CN206494119U - A kind of full-automatic connecting platform of unmanned plane - Google Patents
A kind of full-automatic connecting platform of unmanned plane Download PDFInfo
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- CN206494119U CN206494119U CN201621350334.2U CN201621350334U CN206494119U CN 206494119 U CN206494119 U CN 206494119U CN 201621350334 U CN201621350334 U CN 201621350334U CN 206494119 U CN206494119 U CN 206494119U
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- unmanned plane
- pusher
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- neck
- guide rail
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Abstract
The utility model discloses a kind of full-automatic connecting platform of unmanned plane, it includes sliding axle, Y types guide rail, pusher, linear electric motors, endless screw electric motor, movable handgrip, the plug for charging or transmitting data and aircraft landing round platform；The sliding axle is fixed on landing round platform by mounting bracket, one end close to Y type guide rails is connected with pusher, the both sides of pusher central point are provided with endless screw electric motor, the turned position that endless screw electric motor passes through gear control activity handgrip, movable handgrip is mobilizable to be arranged in pusher, the end of the Y types guide rail is provided with neck, the openings of sizes of the neck is equal with the shoulder of aircraft nose-gear two, and male socket is provided with by support above Y types guide rail end, the male socket matches with the female socket installed on unmanned plane；The linear electric motors are moved forward by pusher, and unmanned plane will be promoted to enter in neck, are caught unmanned plane by movable handgrip when exiting and are pulled out to the release of landing region.
Description
Technical field
The utility model is related to unmanned plane equipment technical field, more particularly to automatically connection is flat for a kind of unmanned plane
Platform.
Background technology
With the development of science and technology, the application field of unmanned plane is more and more extensive, and its field covered includes army, police
Examine, railway, electric power, geography, environmental protection etc., the direction of application include it is aerial throw, monitoring, investigation, detection, photography, relay etc., its
Middle certain fields require more and more higher to the automatic operation of UAS, and particularly large-scale production station is to utilizing unmanned plane
The full-automatic inspection for being timed fixed point proposes higher requirement.At present, most unmanned plane is only capable of realizing both at home and abroad
The automation of aerial inspection process, but can not realize that the functions such as data, charging, recovery are read in the automation after flight landing, it is real
The automation mechanized operation of existing ground-support equipment is the important ring for realizing the complete autonomous unmanned running of UAS.
Therefore, prior art has yet to be improved and developed.
The content of the invention
The purpose of this utility model is to provide a kind of unmanned plane full-automatic connecting platform, it is intended to solve existing unmanned plane
It is only capable of realizing the automation of aerial inspection process, but can not realizes that data, charging, recovery are read in automation after flight landing
Technical problem.
The technical solution of the utility model is as follows：A kind of full-automatic connecting platform of unmanned plane, it includes sliding axle, Y types and led
Rail, pusher, linear electric motors, endless screw electric motor, movable handgrip, the plug for charging or transmitting data and aircraft landing circle
Platform；The sliding axle is fixed on landing round platform by mounting bracket, and one end close to Y type guide rails is connected with pusher, sliding
The both sides of dynamic push rod central point are provided with endless screw electric motor, and endless screw electric motor passes through the turned position of gear control activity handgrip, activity
Handgrip is mobilizable to be arranged in pusher, and the end of the Y types guide rail is provided with neck, the openings of sizes of the neck and flight
The shoulder of device nose-gear two is equal, and is provided with male socket by support above Y types guide rail end, the male socket and nobody
The female socket installed on machine matches；The linear electric motors are moved forward by the pusher for driving sliding axle to fix, and
Promote unmanned plane to enter in the neck of Y type guide rails, unmanned plane is caught by endless screw electric motor rotation activity handgrip when exiting and pulled out
To the release of landing region.
The full-automatic connecting platform of described unmanned plane, wherein, biography is installed on the end face of the pusher wherein one end
Sensor.
The full-automatic connecting platform of described unmanned plane, wherein, the sensor is Hall sensor, and corresponds to pusher
The position of motion, induced magnet is provided with the side of Y type guide rails.
