plane stopping platform, further includes the infrared locating module being electrically connected with the charge controller,
The infrared locating module is used to control infrared locating module to carry out detection and localization, which is used for unmanned plane transmission
Position reference.
A kind of above-mentioned unmanned plane stopping platform, the model ZLM40AD850-10BD of the infrared locating module.
A kind of above-mentioned unmanned plane stopping platform, the sucker control circuit include resistance R4, resistance R5, resistance R6, and three
Pole pipe Q1, triode Q2, the emitter of the triode Q1 are electrically connected with power circuit input terminal, and the current collection of triode Q1 is extremely
The output terminal of sucker control circuit, the base stage of triode Q1 are electrically connected by resistance R5 with the collector of triode Q2, triode
The emitter of Q2 is electrically connected with ground terminal, and the base stage of triode Q2 is electrically connected by resistance R6 with charge controller, and resistance R4 is set
It is placed between emitter and the base stage of triode Q1.
The beneficial effects of the utility model：
1. the platform body of the utility model, into retractable supporting part support, works as platform body by multiple support bar groups
After receiving the information that unmanned plane need to land, start motor, motor drives flywheel to rotate at a high speed, makes platform body in centrifugal force
All the time equilibrium state is under effect, after unmanned plane drops to platform, unmanned plane is adsorbed onto on platform body using permanent magnet,
Motor is stopped.The unmanned plane stopping platform of the utility model is simple in structure, easy to use；
2. the utility model hinged multiple supporting rods on support base, are placed in the fixture block on platform body along supporting rod
The small-scale slip of sliding slot, after unmanned plane drops to platform body, supporting rod can play a supportive role platform body；
3. after unmanned plane drops to landing platform, two magnechucks on platform body are placed in as charging port,
With the magnechuck collective effect on unmanned plane supporting leg, charged system charges unmanned plane.
The utility model is described in further details below with reference to accompanying drawings and embodiments.
Brief description of the drawings
Fig. 1 is the overall structure diagram in snorkeling cabin.
Fig. 2 is the structure diagram one of unmanned plane stopping platform.
Fig. 3 is the structure diagram two of unmanned plane stopping platform.
Fig. 4 is the structure diagram three of unmanned plane stopping platform.
Fig. 5 is the schematic diagram of sucker control circuit.
In figure：1. platform body；11. magnechuck；12. infrared locating module；2. supporting rod；21. sliding slot；3.
Spill spin block；4. support base；5. flywheel；6. rotation axis；7. universal joint；8. connecting shaft.
Embodiment
For the technological means and effect that the utility model is reached predetermined purpose and taken is expanded on further, below in conjunction with attached drawing
And embodiment describes as follows specific embodiment of the present utility model, architectural feature and its effect in detail.
In the description of the present embodiment, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", " on ", " under ",
The orientation or position relationship of the instruction such as "front", "rear", "left", "right", " vertical ", " level ", " top ", " bottom ", " interior ", " outer " are
Based on orientation shown in the drawings or position relationship, it is for only for ease of description the present embodiment and creates and simplify description, without referring to
Show or imply that the device of meaning or element there must be specific orientation, with specific azimuth configuration and operation, therefore cannot manage
Solve the limitation to be created to the present embodiment.
In addition, term " first ", " second ", " the 3rd " etc. are only used for description purpose, and it is not intended that instruction or hint
Relative importance or the implicit quantity for indicating indicated technical characteristic.Thus, the feature of " first ", " second " etc. is defined
It can express or implicitly include one or more this feature.In the description that the present embodiment is created, unless otherwise saying
Bright, " multiple " are meant that two or more.
Term " installation ", " connected ", " connection " should be interpreted broadly, for example, it may be being fixedly connected or removable
Connection is unloaded, or is integrally connected；Can mechanically connect or be electrically connected；It can be directly connected, can also be in
Between medium be indirectly connected, can be the connection inside two elements.For the ordinary skill in the art, can pass through
Concrete condition understands concrete meaning of the above-mentioned term in the present embodiment creation.
