CN205790709U - Unmanned plane interface automatic butt system - Google Patents
Unmanned plane interface automatic butt system Download PDFInfo
- Publication number
- CN205790709U CN205790709U CN201620454487.5U CN201620454487U CN205790709U CN 205790709 U CN205790709 U CN 205790709U CN 201620454487 U CN201620454487 U CN 201620454487U CN 205790709 U CN205790709 U CN 205790709U
- Authority
- CN
- China
- Prior art keywords
- axis
- unmanned plane
- undercarriage
- adjustable stem
- landing platform
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
This utility model relates to unmanned air vehicle technique field, provide unmanned plane interface automatic butt system, including the unmanned plane with undercarriage, landing platform, it is located at the aligning gear on landing platform and controls the control device of aligning gear, aligning gear includes laying respectively at the X-axis adjustable stem that undercarriage can be corrected by undercarriage both sides, lay respectively at the Y-axis adjustable stem that undercarriage can be corrected by the another both sides of undercarriage and the X-axis being positioned at the landing platform back side drives structure and Y-axis to drive structure, undercarriage is provided with interface block, X-axis adjustable stem or Y-axis adjustable stem are provided with and can dock with interface block for being charged unmanned plane and/or the joint of data interaction, control device drives structure and Y-axis to drive structure to electrically connect with X-axis.The problem that this utility model solves the required precision height that in unmanned plane automatic charging lands unmanned plane in prior art, landing place adjusts difficulty, landing place calibration structure is complicated, cost height, interface difficulty are docked.
Description
Technical field
This utility model relates to unmanned air vehicle technique field, more specifically, relating to a kind of unmanned plane interface automatic butt
System.
Background technology
Unmanned air vehicle technique achieves tremendous development in recent years, especially its have advantage of lower cost, no one was injured risk,
The advantages such as survival ability is strong, mobility good, easy to use so that unmanned plane is widely used in forestry monitoring, agricultural plant protection, electricity
The fields such as power line walking, express delivery transport, public security, frontier defense and intelligent transportation.Such as unmanned plane is being applied to Management of City Traffic
Time, use large number of unmanned plane to perform corresponding task while needing long-time, high frequency time, and unmanned plane long-time,
It is required for being charged frequently or carrying out data interaction during high frequency time work.
At present, in Normal practice, it is to control unmanned plane by landing bootstrap technique to drop to unmanned plane with specific course
On charging device, it is then that the unmanned plane dropped on unmanned plane charging device is charged or data interaction by staff.
So, although the most more convenient, but remain a need for substantial amounts of artificial input, and when working outside, manual operation is inconvenient.
Prior art also has some unmanned functions realize in the case of entirely without manual intervention timing or continuous print from
Start building to make, and drop to realize on charging base station automatic charging or the data interaction of unmanned plane by unmanned plane.But, have from
In dynamic charging system, charger is fixing, by adjusting the position of unmanned plane so that unmanned plane drops to charging exactly
Realize charging or data interaction on equipment, and have plenty of and calibrate unmanned seat in the plane by straight-line motion mechanism after unmanned plane lands
Put, then connected the charging inlet of automatic charging system and unmanned plane by mechanical arm.In former charging system, to unmanned plane
Pinpoint landing precision require height, and for electric quantity of power supply this with regard to little unmanned plane for, if repeatedly adjusting landing place, show
So can bring the biggest burden；In latter charging system, although comparing the former to decrease the difficulty of unmanned plane landing, but need
Two groups of motions realize calibrating unmanned plane position and charging inlet to connection function, system complex respectively, it is achieved cost is high, difficulty
Greatly.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane automatic charging system, it is intended to solve in prior art unmanned
, landing place adjustment difficulty, landing place calibration structure complexity, cost high to unmanned plane landing required precision in machine automatic charging
High, the problem of interface difficulty docking.
For solving above-mentioned technical problem, the technical solution of the utility model is: provide a kind of unmanned plane interface automatic butt
System, including having the unmanned plane of undercarriage, landing platform, being located on described landing platform for by the undercarriage school of unmanned plane
Just and be fixed to the aligning gear of described landing platform predeterminated position and control the control device of described aligning gear, described school
Positive mechanism includes laying respectively at X-axis adjustable stem, the difference position that described undercarriage X-direction can be corrected by described undercarriage both sides
The Y-axis adjustable stem that described undercarriage Y-direction can be corrected in the another both sides of described undercarriage and be positioned at described landing platform
The back side drives described X-axis adjustable stem to drive structure and Y-axis to drive structure, described undercarriage with the X-axis of described Y-axis adjustable stem respectively
It is provided with interface block, described X-axis adjustable stem or described Y-axis adjustable stem to be provided with and can dock for described nothing with described interface block
Man-machine being charged and/or the joint of data interaction, described control device and described X-axis drive structure and described Y-axis to drive knot
Structure electrically connects.