The full-automatic connecting platform of described unmanned plane, wherein, the sensor is infrared ray sensor, and correspondingly slip is pushed away
The position of bar motion, infrared receiver is provided with the side of Y type guide rails.
The full-automatic connecting platform of described unmanned plane, wherein, the movement position of the pusher be respectively original position,
Centre position and terminal position.
The full-automatic connecting platform of described unmanned plane, wherein, the male socket front end is provided with connecing of being connected with wire
Touch copper sheet.
The full-automatic connecting platform of described unmanned plane, wherein, the wire includes power line, data transmission line, data and connect
Take-up, charging wire, ground wire.
The full-automatic connecting platform of described unmanned plane, wherein, the unmanned plane can for four rotor wing unmanned aerial vehicles, six rotors without
Any one in man-machine, eight rotor wing unmanned aerial vehicles.
The beneficial effects of the utility model：The utility model by aircraft landing round platform install Y type guide rails, and
Think corresponding neck with unmanned plane undercarriage provided with one in the end of Y type guide rails so that unmanned plane can be fixed on Y type guide rails
Charged in neck；Male socket is installed above Y type guide rail ends, it is relative with the female socket of unmanned aerial vehicle body side
Should；When unmanned plane is dropped on the position of aircraft landing round platform, the pusher on Y type guide rails, and pusher
Center be connected with sliding axle, and sliding axle is under the driving of linear electric motors, and sliding axle promotes pusher motion, and then promotes
Unmanned plane movement on aircraft landing round platform so that unmanned plane can be moved along the edge of Y type guide rails, and then be entered
In neck, the undercarriage of unmanned plane is corresponding with neck chimeric so that the female socket and plug of unmanned plane is corresponding；Realize nobody
It can be pushed in the neck of Y type guide rail ends and be charged by pusher after machine landing, without manually grasping in whole process
Control, using pusher and the position-limiting action of Y type guide rails, realizes that being refined control after unmanned plane landing arrives in spacing neck,
Realize that the circuit of unmanned plane and ground-support equipment is connected, so as to realize the functions such as digital independent, transmission and automatic charging, make nothing
Man-machine terrestrial operation is realized unmanned；By the spacing guiding function of Y type guide rails, make pusher only by moving forward and backward i.e.
Controllable unmanned plane is accurate to up to required position and connects charging equipment automatically, simple and reliable for structure；By using the public affairs of pairing
Connector and female socket so that the circuit of connection is more, solve the monolithic of many battery core assembled batteries during automatic charging
The balance of voltage, test problems；By the use of Y types guide rail and pusher, the pixel accuracy requirement for making unmanned plane land automatically
Step-down, makes realizing for the full Unmanned operation of UAS more reliable.
Brief description of the drawings
Fig. 1 is a kind of structured flowchart of the present utility model.
Fig. 2 is pusher and the structural representation of sliding axle installation in the utility model.
Fig. 3 is the mounting structure schematic diagram of inductor in the utility model.
Fig. 4 is the mounting structure schematic diagram of induced magnet in the utility model.
Fig. 5 is the structural representation of neck in Y type guide rails in the utility model.
Fig. 6 is the structural representation of unmanned plane in the utility model.
Fig. 7 is a kind of location drawing when working in the utility model.
Fig. 8 is another location drawing when working in the utility model.
Fig. 9 is another location drawing when working in the utility model.
Figure 10 is another location drawing when working in the utility model.
Figure 11 is another location drawing when working in the utility model.
Figure 12 is another location drawing when working in the utility model.
Figure 13 is another location drawing when working in the utility model.
Figure 14 is another location drawing when working in the utility model.
Figure 15 is another location drawing when working in the utility model.
Embodiment
To make the purpose of this utility model, technical scheme and advantage clearer, clear and definite, develop simultaneously implementation referring to the drawings
The utility model is further described example.