It cannot keep horizontal across the sea to solve existing unmanned plane landing platform, influence asking for unmanned plane stop
Topic, the present embodiment according to gyroscopic effect principle object rotate when centrifugal force can make itself keep balance, the effect of gravity with
Centrifugal force is compared, and can be neglected, there is provided a kind of unmanned plane stopping platform, as shown in Figure 1, Figure 2, Figure 3 and Figure 4, including with
In stop unmanned plane platform body 1, be provided with multiple supporting rods 2 support base 4, can high-speed rotating rotation axis 6, drive rotation
6 rotating motor of shaft, multiple supporting rods 2 are by 1 support of platform body in the top of support base 4, supporting rod 2 and platform body 1
It is flexibly connected so that platform body 1 can move up and down along supporting rod 2；1 inner cavity of platform body is equipped with flywheel 5, platform body 1
Several balls are equipped between the outer wall of inner wall and flywheel 5, are equipped with connecting shaft 8 at the center of flywheel 5, connecting shaft 8 is pierced by platform
Couple after the bottom wall of body 1 with rotation axis 6；Motor drives rotation axis 6, connecting shaft 8, flywheel 5 to rotate at a high speed, and the flywheel 5 is at a high speed
Centrifugal force during rotation causes platform body 1 to be in equilibrium state.
It is pointed out that the unmanned plane pier of the present embodiment, due to applied on the water surface, especially marine, institute
Landing vertical axis unmanned plane is only capable of with the platform.
It may be noted that the purpose that the present embodiment sets ball is that the high speed for facilitating flywheel 5 rotates, since flywheel 5 rotates at a high speed
When platform body 1 do not rotate, therefore, it is necessary to set ball between platform body 1 and flywheel 5, flywheel 5 turns at a high speed
When dynamic, ball can also rotate, and to reduce the frictional force between flywheel 5 and platform body 1, ball can also revolve flywheel at a high speed
Centrifugal force caused by turning is transferred to platform body 1, platform body 1 is in equilibrium state.
The platform body 1 of the present embodiment is made up of retractable supporting part support multiple supporting rods 2, when platform body 1
After receiving the information that unmanned plane need to land, start motor, motor drives flywheel 5 to rotate at a high speed, makes platform body 1 in centrifugal force
Under the action of be in equilibrium state all the time, after unmanned plane drops to platform, unmanned plane is adsorbed onto platform body 1 using permanent magnet
On, motor is stopped.The unmanned plane stopping platform of the present embodiment is simple in structure, easy to use.
In order to make the flywheel 5 of the present embodiment, when high speed rotates, platform body 1 is in equilibrium state, the present embodiment all the time
The inner cavity of platform body 1 be provided with and be wholly or partially embedded into for 5 high-speed rotating swivelling chute of flywheel, flywheel 5 in swivelling chute, and
Between the cell wall of swivelling chute there is slightly gap, gap to cause flywheel 5 when doing high speed rotary motion, the card of platform body 1
Block is only along the movement of sliding slot 21 by a small margin on supporting rod 2, to keep the balance of platform body 1.
It may be noted that the supporting rod 2 of the present embodiment and coupling for platform body 1, can be that spring connects, fixture block sliding slot 21 connects
Connect, any form such as sliding block slide bar connection, it is only necessary on the premise of supporting role to platform body 1 is met, platform body 1
It can be moved up and down along supporting rod 2 is small-scale.Also, multiple supporting rods 2 of the present embodiment are equal around the central shaft of support base 4
Even distribution, in order to make the unmanned plane stopping platform of the present embodiment simple in structure, easy for installation, as shown in Figure 3 and Figure 4, this implementation
The supporting rod 2 of example is preferably three, is circumferentially uniformly arranged on support base 4, and the circular diameter that three supporting rods 2 are formed is less than
The diameter of platform body 1, the leg root of supporting rod 2 can flexibly be swung；It could so make it that three supporting rods 2 are outward-dipping at the same time
When, fixture block drives platform body 1 to move down, and the upward active force of three supporting rods 2 can play unmanned plane landing platform
Supporting role.
Preferably, being equipped with sliding slot 21 on three supporting rods 2 of the present embodiment, platform body 1 is equipped with multiple be used for
The fixture block of sliding slot 21 is caught in, which can slide along sliding slot 21；Supporting rod 2 is hinged with support base 4 so that supporting rod 2 can be along hinge
Meet place to swing to the diametric(al) of support base 4, so as to fulfill downslide of the fixture block in sliding slot 21 or move up.