Alternatively, described X-axis drives structure to include the X-axis being fixed on the described landing platform back side and arranging along X-direction
Bidirectional-screw, the X-axis driving described X-axis Bidirectional-screw to rotate drive motor and are respectively arranged on the two of described X-axis Bidirectional-screw
End and can be towards or away from the X-axis feed screw nut of movement, each described X-axis feed screw nut and least one set can be moved along X-direction
Dynamic X-axis slide assemblies is fixing to be connected, and described X-axis adjustable stem is fixing with described X-axis slide assemblies to be connected, and described X-axis drives electricity
Machine electrically connects with described control device.
Alternatively, described X-axis slide assemblies is four groups, and each described X-axis feed screw nut is respectively symmetrically along the both sides of Y direction
X-axis slide assemblies described in two groups is set, is positioned at X-axis slide assemblies described in two groups of described X-axis Bidirectional-screw the same side and is positioned at same
On one straight line.
Alternatively, described X-axis slide assemblies includes the X-axis guide rail arranged along X-direction and is slidedly arranged on described X-axis guide rail
On X-axis slide block, be positioned at two X-axis slide blocks of each described X-axis feed screw nut not homonymy and connect by a head rod is fixing, institute
State landing platform and be provided with the first chute being available for the slip of each described X-axis slide block, each described X-axis slide block and described X-axis adjustable stem
Fixing connection.
Alternatively, the described landing platform back side is additionally provided with and opens for the X-axis position sensing described X-axis feed screw nut position
Closing, described X-axis position switch electrically connects with described control device.
Alternatively, described Y-axis drives structure to include the Y-axis being fixed on the described landing platform back side and arranging along Y direction
Bidirectional-screw, the Y-axis driving described Y-axis Bidirectional-screw to rotate drive motor and are respectively arranged on the two of described Y-axis Bidirectional-screw
End and can be towards or away from the Y-axis feed screw nut of movement, each described Y-axis feed screw nut and least one set can be moved along Y direction
Dynamic Y-axis slide assemblies is fixing to be connected, and described Y-axis adjustable stem is fixing with described Y-axis slide assemblies to be connected, and described Y-axis drives electricity
Machine electrically connects with described control device.
Alternatively, described Y-axis slide assemblies is four groups, and each described Y-axis feed screw nut is respectively symmetrically along the both sides of X-direction
Y-axis slide assemblies described in two groups is set, is positioned at Y-axis slide assemblies described in two groups of described Y-axis Bidirectional-screw the same side and is positioned at same
On one straight line.
Alternatively, described Y-axis slide assemblies includes the Y-axis guide rail arranged along Y direction and is slidedly arranged on described Y-axis guide rail
On Y-axis slide block, be positioned at two Y-axis slide blocks of each described Y-axis feed screw nut not homonymy and connect by one second connecting rod is fixing, institute
State landing platform and be provided with the second chute being available for the slip of each described Y-axis slide block, each described Y-axis slide block and described Y-axis adjustable stem
Fixing connection.
Alternatively, the described landing platform back side is additionally provided with and opens for the Y-axis position sensing described Y-axis feed screw nut position
Closing, described Y-axis position switch electrically connects with described control device.
Alternatively, also include that battery charger, described undercarriage include two parallel pipes for supporting described unmanned plane, institute
Stating interface block is four, is respectively equipped with interface block described in outside the both ends of each described parallel pipe, each described interface block with
Described parallel pipe is parallel, and the both ends of the adjustable stem being not provided with described joint all extend internally for compressing described interface block
Extension, described battery charger is electrically connected by wire with described joint.