As shown in figure 1, the utility model discloses a kind of full-automatic connecting platform of unmanned plane, it includes sliding axle 1, Y types
Guide rail 9, pusher 6, linear electric motors 3, endless screw electric motor 4, movable handgrip 12, the male socket 10 for charging or transmitting data
With aircraft landing round platform 13；The sliding axle 1 is fixed on landing round platform 13 by mounting bracket 2, close to Y types guide rail 9
One end is connected with pusher 6, and the both sides of the central point of pusher 6 are provided with endless screw electric motor 4, and endless screw electric motor 4 passes through gear control
The turned position of activity handgrip 12 processed, movable handgrip 12 is mobilizable to be arranged in pusher 6, the end of the Y types guide rail 9
Provided with neck 15, the openings of sizes of the neck 15 is equal with the shoulder of unmanned plane nose-gear two, and passes through above the end of Y types guide rail 9
Support 14 is provided with male socket 10, and the male socket 10 matches with the female socket installed on unmanned plane 11；It is described straight
Line motor 3 is moved forward by the pusher 6 for driving sliding axle 1 to fix, and promotes unmanned plane into the neck of Y types guide rail 9
In 15, unmanned plane 11 is caught by the rotation activity handgrip 12 of endless screw electric motor 4 when exiting and the release of landing region is pulled out to.
After said structure, the utility model pusher drops to the unmanned plane of landing round platform to promote so that nothing
It is man-machine can be by pusher shift position, and Y types guide rail can control direction of the unmanned plane along Y type guide rails to move, and
In the neck that Y type guide rails are pushed to along guide rail so that the undercarriage of unmanned plane can be nested in neck, and then realize fixation
Unmanned plane, also make it that male socket is corresponding with female socket, when unmanned plane is promoted, the female socket quilt of unmanned plane
Male socket is inserted, and is charged, reads data or transmission data, and pusher is slided in the presence of linear electric motors
Axle promotes pusher movement；So outside controller is detected after unmanned plane landing, linear electric motors just can be automatically controlled
Sliding axle is driven, and sliding axle promotes pusher, pusher promotes unmanned plane to be moved along Y type guide rails, and unmanned plane is pushed away
Move in neck, then the female socket of unmanned plane is inserted by male socket；It is achieved that full-automatic connection, whole process
Be operated without anyone personnel, without personnel take part in adjustment unmanned plane position, just can realize unmanned plane charging and
Transmit data.
Progressive one is said, sensor 5 is provided with the pusher 6 of the present utility model wherein end face of one end；By in cunning
Install sensor on dynamic push rod so that pusher senses the inductor of Y type guide rails side, and to the position according to inductor
To determine the position of pusher, and then to the movable handgrip in pusher, endless screw electric motor is controlled by controller outside the venue,
Rotary moveable handgrip fills with the frame of electric unmanned plane to catch, then by the middle of unmanned plane abjection to landing round platform.
Preferably, sensor 5 of the present utility model can be Hall sensor, and the position that correspondence pusher 1 is moved
Put, induced magnet 7,8 is installed in the side of Y types guide rail 9；Pusher is caused by the cooperation of induced magnet and sensor
Position can be identified, and then recognize the position that unmanned plane has been pushed to, or be dragged out specific position, and then
Control linear electric motors stopping or the work of endless screw electric motor.
Sensor of the present utility model can also be infrared ray sensor, and the position of correspondence pusher motion, in Y types
The side of guide rail 9 is provided with infrared receiver；By the cooperation of infrared ray sensor and infrared receiver, when infrared ray hair
Signal is projected, and infrared receiver receives signal, and then judges the position of pusher so that ability controller outside the venue can be with
The position of pusher is known in real time, and then controls linear electric motors and endless screw electric motor, and then controls sliding axle and movable handgrip.
Furtherly, the movement position of pusher 6 of the present utility model is respectively original position, centre position and end
Position；These positions are set with crossing so that the sensor of pusher can be according to these specific positions, and feed back to outside the venue
Controller, manipulation linear electric motors, endless screw electric motor etc. are realized according to these positions；The step of control has been divided by these positions
Suddenly, and control flow.
Furtherly, the front end of male socket 10 of the present utility model is provided with the contact copper sheet being connected with wire；By this
Contact copper sheet is write, to realize data transfer and charging.