In the present embodiment, the lower end of preferably supporting rod 2 is installed with spill spin block 3, support base 4 be equipped with for spill spin block 3 to
Groove that is interior or outwards waving, spill spin block 3 are partially submerged into groove, and are hinged with support base 4 using hinge pin.Due to three supports
The circular diameter of 2 lower end of bar and 3 junction of spill spin block is less than the diameter of platform body 1, so spill spin block 3 could be caused outwards to wave
When, supporting rod 2 is outward-dipping, drives platform body 1 to move down so as to fulfill fixture block；When spill spin block 3 inwardly waves, support
Bar 2 slopes inwardly, and shell realizes that fixture block drives platform body 1 to move up.
In order to make the platform body 1 of the present embodiment keep flat when stormy waves on the moment or sea that unmanned plane lands is larger
Weighing apparatus, the connecting shaft 8 and 6 connection place of rotation axis of the present embodiment are equipped with universal joint 7.The present embodiment set universal joint 7 purpose be：Nothing
How to change by the stormy waves on sea, although motor is tilted with support base 4 under the action of stormy waves, as long as motor drives flywheel 5
Rotate at a high speed, platform body 1 can remain balance under the influence of centrifugal force.
It may be noted that the motor of the present embodiment can be fixed on the upper surface of support base 4, support base 4 can also be fixed on
Lower face, when motor is fixed on the lower end of support base 4, rotation axis 6 couples after passing through support base 4 with connecting shaft 8.
As shown in Figure 1,1 lower end of platform body of the present embodiment can set used in floating chamber, used in floating chamber can thus be placed
Across the sea, stopped for unmanned plane.The preferably annular used in floating chamber of used in floating chamber, the annular used in floating chamber is by being placed in annular used in floating chamber inner ring
On support frame be fixedly connected with support base 4.Platform body 1 swims in the water surface at work, by used in floating chamber, due to floating
Cabin is connected by support frame with support base 4, and when there is stormy waves on sea, used in floating chamber can follow stormy waves to rock together, at this time, pass through
The universal joint 7 for being placed in the lower section of platform body 1 couples with the rotation axis 6 being placed on support base 4, so as to ensure to set above support frame
The platform body 1 put keeps parallel with horizontal plane.In short, connected between rotation axis 6 and platform body 1 by universal joint 7, with
Keep the levelness of platform body 1.
When platform body 1 is fixedly connected with used in floating chamber, the present embodiment sets the work of gyroscope 5 inside platform body 1
With further including：Rotated by gyroscope 5, keep the levelness of platform body 1, and pass through the effect of universal joint 7, platform body
1 will not follow support frame to tilt together, can so ensure when there is stormy waves, and platform body 1 can still keep horizontal, have
Stopped beneficial to unmanned plane.
The purpose that the present embodiment sets permanent magnet on platform body 1 is：Further ensure that unmanned plane is stopped by magnetic force
When on platform body 1, because of stormy waves unmanned plane will not be caused to drop in water.
Need to stress is：Also have the function of to charge for unmanned plane on the platform body 1 of the present embodiment, specific knot
Structure is：
Platform body 1 is equipped with two magnechucks 11 for unmanned plane charging, and two magnechucks 11 pass through Charging
System charges unmanned plane.Charging system includes charge controller, power circuit, sucker control circuit, charging control circuit,
Power circuit is electrically connected with charge controller, for providing the electric energy needed for charge controller work；Charge controller and sucker
Control circuit is electrically connected, for controlling the working status of magnechuck 11 by sucker control circuit；Charge controller is also with filling
Electric control circuit is electrically connected, for controlling the charged state to unmanned plane.
It is preferred that charge controller is DPS digitial controllers, its model TMS320.The controller of the model has
The high speed processing ability of 150MHz, possesses 32 floating point processing units, and 6 DMA channels are supported ADC, McBSP and EMIF, had more
PWM up to 18 tunnels is exported, wherein there is the PWM that 6 tunnels are the distinctive higher precisions of TI to export (HRPWM), 12 16 passage ADC.