The unmanned plane interface automatic butt system that this utility model provides has the advantages that
One, the landing gear position utilizing two groups of adjustable stem correction unmanned planes reaches to revise the mesh of unmanned plane landing place
, reduce the burden of unmanned plane landing precision requirement, it is easier to realize unmanned plane rapid descent, shorten the landing time, carry
High workload efficiency；
Two, for having the unmanned plane of undercarriage, on the premise of not changing former housing construction, outside four of undercarriage
Wide position mounting interface seat gets final product interface automatic butt system in adaptive the present embodiment, completes automatic charging and/or automatically transmits
Deng, therefore, the unmanned plane kind being suitable for is wider with specification limit；
Three, the joint docked with interface block is located on adjustable stem, when X-axis adjustable stem moves to respectively with Y-axis adjustable stem
After Wei, i.e. correct unmanned plane landing place, meanwhile, also secure unmanned plane, and complete the automatic butt of interface block and joint,
Quickly realize unmanned plane landing after be charged and/data interaction before preparation；
Four, X-axis adjustable stem and Y-axis adjustable stem are plane move toward one another, by adjusting position and the Y-axis of X-axis position switch
The position of position switch, makes X-axis adjustable stem be parked in different positions from Y-axis adjustable stem to adapt to the undercarriage of different span, from
And adapt to the unmanned plane of different size；
Five, X-axis adjustable stem and Y-axis adjustable stem two orthogonal directions in plane move, and only need one in each direction
Driver part, X-direction and Y direction action in a fixed order respectively, it is not necessary to coupled movements, mechanism kinematic and driving control
Simply, reliability is high, low cost.
Accompanying drawing explanation
Fig. 1 is that the unmanned plane that this utility model embodiment provides drops to the top view on landing platform；
Fig. 2 is the schematic rear view of the landing plane that this utility model embodiment provides；
Fig. 3 is the top view of the undercarriage of the unmanned plane that this utility model embodiment provides；
Fig. 4 is the side view of the undercarriage of the unmanned plane that this utility model embodiment provides；
Fig. 5 is the structure flow chart of the unmanned plane interface automatic butt system that this utility model embodiment provides；
100-unmanned plane；110-undercarriage；111-parallel pipe；
120-interface block；200-landing platform；210-X axle adjustable stem；
211-extension；220-Y axle adjustable stem；230-X axle drives structure；
231-X axle Bidirectional-screw；232-X axis drive motor；233-X axial filament stem nut；
234-X axle slide assemblies；2341-X axis rail；2342-X axle slide block；
235-head rod；236-X shaft position switchs；240-Y axle drives structure；
241-Y axle Bidirectional-screw；242-Y axis drive motor；243-Y axial filament stem nut；
244-Y axle slide assemblies；2441-Y axis rail；2442-Y axle slide block；
245-the second connecting rod；246-Y shaft position switchs；250-joint；
260-landing plane；270-battery charger.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearer, below in conjunction with accompanying drawing and enforcement
Example, is further elaborated to this utility model.Should be appreciated that specific embodiment described herein is only in order to explain
This utility model, is not used to limit this utility model.
It should be noted that when element is referred to as " being fixed on " or " being arranged at " another element, and it can be directly separately
On one element or may be simultaneously present centering elements.When an element is referred to as " being connected to " another element, and it is permissible
It is directly to another element or may be simultaneously present centering elements.
Also, it should be noted the orientation term such as left and right, upper and lower in the present embodiment, be only each other relative concept or
With the normal operating condition of product as reference, and should not be regarded as restrictive.
The unmanned plane interface automatic butt system that this utility model embodiment provides, directly participate in completely without people
In the case of, it is achieved the automatic butt of interface, it is widely used in unmanned plane carrying out automatic charging or unmanned plane being carried out data friendship
Mutually, or unmanned plane is carried out automatic charging and data interaction simultaneously, or otherwise automatic supply etc..
With reference to Fig. 1, Fig. 2 and Fig. 5, unmanned plane interface automatic butt system include having undercarriage 110 unmanned plane 100,
Landing platform 200, it is located on landing platform 200 for the undercarriage 110 of unmanned plane 100 being corrected and being fixed to landing platform
The aligning gear of 200 predeterminated positions and the control device (not shown) of control aligning gear.Aligning gear includes being located at
Two X-axis adjustable stem 210, two Y-axis adjustable stems 220 above landing platform 200, it is located at landing platform 200 back side and drives two X-axis schools
Positive bar 210 drives structure 230 and the Y-axis driving two Y-axis adjustable stems 220 to move along Y direction along the X-axis that X-direction moves
Drive structure 240.Two X-axis adjustable stems 210 lay respectively at the undercarriage 110 both sides along X-direction, can be to undercarriage 110X direction
It is corrected.In the present embodiment, undercarriage 110 is provided with interface block 120, and Y-axis adjustable stem 220 is provided with can be with interface block 120
Docking, for being charged unmanned plane 100 and/or the joint 250 of data interaction, controls device and drives structure 230 and Y with X-axis
Axle drives structure 240 to electrically connect.It is of course also possible to joint 250 is arranged on X-axis adjustable stem 210.