Furtherly, wire of the present utility model includes power line, data transmission line, data receiver line, charging wire, ground connection
Line.
In real work, unmanned plane of the present utility model can be four rotor wing unmanned aerial vehicles, six rotor wing unmanned aerial vehicles, eight rotors
Any one in unmanned plane, and the unmanned plane that correspondence the utility model is used, the bottom of the unmanned plane is provided with bikini
Undercarriage.
Operation principle of the present utility model：
Control the action that moves forward and backward of sliding axle by computer and relevant control circuit, movable handgrip is grabbed through and discharged
Action, unmanned plane is by the neck direction with regard to itself programme-control its head sensing Y type guide rails and drops to aircraft automatically
Drop in the range of round platform, linear electric motors driving sliding axle and its connected pusher travel forward, and promote landing round platform region
The bayonet socket direction of interior unmanned plane to Y type guide rails is moved, due to the bikini undercarriage that unmanned plane is installed, first two of undercarriage
Post contact slide push rod first, now due to the promotion of pusher, forces unmanned plane head to point to the neck of Y type guide rails all the time
Direction, this corrected for unmanned plane in automatic descent Heading control not precisely, pusher continues to press on unmanned plane
Moved to neck direction, now due to the spacing guiding function of Y type guide rails, unmanned plane is fallen into the neck of Y type guide rails
And the male socket positioned at Y type guide rail ends is automatically inserted into the female socket of unmanned plane, and realize that circuit is connected, program control
Automatic charging processed, after charging terminates, the nose-gear for catching unmanned plane, straight-line electric are rotated by endless screw electric motor control activity handgrip
Machine drives sliding axle setback and unmanned plane is pulled out neck, when rail plate moves to centre position, sliding axle pause
Motion, and control endless screw electric motor rotation activity handgrip to discharge unmanned plane, sliding axle continues to back to endpoint location, and unmanned plane is again
Automatic takeoff.
Above-mentioned unmanned plane is a kind of four rotor wing unmanned aerial vehicle, and it includes being provided with unmanned aerial vehicle body, tail wheel type landing gear
110th, the structure such as female socket 111, capstan/propeller 113, motor, motor mount, horn 112, horn mounting seat；Nobody
Machine fuselage is to connect the main body that unmanned plane sings parts；The tail wheel type landing gear 110 is made up of three supports that rise and fall, head
Direction front fuselage is installed side by side installs one on axis on rear side of two, fuselage；The female socket 111 is arranged on unmanned plane
Afterbody center, is horizontally mounted, and female socket front end is provided with the contact copper sheet being connected with wire, and the wire includes
But power line, data transmission line, data receiver line, charging wire, ground wire are not limited to, its connecting object is above-described male
Socket, each wire of the above is corresponded with corresponding male socket.The horn mounting seat is used to connect fuselage and horn, along machine
Body both sides are arranged symmetrically；The motor mount is used to install motor and connection horn, and propeller is installed on motor shaft.It is described
Horn, horn mounting seat, motor mount, motor and propeller are four.
As shown in fig. 7, unmanned plane is dropped on landing round platform, linear electric motors driving sliding axle, and the cunning being connected through
Dynamic push rod is by initial position 1（It is the position of unmanned plane in Fig. 7）；As shown in figure 8, pusher is moved forward, nobody is reached
Put 2 in seat in the plane（It is the position of unmanned plane in Fig. 8）, unmanned plane nose-gear contacted with pusher, and unmanned plane is pushed forward；
As shown in figure 9, when only one of which undercarriage is contacted in pusher, due to the influence of unbalance of stress, making unmanned plane automatic
Correct head to point to, and finally balance two pin of nose-gear, while contact slide push rod is promoted forward, when arrival position
When putting 4（It is such as the position of unmanned plane in Figure 10）, because Y type guide rails have spacing guide effect, aircraft can be forced to exist
Also to landing round platform central motion when travelling forward, and the neck of guide rail is finally reached, reaches position 5（Such as unmanned plane in Figure 11
Position）, when pusher promotes unmanned plane in-position 5（Such as the position of unmanned plane in Figure 11）When, pusher end face
Hall sensor sensing is located at the induced magnet 8 of Y type guide rails side, and triggers halt instruction, and linear electric motors are stopped, this
When, the male socket of Y type guide rail ends inserts the female socket of unmanned plane tail, and the contact chip of two socket correspondence positions starts phase
The circuit of connection needed for mutually contacting and connect, and charger automatic charging is controlled by controller.After charging is finished, movable handgrip
The undercarriage of unmanned plane is caught, is dragged outward（As shown in Figure 12）；Unmanned plane is dragged to the position at landing round platform center by movable handgrip
Put（It is the unmanned plane position in Figure 13）；Movable handgrip is decontroled as shown in figure 14；Finally, as shown in figure 15, movable handgrip
Original position is returned in the presence of sliding axle and linear electric motors；Unmanned plane starts to take off.