Beneficial to its FPU Float Point Unit, user can quickly write control algolithm without expending the excessive time in processing decimal operation
And energy, compared with former generation DSP, average behavior improves 50%, and compatible with fixed point C28x controller softwares, so as to simplify software
Exploitation, shortens the construction cycle, reduces development cost.
As shown in figure 5, the sucker control circuit includes resistance R4, resistance R5, resistance R6, triode Q1, triode Q2, three
The emitter of level pipe Q1 is electrically connected with power circuit input terminal, the output terminal of the current collection extremely sucker control circuit of triode Q1,
The base stage of triode Q1 is electrically connected by resistance R5 with the collector of triode Q2, and emitter and the ground terminal of triode Q2 are electrically connected
Connect, the base stage of triode Q2 is electrically connected by resistance R6 with charge controller, resistance R4 be arranged at the emitter of triode Q1 with
Between base stage.
For above-mentioned charging control circuit with sucker control circuit with identical, its main function is to play control to fill unmanned plane
The connecting and disconnecting of the circuit of electricity.
In order to enable unmanned plane fast, easily to search unmanned plane stopping platform, on the platform body 1 of the present embodiment
Infrared locating module 12 is additionally provided with, which is electrically connected with charge controller, which uses
In controlling infrared locating module 12 to carry out detection and localization, which is used to transmit position reference to unmanned plane.
It is preferred that the model ZLM40AD850-10BD of infrared locating module 12.The infrared locating module 12 of the model has
It is small, power is low, good by water-proofing treatment the characteristics of long working life, applied in the underwater charge control system, not only
It is of low cost, and significant effect, can be good at playing the effect of auxiliary positioning, it is ensured that charging head and electronic equipment it is accurate
Positioning.
Above content is to combine specific preferred embodiment further detailed description of the utility model, it is impossible to
Assert that the specific implementation of the utility model is confined to these explanations.For the ordinary skill of the utility model technical field
For personnel, without departing from the concept of the premise utility, some simple deduction or replace can also be made, should all be regarded
To belong to the scope of protection of the utility model.
Claims (10)
1. a kind of unmanned plane stopping platform, it is characterised in that including the platform body for stopping unmanned plane（1）, support base
（4）, tilt be installed on support base（4）Go up and be used for support platform body（1）Multiple supporting rods（2）, the supporting rod（2）With
Support base（4）It is flexibly connected, is used for realization the supporting rod（2）Along the support base（4）Diametric swing；
The supporting rod（2）With platform body（1）It is flexibly connected so that platform body（1）Can be along supporting rod（2）It is mobile；
Further include and be placed in platform body（1）The flywheel of inner cavity（5）, drive the flywheel（5）High-speed rotating rotation axis（6）, be
The rotation axis（6）The motor of power, the platform body are provided（1）Inner wall and flywheel（5）Outer wall between be equipped with it is some
A ball, the flywheel（5）Center at be provided with connecting shaft（8）, the connecting shaft（8）It is pierced by platform body（1）Bottom wall
Afterwards with rotation axis（6）Pass through universal joint（7）Connection.
2. unmanned plane stopping platform as claimed in claim 1, it is characterised in that multiple supporting rods（2）On be equipped with cunning
Groove（21）, the platform body（1）It is equipped with multiple for being caught in sliding slot（21）Fixture block, which can be along sliding slot（21）It is sliding
It is dynamic；
The supporting rod（2）With support base（4）It is hinged so that supporting rod（2）Can inwardly or outwardly it be swung along hinged place, so that real
Existing fixture block is in sliding slot（21）Interior downslide moves up.
3. unmanned plane stopping platform as claimed in claim 1, it is characterised in that the motor is fixed on support base（4）Under
End, the rotation axis（6）Through support base（4）Afterwards with connecting shaft（8）Connection.
4. unmanned plane stopping platform as claimed in claim 1, it is characterised in that the motor is fixed on support base（4）It is upper
End.
5. such as claim 1-4 any one of them unmanned plane stopping platforms, it is characterised in that the platform body（1）On set
There is permanent magnet.