In the present embodiment, landing platform 200 includes the smooth landing plane 260 of a surfacing, supports landing plane 260
Column (not shown), be fixed on the base plate (not shown) of column bottom and that each part mentioned above is connected as one is whole
The framework (not shown) of body.Two X-axis adjustable stem 210, two Y-axis adjustable stems 220 are positioned at above landing plane 260, for school
Positive unmanned plane 100, X-axis drives structure 230, Y-axis to drive the parts such as structure 240 and control device to be then positioned at landing platform 200
Internal.
In the present embodiment, control device and include controlling device and control system, drive knot for ground communication and adjustable stem
The control of structure, thus realize automatic charging and/or the data interaction etc. of unmanned plane 100.
Specifically, as in figure 2 it is shown, X-axis drives structure 230 to include being fixed on landing plane 260 back side and setting along X-direction
The X-axis Bidirectional-screw 231 put, the X-axis driving X-axis Bidirectional-screw 231 to rotate drive motor 232 and to be respectively arranged on X-axis two-way
The both ends of screw mandrel 231 and can be towards or away from the X-axis feed screw nut 233 of movement.X-axis drives motor 232 and controls device electricity
Connect.The screw thread at X-axis Bidirectional-screw 231 two ends is respectively left-handed and dextrorotation, when X-axis drives motor 232 to drive X-axis Bidirectional-screw
During 231 forward or reverse, i.e. opposing along X-axis Bidirectional-screw 231 with the X-axis feed screw nut 233 of two ends threaded engagement respectively or phase
To motion.As can be seen from Figure, each X-axis feed screw nut 233 is respectively symmetrically along the both sides of Y direction that to arrange two groups of X-axis sliding
Dynamic assembly 234, the two groups of X-axis slide assemblies 234 being positioned at each X-axis Bidirectional-screw 231 the same side are located along the same line.This
Sample, is i.e. to have four groups of X-axis slide assemblies 234.Each X-axis adjustable stem 210 and the two groups of X being positioned at X-axis feed screw nut 233 both sides
Axle slide assemblies 234 is fixing to be connected.
X-axis slide assemblies 234 includes the X-axis guide rail 2341 arranged along X-direction and is slidedly arranged on X-axis guide rail 2341
X-axis slide block 2342, the two X-axis slide blocks 2342 being positioned at each X-axis feed screw nut 233 not homonymy are fixed by a head rod 235
Connecting, landing platform 200 is provided with and is available for the first chute (not shown) that each X-axis slide block 2342 slides, each X-axis slide block
2342 fixing with X-axis adjustable stem 210 are connected.
In the present embodiment, it is additionally provided with the X-axis position for sensing X-axis feed screw nut 233 position at landing plane 260 back side
Switch 236, X-axis position switch 236 electrically connects with controlling device.When X-axis feed screw nut 233 moves and touches X-axis position switch
After 236, position switch feed back motion stops signal and drives motor 232 to stop operating to control device, control device control X-axis,
I.e. X-axis adjustable stem 210 motion puts in place stop motion.
In the present embodiment, Y-axis drives structure 240 to include the Y being fixed on landing plane 260 back side and arranging along Y direction
Axle Bidirectional-screw 241, the Y-axis driving Y-axis Bidirectional-screw 241 to rotate drive motor 242 and are respectively arranged on Y-axis Bidirectional-screw
The both ends of 241 and can be towards or away from the Y-axis feed screw nut 243 of movement.Y-axis drives motor 242 to electrically connect with controlling device.
Same, the screw thread at Y-axis Bidirectional-screw 241 two ends is respectively left-handed and dextrorotation, when Y-axis drives motor 242 to drive the two-way silk of Y-axis
During bar 241 forward or reverse, i.e. opposing along Y-axis Bidirectional-screw 241 with the Y-axis feed screw nut 243 of two ends threaded engagement respectively or
Move toward one another.As can be seen from Figure, each Y-axis feed screw nut 243 is respectively symmetrically along the both sides of X-direction and arranges two groups of Y-axis
Slide assemblies 244, the two groups of Y-axis slide assemblies 244 being positioned at each Y-axis Bidirectional-screw 241 the same side are located along the same line.This
Sample, is i.e. to have four groups of Y-axis slide assemblies 244.Each Y-axis adjustable stem 220 and the two groups of Y being positioned at Y-axis feed screw nut 243 both sides
Axle slide assemblies 244 is fixing to be connected.