When the voltage sensor on controller senses that voltage reaches preset value, control charger stops charging, and touches
The endless screw electric motor in pusher is sent out, control activity handgrip rotation 180 degree grabs the unmanned plane undercarriage in front of through push rod, now directly
Line motor starts control sliding axle and exits motion backward, and due to promptly acting for movable handgrip, unmanned plane, which is driven, follows cunning
Dynamic push rod exits the neck and breakaway plug of Y type guide rails, when guide rail moves to 7 position of induced magnet, linear electric motors pause fortune
Dynamic, endless screw electric motor control activity handgrip rotation 180 degree unclamps unmanned plane, and linear electric motors continue to drive sliding axle to be withdrawn into initial bit
Put 1（It is the position of pusher in Fig. 7）.
The utility model on aircraft landing round platform by installing Y type guide rails, and the end of Y type guide rails is provided with one
Think corresponding neck with unmanned plane undercarriage so that unmanned plane, which can be fixed in the neck of Y type guide rails, to charge；In Y type guide rails
Male socket is installed, the female socket with unmanned aerial vehicle body side is corresponding above end；When unmanned plane drops to flight
On the position of device landing round platform, the pusher on Y type guide rails, and the center of pusher is connected with sliding axle, and
Sliding axle is under the driving of linear electric motors, and sliding axle promotes pusher motion, and then promotes on aircraft landing round platform
Unmanned plane is moved so that unmanned plane can be moved along the edge of Y type guide rails, and then enter in neck, and unmanned plane rises and falls
Frame is corresponding with neck chimeric so that the female socket and plug of unmanned plane is corresponding；It can be slided after realizing unmanned plane landing
Push rod, which is pushed in the neck of Y type guide rail ends, to be charged, and without manual control in whole process, utilizes pusher and Y
The position-limiting action of type guide rail, realizes that being refined control after unmanned plane landing arrives in spacing neck, realizes that unmanned plane is auxiliary with ground
Help the circuit of equipment to connect, so as to realize the functions such as digital independent, transmission and automatic charging, realize the terrestrial operation of unmanned plane
It is unmanned；By the spacing guiding function of Y type guide rails, pusher is set only to be accurate to by moving forward and backward i.e. controllable unmanned plane
Charging equipment is connected up to required position and automatically, it is simple and reliable for structure；By using the male socket and female socket of pairing, make
The circuit that must be connected is more, solves monolithic voltage balance, the test problems of many battery core assembled batteries during automatic charging；It is logical
Cross the use of Y types guide rail and pusher, the pixel accuracy requirement step-down for making unmanned plane land automatically, make UAS completely without
Realizing for peopleization operation is more reliable.
It should be appreciated that application of the present utility model is not limited to above-mentioned citing, those of ordinary skill in the art are come
Say, can according to the above description be improved or converted, all these modifications and variations should all belong to the appended power of the utility model
The protection domain that profit is required.