6. unmanned plane stopping platform as claimed in claim 1, it is characterised in that the platform body（1）It is equipped with and supplies nobody
Two magnechucks of machine charging（11）, described two magnechucks（11）Charged by charging system to unmanned plane.
7. unmanned plane stopping platform as claimed in claim 6, it is characterised in that the charging system include charge controller,
Power circuit, sucker control circuit, charging control circuit, the power circuit are electrically connected with charge controller, are filled for providing
Electric energy needed for electric controller work；The charge controller is electrically connected with sucker control circuit, for controlling electricity by sucker
Road controls magnechuck（11）Working status；The charge controller is also electrically connected with charging control circuit, for control pair
The charged state of unmanned plane.
8. unmanned plane stopping platform as claimed in claim 7, it is characterised in that the charge controller is digital control for DPS
Device, its model TMS320.
9. unmanned plane stopping platform as claimed in claim 7 or 8, it is characterised in that further include and charge controller electricity
The infrared locating module of connection（12）, the infrared locating module（12）For controlling infrared locating module（12）Carry out positioning inspection
Survey, the infrared locating module（12）For transmitting position reference to unmanned plane.
10. unmanned plane stopping platform as claimed in claim 7 or 8, it is characterised in that the sucker control circuit includes resistance
R4, resistance R5, resistance R6, triode Q1, emitter and the power circuit input terminal of triode Q2, the triode Q1 are electrically connected
Connect, the output terminal of the current collection extremely sucker control circuit of triode Q1, the base stage of triode Q1 passes through resistance R5 and triode Q2
Collector be electrically connected, the emitter of triode Q2 is electrically connected with ground terminal, and the base stage of triode Q2 passes through resistance R6 and charges
Controller is electrically connected, and resistance R4 is arranged between emitter and the base stage of triode Q1.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201721170895.9U CN207225605U (en) | 2017-09-13 | 2017-09-13 | A kind of unmanned plane stopping platform |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201721170895.9U CN207225605U (en) | 2017-09-13 | 2017-09-13 | A kind of unmanned plane stopping platform |
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| CN207225605U true CN207225605U (en) | 2018-04-13 |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107628203A (en) * | 2017-09-13 | 2018-01-26 | 余拓 | A kind of unmanned plane stopping platform |
| CN108725821A (en) * | 2018-04-30 | 2018-11-02 | 中山市翔实机械设备有限公司 | A kind of dual-purpose portable unmanned plane launching platform |
| CN109515640A (en) * | 2018-11-22 | 2019-03-26 | 深圳市海斯比船艇科技股份有限公司 | Unmanned boat folding and unfolding unmanned plane device and control method based on electroactive polymer |
| CN110525593A (en) * | 2019-09-27 | 2019-12-03 | 北京理工大学 | The the rising and falling of a kind of boat-carrying unmanned plane is fixed and charging system |
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2017
- 2017-09-13 CN CN201721170895.9U patent/CN207225605U/en active Active
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107628203A (en) * | 2017-09-13 | 2018-01-26 | 余拓 | A kind of unmanned plane stopping platform |
| CN107628203B (en) * | 2017-09-13 | 2024-04-05 | 余拓 | Unmanned aerial vehicle berths platform |
| CN108725821A (en) * | 2018-04-30 | 2018-11-02 | 中山市翔实机械设备有限公司 | A kind of dual-purpose portable unmanned plane launching platform |
| CN109515640A (en) * | 2018-11-22 | 2019-03-26 | 深圳市海斯比船艇科技股份有限公司 | Unmanned boat folding and unfolding unmanned plane device and control method based on electroactive polymer |
| CN109515640B (en) * | 2018-11-22 | 2020-11-06 | 深圳市海斯比海洋科技股份有限公司 | Unmanned ship launching and retracting unmanned aerial vehicle device based on electroactive polymer and control method |
| CN110525593A (en) * | 2019-09-27 | 2019-12-03 | 北京理工大学 | The the rising and falling of a kind of boat-carrying unmanned plane is fixed and charging system |
| CN110525593B (en) * | 2019-09-27 | 2020-09-22 | 北京理工大学 | Shipborne unmanned aerial vehicle lifting, fixing and charging system |
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