Y-axis slide assemblies 244 includes the Y-axis guide rail 2441 arranged along Y direction and is slidedly arranged on Y-axis guide rail 2441
Y-axis slide block 2442, the two Y-axis slide blocks 2442 being positioned at each Y-axis feed screw nut 243 not homonymy are fixed by one second connecting rod 245
Connecting, landing platform 200 is provided with and is available for the second chute that each Y-axis slide block 2442 slides, and each Y-axis slide block 2442 corrects with Y-axis
Bar 220 is fixing to be connected.
Same, landing plane 260 back side is additionally provided with the Y-axis position switch for sensing Y-axis feed screw nut 243 position
246, Y-axis position switch 246 electrically connects with controlling device.When Y-axis feed screw nut 243 moves and touches Y-axis position switch 246
After, position switch feed back motion stops signal and drives motor 242 to stop operating to control device, control device control Y-axis, i.e. Y
Axle adjustable stem 220 motion puts in place stop motion.
In the present embodiment, X-axis adjustable stem 210 and Y-axis adjustable stem 220 are plane move toward one another, as such, it is possible to by adjusting
The position of X-axis position switch 236 and the position of Y-axis position switch 246, make X-axis adjustable stem 210 and Y-axis adjustable stem 220 be parked in not
Same position adapts to the undercarriage 110 of different span, thus adapts to the unmanned plane 100 of different size.
And, X-axis adjustable stem 210 and Y-axis adjustable stem 220 two orthogonal directions in plane move, in each direction
Only need a driver part, X-direction and Y direction action in a fixed order respectively, it is not necessary to coupled movements, mechanism kinematic and
Driving and control simply, reliability is high, low cost.
With reference to Fig. 3, Fig. 4, the undercarriage 110 of unmanned plane 100 includes two parallel pipes 111 for supporting unmanned plane 100, connects
Mouth seat 120 is four, and interface block 120 is four, is respectively equipped with an interface block 120, respectively outside the both ends of each parallel pipe 111
Interface block 120 is parallel with parallel pipe 111.In the present embodiment, joint 250 is located on Y-axis adjustable stem 220, and is not provided with joint 250
The both ends of X-axis adjustable stem 210 all extend internally the extension 211 for compressing interface block 120.Same, work as joint
250 when being located on X-axis adjustable stem 210, then extension 211 is correspondingly arranged at the two ends of the Y-axis adjustable stem 220 being not provided with joint 250
Inside portion.
Referring again to Fig. 1, in the present embodiment, unmanned plane 100 interface automatic butt system also includes battery charger 270,
Battery charger 270 electrically connects with joint 250.So, when interface block 120 and the joint of Y-axis adjustable stem 220 of unmanned plane 100
After 250 docking, i.e. realize charging automatically, biography and the storage down of data can also be carried out while charging.Certainly, battery fills
Electrical equipment 270 can also directly be replaced by the main frame with data storage function, and main frame electrically connects with joint 250, and passes through joint
250 realize the Data Over Cable transmission of unmanned plane 100 with the electrical connection of interface block 120.
With reference to Fig. 1, Fig. 5, in the present embodiment, workflow and the principle of unmanned plane 100 interface automatic butt system be: nothing
Man-machine 100 drop in the smooth landing plane 260 of landing platform 200, and now unmanned plane 100 is positioned at two X in landing plane 260
In the moving region of axle adjustable stem 210 and two Y-axis adjustable stems 220, it is positioned at two X-axis corrections of both sides in landing platform 200 plane
Bar 210 is driven by X-axis slide block 2342 under X-axis drives the driving of motor 232 yearns for central area motion, two X-axis schools mutually
Positive bar 210 promotes undercarriage 110 to move along X axis central area, after X-axis adjustable stem 210 motion puts in place, unmanned plane 100
Axis overlaps with Y-axis, and now, two parallel pipes 111 and interface block 120 bottom undercarriage 110 are inside by X-direction both ends
The extension 211 arranged compresses constraint, and now, undercarriage 110 only has the one-movement-freedom-degree in Y direction；Then, two Y-axis
Adjustable stem 220 is driven by Y-axis slide block 2442 under Y-axis drives the driving of motor 242 yearns for central area motion, mutually when two
Y-axis adjustable stem 220 promotes undercarriage 110 to move along Y direction after contacting with undercarriage 110, treats that Y-axis adjustable stem 220 moves to
After Wei, now unmanned plane 100 is positioned to the central area of landing plane 260, be positioned at connecing of Y-axis adjustable stem 220 two ends simultaneously
250 dock respectively with the interface block 120 on undercarriage 110 and compress, being automatically positioned and connecing after so far unmanned plane 100 landing
Mouth automatic butt has worked；Control device and send charging instruction, by docking of joint 250 and interface block 120, start nothing
Man-machine 100 are charged.Charging can individually complete, it is also possible to while charging, utilize wire carry out the biography down of data with
Storage, or, it is also possible to individually carry out biography and the storage down of data.