Claims (8)
1. a kind of full-automatic connecting platform of unmanned plane, it is characterised in that including sliding axle, Y types guide rail, pusher, straight-line electric
Machine, endless screw electric motor, movable handgrip, the plug for charging or transmitting data and aircraft landing round platform；The sliding axle passes through
Mounting bracket is fixed on landing round platform, and one end close to Y type guide rails is connected with pusher, the both sides of pusher central point
Endless screw electric motor is installed, endless screw electric motor is by the turned position of gear control activity handgrip, and movable handgrip is mobilizable to be arranged on
In pusher, the end of the Y types guide rail is provided with neck, openings of sizes and the shoulder phase of aircraft nose-gear two of the neck
Deng, and male socket is provided with by support above Y types guide rail end, the male socket is inserted with the female installed on unmanned plane
Seat matches；The linear electric motors are moved forward by the pusher for driving sliding axle to fix, and promote unmanned plane to enter Y types
In the neck of guide rail, unmanned plane is caught by endless screw electric motor rotation activity handgrip when exiting and the release of landing region is pulled out to.
2. the full-automatic connecting platform of unmanned plane according to claim 1, it is characterised in that the pusher wherein one end
End face on sensor is installed.
3. the full-automatic connecting platform of unmanned plane according to claim 2, it is characterised in that the sensor is hall sensing
Device, and the position of correspondence pusher motion, induced magnet is provided with the side of Y type guide rails.
4. the full-automatic connecting platform of unmanned plane according to claim 2, it is characterised in that the sensor passes for infrared ray
Sensor, and the position of correspondence pusher motion, infrared receiver is provided with the side of Y type guide rails.
5. the full-automatic connecting platform of unmanned plane according to claim 4, it is characterised in that the motion bit of the pusher
Put respectively original position, centre position and terminal position.
6. the full-automatic connecting platform of unmanned plane according to claim 1, it is characterised in that install the male socket front end
There is the contact copper sheet being connected with wire.
7. the full-automatic connecting platform of unmanned plane according to claim 6, it is characterised in that the wire include power line,
Data transmission line, data receiver line, charging wire, ground wire.
8. the full-automatic connecting platform of unmanned plane according to claim 1, it is characterised in that the unmanned plane can be four rotations
Any one in wing unmanned plane, six rotor wing unmanned aerial vehicles, eight rotor wing unmanned aerial vehicles.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621350334.2U CN206494119U (en) | 2016-12-09 | 2016-12-09 | A kind of full-automatic connecting platform of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621350334.2U CN206494119U (en) | 2016-12-09 | 2016-12-09 | A kind of full-automatic connecting platform of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206494119U true CN206494119U (en) | 2017-09-15 |
Family
ID=59800288
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621350334.2U Withdrawn - After Issue CN206494119U (en) | 2016-12-09 | 2016-12-09 | A kind of full-automatic connecting platform of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206494119U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106542091A (en) * | 2016-12-09 | 2017-03-29 | 佛山科学技术学院 | A kind of full-automatic connecting platform of unmanned plane |
| CN108482697A (en) * | 2018-06-06 | 2018-09-04 | 深圳草莓创新技术有限公司 | A kind of unmanned plane automatic positioning charging unit and its method |
| JP7466890B2 (en) | 2020-03-05 | 2024-04-15 | 国立大学法人東北大学 | Passive guidance mechanism and aircraft landing system |
-
2016
- 2016-12-09 CN CN201621350334.2U patent/CN206494119U/en not_active Withdrawn - After Issue
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106542091A (en) * | 2016-12-09 | 2017-03-29 | 佛山科学技术学院 | A kind of full-automatic connecting platform of unmanned plane |
| CN108482697A (en) * | 2018-06-06 | 2018-09-04 | 深圳草莓创新技术有限公司 | A kind of unmanned plane automatic positioning charging unit and its method |
| CN108482697B (en) * | 2018-06-06 | 2023-09-19 | 深圳草莓创新技术有限公司 | Unmanned aerial vehicle automatic positioning charging device and method thereof |
| JP7466890B2 (en) | 2020-03-05 | 2024-04-15 | 国立大学法人東北大学 | Passive guidance mechanism and aircraft landing system |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20170915 Effective date of abandoning: 20180814 |