After charging and/or data interaction complete, after unmanned plane 100 start, control device and send instruction, two X-axis corrections
The opposing motion of order in no particular order of bar 210 and two Y-axis adjustable stems 220, i.e. moves away from unmanned plane 100, when two X-axis adjustable stems
210 and two Y-axis adjustable stem 220 move and move to after landing plane 260 marginal position stops respectively, unmanned plane 100 takes off, it is achieved
Letting fly away of unmanned plane 100.
To sum up, the unmanned plane 100 interface automatic butt system that this utility model provides has the advantages that
One, undercarriage 110 position utilizing two groups of adjustable stem correction unmanned planes 100 reaches to revise unmanned plane 100 and lands
The purpose of position, reduces unmanned plane 100 and lands the burden of precision requirement, it is easier to realize unmanned plane 100 rapid descent, contracting
The short landing time, improve work efficiency；
Two, for having the unmanned plane 100 of undercarriage 110, on the premise of not changing former housing construction, at undercarriage
Four gabarit position mounting interface seats 120 of 110 get final product interface automatic butt system in adaptive the present embodiment, complete automatic charging
And/or automatic transmission etc., therefore, the unmanned plane kind being suitable for is wider with specification limit；
Three, the joint 250 docked with interface block 120 is located on adjustable stem, when X-axis adjustable stem 210 and Y-axis adjustable stem
220 respectively motion put in place after, i.e. correct unmanned plane 100 landing place, meanwhile, also secure unmanned plane 100, and complete interface
Seat 120 and the automatic butt of joint 250, be charged after quickly realizing unmanned plane 100 landing and preparation before/data interaction
Work；
Four, X-axis adjustable stem 210 and Y-axis adjustable stem 220 are plane move toward one another, by adjusting X-axis position switch 236
Position and the position of Y-axis position switch 246, make X-axis adjustable stem 210 be parked in different positions from Y-axis adjustable stem 220 and adapt to not
With the undercarriage 110 of span, thus adapt to the unmanned plane 100 of different size；
Five, X-axis adjustable stem 210 and Y-axis adjustable stem 220 two orthogonal directions in plane move, in each direction only
Need a driver part, X-direction and Y direction action in a fixed order respectively, it is not necessary to coupled movements, mechanism kinematic and driving
Dynamic control is simple, and reliability is high, low cost.
These are only preferred embodiment of the present utility model, not in order to limit this utility model, all in this practicality
Any amendment, equivalent and the improvement etc. made within novel spirit and principle, should be included in guarantor of the present utility model
Within the scope of protecting.
Claims (10)
1. unmanned plane interface automatic butt system, it is characterised in that: include there is the unmanned plane of undercarriage, landing platform, be located at
For the undercarriage of unmanned plane corrects and is fixed to the aligning gear of described landing platform predeterminated position on described landing platform
And controlling the control device of described aligning gear, described aligning gear includes laying respectively at described undercarriage both sides can be to described
X-axis adjustable stem that undercarriage X-direction is corrected, lay respectively at the another both sides of described undercarriage and described undercarriage Y-direction can be entered
The Y-axis adjustable stem of row correction and be positioned at the described landing platform back side and drive described X-axis adjustable stem and described Y-axis adjustable stem respectively
X-axis drive structure and Y-axis to drive structure, described undercarriage is provided with interface block, described X-axis adjustable stem or the correction of described Y-axis
Bar is provided with and can dock with described interface block for being charged described unmanned plane and/or the joint of data interaction, described control
Device processed drives structure and described Y-axis to drive structure to electrically connect with described X-axis.
2. unmanned plane interface automatic butt system as claimed in claim 1, it is characterised in that: described X-axis drives structure to include
It is fixed on the described landing platform back side and the X-axis Bidirectional-screw arranged along X-direction, the X that drives described X-axis Bidirectional-screw to rotate
Axis drive motor and be respectively arranged on described X-axis Bidirectional-screw both ends and can towards or away from the X-axis feed screw nut of movement,
Each described X-axis feed screw nut can be connected along the X-axis slide assemblies that X-direction moves is fixing with least one set, described X-axis adjustable stem
Fixing with described X-axis slide assemblies and be connected, described X-axis drives motor to electrically connect with described control device.
3. unmanned plane interface automatic butt system as claimed in claim 2, it is characterised in that: described X-axis slide assemblies is four
Group, each described X-axis feed screw nut is respectively symmetrically along the both sides of Y direction and arranges X-axis slide assemblies described in two groups, is positioned at described X
X-axis slide assemblies described in two groups of axle Bidirectional-screw the same side is located along the same line.
4. unmanned plane interface automatic butt system as claimed in claim 3, it is characterised in that: described X-axis slide assemblies includes
Along X-direction arrange X-axis guide rail and be slidedly arranged on the X-axis slide block on described X-axis guide rail, be positioned at each described X-axis feed screw nut
Two X-axis slide blocks of homonymy do not connect by a head rod is fixing, and described landing platform is provided with and is available for each described X-axis slide block
The first chute slided, each described X-axis slide block is fixing with described X-axis adjustable stem to be connected.
5. the unmanned plane interface automatic butt system as described in Claims 2 or 3 or 4, it is characterised in that: described landing platform
The back side is additionally provided with the X-axis position switch for sensing described X-axis feed screw nut position, described X-axis position switch and described control
Device electrically connects.
6. unmanned plane interface automatic butt system as claimed in claim 1, it is characterised in that: described Y-axis drives structure to include
It is fixed on the described landing platform back side and the Y-axis Bidirectional-screw arranged along Y direction, the Y that drives described Y-axis Bidirectional-screw to rotate
Axis drive motor and be respectively arranged on described Y-axis Bidirectional-screw both ends and can towards or away from the Y-axis feed screw nut of movement,
Each described Y-axis feed screw nut can be connected along the Y-axis slide assemblies that Y direction moves is fixing with least one set, described Y-axis adjustable stem
Fixing with described Y-axis slide assemblies and be connected, described Y-axis drives motor to electrically connect with described control device.
7. unmanned plane interface automatic butt system as claimed in claim 6, it is characterised in that: described Y-axis slide assemblies is four
Group, each described Y-axis feed screw nut is respectively symmetrically along the both sides of X-direction and arranges Y-axis slide assemblies described in two groups, is positioned at described Y
Y-axis slide assemblies described in two groups of axle Bidirectional-screw the same side is located along the same line.
8. unmanned plane interface automatic butt system as claimed in claim 7, it is characterised in that: described Y-axis slide assemblies includes
Along Y direction arrange Y-axis guide rail and be slidedly arranged on the Y-axis slide block on described Y-axis guide rail, be positioned at each described Y-axis feed screw nut
Two Y-axis slide blocks of homonymy do not connect by one second connecting rod is fixing, and described landing platform is provided with and is available for each described Y-axis slide block
The second chute slided, each described Y-axis slide block is fixing with described Y-axis adjustable stem to be connected.
9. the unmanned plane interface automatic butt system as described in claim 6 or 7 or 8, it is characterised in that: described landing platform is carried on the back
Face is additionally provided with the Y-axis position switch for sensing described Y-axis feed screw nut position, and described Y-axis position switch controls dress with described
Put electrical connection.
10. unmanned plane interface automatic butt system as claimed in claim 1, it is characterised in that: also include battery charger, institute
Stating undercarriage and include two parallel pipes for supporting described unmanned plane, described interface block is four, the two of each described parallel pipe
Being respectively equipped with interface block described in outside end, each described interface block is parallel with described parallel pipe, is not provided with the school of described joint
The both ends of positive bar all extend internally the extension for compressing described interface block, and described battery charger leads to described joint
Cross wire electrical connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620454487.5U CN205790709U (en) | 2016-05-18 | 2016-05-18 | Unmanned plane interface automatic butt system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620454487.5U CN205790709U (en) | 2016-05-18 | 2016-05-18 | Unmanned plane interface automatic butt system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205790709U true CN205790709U (en) | 2016-12-07 |
Family
ID=58118598
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620454487.5U Expired - Fee Related CN205790709U (en) | 2016-05-18 | 2016-05-18 | Unmanned plane interface automatic butt system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205790709U (en) |
Cited By (8)
| 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 |
| CN107651205A (en) * | 2017-05-19 | 2018-02-02 | 成都天麒科技有限公司 | Unmanned plane positions power taking cell system |
| CN108340329A (en) * | 2018-04-24 | 2018-07-31 | 深圳市劲拓自动化设备股份有限公司 | A kind of plate position corrector |
| CN108454859A (en) * | 2018-05-16 | 2018-08-28 | 星际控股集团有限公司 | A kind of fixed mechanism of unmanned plane on intelligent warning lamp |
| CN108502201A (en) * | 2017-05-27 | 2018-09-07 | 星逻智能科技(苏州)有限公司 | Unmanned plane shuts down library |
| CN108698709A (en) * | 2017-09-30 | 2018-10-23 | 深圳市大疆创新科技有限公司 | Shut down platform, unmanned vehicle base station, the landing method of unmanned vehicle and system |
| WO2019085151A1 (en) * | 2017-10-30 | 2019-05-09 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle positioning device and parking apron |
| CN110382362A (en) * | 2017-12-28 | 2019-10-25 | 深圳市大疆创新科技有限公司 | A kind of positioning device of unmanned plane |
-
2016
- 2016-05-18 CN CN201620454487.5U patent/CN205790709U/en not_active Expired - Fee Related
Cited By (11)
| 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 |
| CN107651205A (en) * | 2017-05-19 | 2018-02-02 | 成都天麒科技有限公司 | Unmanned plane positions power taking cell system |
| CN107697314A (en) * | 2017-05-19 | 2018-02-16 | 成都天麒科技有限公司 | A kind of unmanned plane lifting gear |
| CN107697314B (en) * | 2017-05-19 | 2020-04-28 | 成都天麒科技有限公司 | Unmanned aerial vehicle take-off and landing device |
| CN108502201A (en) * | 2017-05-27 | 2018-09-07 | 星逻智能科技(苏州)有限公司 | Unmanned plane shuts down library |
| CN108698709A (en) * | 2017-09-30 | 2018-10-23 | 深圳市大疆创新科技有限公司 | Shut down platform, unmanned vehicle base station, the landing method of unmanned vehicle and system |
| CN108698709B (en) * | 2017-09-30 | 2022-03-22 | 深圳市大疆创新科技有限公司 | Shutdown platform, unmanned aerial vehicle base station, and landing method and system of unmanned aerial vehicle |
| WO2019085151A1 (en) * | 2017-10-30 | 2019-05-09 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle positioning device and parking apron |
| CN110382362A (en) * | 2017-12-28 | 2019-10-25 | 深圳市大疆创新科技有限公司 | A kind of positioning device of unmanned plane |
| CN108340329A (en) * | 2018-04-24 | 2018-07-31 | 深圳市劲拓自动化设备股份有限公司 | A kind of plate position corrector |
| CN108454859A (en) * | 2018-05-16 | 2018-08-28 | 星际控股集团有限公司 | A kind of fixed mechanism of unmanned plane on intelligent warning lamp |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205790709U (en) | Unmanned plane interface automatic butt system | |
| CN106873623B (en) | Unmanned aerial vehicle rapid autonomous endurance system and method thereof | |
| CN108328353A (en) | A kind of movable type logistics conveyer system | |
| CN202922160U (en) | Battery automatic changing system of small sized multi-rotor unmanned aerial vehicle | |
| CN207089676U (en) | Unmanned plane touch down attitude adjusts fixed system and the airplane parking area using the system | |
| CN107414783A (en) | A kind of modularization wheeled pipe robot | |
| CN105775735A (en) | Material taking mechanism for battery cores | |
| CN109483192A (en) | A kind of spatial truss unit quick fit system and method based on robot | |
| CN112706937B (en) | Flexible and accurate autonomous take-off and landing device for unmanned aerial vehicle and control method | |
| DE202020104652U1 (en) | Patient couch for a medical imaging system | |
| CN208122755U (en) | A kind of tunnel overhead working punch device | |
| CN108012825A (en) | One kind automation hydrojet control method | |
| CN105417114A (en) | Lifting type conveyor | |
| CN207386759U (en) | A kind of electronic circuit board welding mechanism | |
| CN109436385A (en) | A kind of automatic debugging system for solar wing simulation wall posture | |
| CN106114822A (en) | The dynamic many rotors agricultural plant protection helicopter flight attitude regulator control system of oil | |
| CN107323659A (en) | A kind of Intelligent unattended machine for being easy to store based on Internet of Things | |
| CN205366052U (en) | Retractable wing | |
| CN207986215U (en) | A kind of movable type logistics conveyer system | |
| CN106114832A (en) | A kind of multipurpose agricultural depopulated helicopter | |
| CN109291819A (en) | A kind of vertical charging equipment of new-energy automobile | |
| CN205293066U (en) | Empty amphibious unmanned aerial vehicle of water transfers appearance counter weight control system | |
| CN209318999U (en) | A kind of efficient laser welding machine structure | |
| CN105345806A (en) | Monitoring robot capable of ascending and descending automatically | |
| CN207139784U (en) | A kind of modularization wheeled pipe robot |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161207 Termination date: 20190518 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |