CN107757942A - The electric power supply control system of unmanned plane - Google Patents
The electric power supply control system of unmanned plane Download PDFInfo
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- CN107757942A CN107757942A CN201610695150.8A CN201610695150A CN107757942A CN 107757942 A CN107757942 A CN 107757942A CN 201610695150 A CN201610695150 A CN 201610695150A CN 107757942 A CN107757942 A CN 107757942A
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- Prior art keywords
- power supply
- unmanned plane
- component
- tumbler
- cable
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F3/00—Ground installations specially adapted for captive aircraft
- B64F3/02—Ground installations specially adapted for captive aircraft with means for supplying electricity to aircraft during flight
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- Aviation & Aerospace Engineering (AREA)
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Abstract
The present invention relates to a kind of electric power supply control system of unmanned plane, the electric power supply control system of the unmanned plane includes control terminal and administration of power supply, control terminal can produce the control instruction of the state of flight of control unmanned plane, and control terminal can also send the control signal of the work of control administration of power supply, administration of power supply can power to unmanned plane, drive component can receive control signal, and it can be worked according to control signal, drive component can drive tumbler to rotate, tumbler rotates and makes cable winds on tumbler, or cable is set to be discharged from from tumbler, cable is set to pull movable pulley component to be slided towards first direction simultaneously；Pull force calculation component can produce an elastic pulling force towards second direction, and pull force calculation component can detect value of thrust of the cable to movable pulley component, and value of thrust can be fed back to control terminal by pull force calculation component；Wherein, control terminal sends control signal according to control instruction and value of thrust.The electric power supply control system of above-mentioned unmanned plane is safer.
Description
Technical field
The present invention relates to unmanned plane field, more particularly to a kind of electric power supply control system of unmanned plane.
Background technology
Unmanned aerial vehicle body, which is directly powered, can be limited to the weight and volume of battery, and battery capacity is also limited, and
Existing unmanned plane typically can only be stagnant empty 10~30 minutes, far can not meet the needs of unmanned plane is stagnant empty for a long time.It is directed to for this
Empty demand stagnant for a long time, which is proposed, is tethered at unmanned plane product, i.e., is directly powered by land cable to aerial unmanned plane is detained,
But unwrapping wire is excessive or take-up not in time, it may appear that the situation of cable tangled up and knotted, easily trigger safety problem.
The content of the invention
Based on this, it is necessary to provide a kind of electric power supply control system of safer unmanned plane.
It a kind of electric power supply control system of unmanned plane, can be powered to unmanned plane, and can control the state of flight of the unmanned plane,
The electric power supply control system of the unmanned plane includes control terminal and administration of power supply, and the control terminal can produce the control unmanned plane
The control instruction of state of flight, and the control terminal can also send the control signal for the work for controlling the administration of power supply, it is described
Administration of power supply can give the unmanned plane to power, and the administration of power supply includes：
Power Supply Assembly；
Support；
Drive component, it is fixed on the support, the drive component can receive the control signal, and can be according to described
Control signal works；
Tumbler, it is rotatably installed on the support, and is connected with the drive component, so that the driving
Component can drive the tumbler to rotate；
Fixed pulley assembly, it is rotatably installed on the support；
Movable pulley component, can relatively described bracket slide；
Cable, one end are used to bypass the fixed pulley assembly, the dynamic cunning successively with the unmanned mechatronics, the other end
Electrically connected after wheel assembly and the tumbler with the Power Supply Assembly, wherein, the tumbler rotates and makes the cable winds
On the tumbler, or the cable is discharged from the tumbler, while the cable is pulled the movable pulley
Component slides towards first direction；
Pull force calculation component, it is fixedly connected with the movable pulley component, the pull force calculation component can produce one towards
The elastic pulling force in two directions, the second direction is opposite to the first direction, so that the pull force calculation component can detect institute
Value of thrust of the cable to the movable pulley component is stated, and the value of thrust can be fed back to the control by the pull force calculation component
End；Wherein, the control terminal sends the control signal according to the control instruction and the value of thrust.
In one of the embodiments, the drive component includes motor and consolidated with the output shaft of the motor
Surely the gear connected, the motor can receive the control signal, and can drive the gear according to the control signal
Rotate, the tumbler is meshed with the gear, so that the gear can drive the tumbler to rotate.
In one of the embodiments, the tumbler includes：
Shaft-like connecting portion, rotationally it is arranged in the support；
First round plate, regularly it is sheathed on the shaft-like connecting portion, edge and the tooth of first round plate
Wheel is meshed；
Second round plate, regularly it is sheathed on the shaft-like connecting portion, and and interval relative with first round plate
Set.
In one of the embodiments, the support includes two intervals and the first supporting plate being oppositely arranged and second
Fagging, the shaft-like connecting portion are rotationally arranged in first supporting plate and second supporting plate, the shaft-like connection
Portion is the hollow stem of both ends open, and the via being connected with the shaft-like connecting portion is offered on the shaft-like connecting portion, described
Via is on one section of shaft-like connecting portion between first round plate and second round plate, first disk
Portion is located at the shaft-like connecting portion and passed on one end of first supporting plate, and the cable is close to one end of the Power Supply Assembly
Opening after through the via from the shaft-like connecting portion close to one end of first round plate passes.
In one of the embodiments, the movable pulley component includes guide rail, sliding block, fixed mount and movable pulley, described to lead
Rail extends along the first direction, the slide block set on the guide rail, and along the guide rail bearing of trend slidably, institute
State fixed mount to be fixed on the sliding block, the movable pulley is rotatably fixed on the fixed mount, and the cable is away from institute
State unmanned plane one end bypass the fixed pulley assembly, the movable pulley and the tumbler after be electrically connected with the Power Supply Assembly
Connect.
In one of the embodiments, one section of line between the fixed pulley assembly and the movable pulley component
Cable is parallel with one section of cable between the movable pulley component and the tumbler.
In one of the embodiments, the drive component is electrically connected with the pull force calculation component with the Power Supply Assembly
Connect.
In one of the embodiments, the pull force calculation component includes signal feedback device and fed back with the signal to fill
The tensiometer being fixedly connected is put, the tensiometer is fixedly connected with the movable pulley component, and the tensiometer gives the movable pulley
Component provides an elastic pulling force towards the second direction, so that the tensiometer can detect the cable to the movable pulley
The value of thrust of component, and the value of thrust can be transferred to the signal feedback device, the signal feedback device can be by described in
Value of thrust feeds back to control terminal.
In one of the embodiments, the Power Supply Assembly includes shell, generator and rectifier, is installed on the shell
There are power interface and current output interface, the generator is regularly contained in the shell, the rectifier and the hair
Motor, the power interface, the current output interface electrically connect, and the cable electrically connects with the current output interface.
In one of the embodiments, the Power Supply Assembly also includes rechargeable battery, and the rechargeable battery regularly houses
In in the shell, and electrically connected with the rectifier, the current output interface.
The drive component of the electric power supply control system of above-mentioned unmanned plane can drive according to the control signal that control terminal is sent
Tumbler rotates, one end of cable be used for unmanned mechatronics, the other end successively around fixed pulley assembly, movable pulley component and
Electrically connected after tumbler with Power Supply Assembly, tumbler rotates and makes cable winds on tumbler, or makes cable from tumbler
Upper release, while make cable pull movable pulley component to be slided towards first direction, and pull force calculation component can produce one towards the
The elastic pulling force in two directions, second direction is with first direction on the contrary, so that pull force calculation component can detect cable to movable pulley
The value of thrust of component, and value of thrust can be transferred to control terminal by pull force calculation component, and control terminal need to according to control instruction and
Two parameters of value of thrust judge whether to send control signal to control whether drive component works, so as to control turning for tumbler
Dynamic, controlling cable is that line is wound on tumbler, i.e. take-up, or is discharged from tumbler, i.e. unwrapping wire, and is only filled when signal feeds back
Value of thrust increase or reduction that the movable pulley component that feedback detects is subject to are put, when the control instruction of no control unmanned plane during flying
When, control terminal would not send control signal to drive component, not only realize the folding and unfolding of intelligent control cable, additionally it is possible to effectively
Ground avoids unwrapping wire excessive or take-up the problem of caused cable winds knot not in time, more safe.
Brief description of the drawings
Fig. 1 is the electric power supply control system of unmanned plane and circuit, the signal connection figure of unmanned plane of an embodiment；
Fig. 2 is that the administration of power supply of the electric power supply control system of the unmanned plane shown in Fig. 1 is connected with the structural representation of unmanned plane；
Fig. 3 is that the Power Supply Assembly of the electric power supply control system of the unmanned plane shown in Fig. 1 eliminates the structural representation of part enclosure
Figure；
Fig. 4 is that the electric power supply control system of the unmanned plane shown in Fig. 1 does not connect the structural representation of unmanned plane.
Embodiment
For the ease of understanding the present invention, the present invention is described more fully below with reference to relevant drawings.In accompanying drawing
Give the preferred embodiment of the present invention.But the present invention can realize in many different forms, however it is not limited to herein
Described embodiment.On the contrary, the purpose for providing these embodiments is to make the understanding to the disclosure more saturating
It is thorough comprehensive.
It should be noted that when element is referred to as " being fixed on " another element, it can be directly on another element
Or there may also be element placed in the middle.When an element is considered as " connection " another element, it can be directly connected to
To another element or it may be simultaneously present centering elements.Term as used herein " vertical ", " horizontal ", " left side ",
" right side " and similar statement are for illustrative purposes only.
Unless otherwise defined, all of technologies and scientific terms used here by the article is with belonging to technical field of the invention
The implication that technical staff is generally understood that is identical.Term used in the description of the invention herein is intended merely to description tool
The purpose of the embodiment of body, it is not intended that in the limitation present invention.
As shown in figure 1, the electric power supply control system 10 of the unmanned plane of an embodiment, can power to unmanned plane 20, and it is controllable
The state of flight of unmanned plane 20 processed.The electric power supply control system 10 of the unmanned plane includes control terminal 100 and administration of power supply 200.
Control terminal 100 is the control device of unmanned plane 20 and administration of power supply 200.Wherein, control terminal 100 can produce control nothing
The control instruction of man-machine 20 state of flight, and control terminal 100 can also send the control letter of the work of control administration of power supply 200
Number.
Also referring to Fig. 2, administration of power supply 200 can power to unmanned plane 20.Wherein, administration of power supply 200 includes power supply group
Part 210, support 220, drive component 230, tumbler 240, fixed pulley assembly 250, movable pulley component 260, cable 270 and pulling force
Detection components 280.
Also referring to Fig. 3, Power Supply Assembly 210 includes shell 212, generator 213, rectifier 214 and rechargeable battery
215。
Shell 212 is generally rectangular shaped housing.Wherein, power interface and current output interface 216 are installed on shell 212.
Power interface can electrically connect with external power supply.External power supply for example can be civil power.
Generator 213 is regularly contained in shell 212.Specifically, generator 213 is ac generator.
Rectifier 214 is regularly contained in shell 212, and with generator 213, power interface, current output interface 216
Electrically connect, so that Power Supply Assembly 210 can be powered by external power supply, directly can also be powered by generator 213.
Rechargeable battery 215 electrically connects with rectifier 214, current output interface 216.Wherein, rechargeable battery 215 and rectification
The electrical connection of device 214 is to be able to charge to rechargeable battery 215；Rechargeable battery 215 electrically connected with current output interface 216 be for
Powered when extraneous power supply is not powered and alternating current generator 213 does not also work.
It is appreciated that in other embodiments, rechargeable battery 215 can omit；Or generator 213 and electricity are only set
One in source interface.
Also referring to Fig. 4, support 220 is drive component 230, fixed pulley assembly 250, movable pulley component 260 and rotated
The support member of part 240.In use, support 220 is placed on work ground.Specifically, support 220 includes the first supporting plate
222 and the second supporting plate 224 for being spaced and be oppositely arranged with the first supporting plate 222, the first supporting plate 222 and the second supporting plate
224 one end can be fixed on work ground.
Drive component 230 is fixed on support 220, and drive component 230 can receive control signal, and can be according to control signal
Work.Wherein, drive component 230 can be powered by external power supply, directly can also be powered by Power Supply Assembly 210.Specifically,
Drive component 230 includes motor 232 and gear 234.
Motor 232 can receive control signal, and can be rotated according to control signal band moving gear 234.Specifically illustrating
Embodiment in, motor 232 is between the first supporting plate 222 and the second supporting plate 224, and motor 232 is defeated
Shaft is rotationally arranged in the first supporting plate 222.Wherein, motor 232 can be powered by external power supply, can also be direct
Powered by Power Supply Assembly 210.
Gear 234 is fixedly connected with the output shaft of motor 232, so that motor 232 can be 234 turns with moving gear
It is dynamic.Specifically, the output shaft that gear 234 is sheathed on motor 232 is passed on one end of the first supporting plate 222.
Tumbler 240 is rotatably installed on support 220, and is connected with drive component 230, so that drive component
230 can drive tumbler 240 to rotate.Specifically, tumbler 240 is rotatably installed on the first supporting plate 222 and the second support
On plate 224.Specifically in the illustrated embodiment, tumbler 240 is meshed with gear 234, and motor 232 is passed through gear
234 can drive tumbler 240 to rotate.
Further, tumbler 240 includes shaft-like connecting portion 244, the first round plate 246 and the second round plate 248.
Shaft-like connecting portion 244 is rotationally arranged in the first supporting plate 222 and the second supporting plate 224 of support 220.Specifically
, shaft-like connecting portion 244 is the hollow stem of both ends open, offers what is communicated with shaft-like connecting portion 244 on shaft-like connecting portion 244
Via (not shown).
First round plate 246 is regularly sheathed on shaft-like connecting portion 244, edge and the gear 234 of the first round plate 246
It is meshed.Passed specifically, the first round plate 246 is located at shaft-like connecting portion 244 on one end of the first supporting plate 222.
Second round plate 248 is regularly sheathed on shaft-like connecting portion 244, and relatively and is spaced with the first round plate 246
Set.Wherein, on one section of shaft-like connecting portion 244 of the via between the first round plate 246 and the second round plate 248.Specifically
, the one end of shaft-like connecting portion 244 away from the first round plate 246 passes through the first supporting plate 222 after passing the second round plate 248,
So that the second round plate 248 is between the first supporting plate 222 and the second supporting plate 224.
Fixed pulley assembly 250 is rotatably installed on support 220.Specifically, fixed pulley assembly 250 is rotatably mounted
In in the second supporting plate 224.Wherein, fixed pulley assembly 250 includes locating rack 252 and fixed pulley 254, and locating rack 252 is fixed on
In second supporting plate 224, fixed pulley 254 is rotatably installed on locating rack 252.
Movable pulley component 260 can opposite brackets 220 slide.Specifically, movable pulley component 260 includes guide rail 262, sliding block
264th, fixture 266 and movable pulley 268.
Guide rail 262 extends in a first direction.Specifically, the substantially bar shaped of guide rail 262 is shaft-like.
Sliding block 264 is sheathed on guide rail 262, and along guide rail 262 bearing of trend slidably.
Fixture 266 is fixed on sliding block 264, so that sliding block 264 can drive fixture 266 to slide.
Movable pulley 268 is rotatably fixed on fixture 266.
One end of cable 270 is used to electrically connect with unmanned plane 20, and the other end bypasses the fixed pulley of fixed pulley assembly 250 successively
254th, the current output interface 216 after the movable pulley 268 and tumbler 240 of movable pulley component 260 with Power Supply Assembly 210 is electrically connected
Connect.Wherein, tumbler 240 rotates and cable 270 is wrapped on tumbler 240, or makes cable 270 from tumbler 240
Release, meanwhile, make cable 270 pull movable pulley component 260 to be slided towards first direction.Specifically, cable 270 can be wrapped in it is shaft-like
On connecting portion 244, and the cable 270 being wrapped on shaft-like connecting portion 244 is located at the first round plate 246 and the second round plate 248
Between.Wherein, cable 270 close to one end of Power Supply Assembly 210 pass through via after from shaft-like connecting portion 244 close to the first round plate
The opening of 246 one end is passed and electrically connected with the current output interface 216 of Power Supply Assembly 210.
Pull force calculation component 280 is fixedly connected with movable pulley component 260, and pull force calculation component 280 can produce a court
The pulling force of second direction, second direction is with first direction on the contrary, so that pull force calculation component 280 can detect cable 270 and be slided to dynamic
The value of thrust of wheel assembly 260, and pull force calculation component 280 can feed back to value of thrust control terminal 100.Wherein, pull force calculation group
Part 280 can be powered by external power supply, directly can also be powered by Power Supply Assembly 210.Specifically, pull force calculation component 280
It is fixedly connected with the fixture 266 of movable pulley component 260.
Further, one section of cable 270 between fixed pulley assembly 250 and movable pulley component 260 (is denoted as line segment
AB it is) parallel with one section of cable 270 (being denoted as line segment CD) between movable pulley component 260 and tumbler 240, so that two
The pulling force born on section cable 270 is equal, so that the pulling force that pull force calculation component 280 detects is exactly suffered by cable 270
Twice of pulling force.The pulling force detected according to pull force calculation component 280 can calculate the pulling force on cable 270.
Specifically in the present embodiment, pull force calculation component 280 includes signal feedback device 282 and tensiometer 284.
Signal feedback device 282 is fixed on work-yard.Wherein, signal feedback device 282 passes through nothing with control terminal 100
Line signal connects.Wherein, signal feedback device 282 can be powered by external power supply, directly can also be supplied by Power Supply Assembly 210
Electricity.
Tensiometer 284 is fixedly connected with signal feedback device 282, the fixture of tensiometer 284 and movable pulley component 260
266 are fixedly connected, and tensiometer 284 provides an elastic pulling force towards second direction to wheel assembly 260 is slided, so that tensiometer
284 can detect value of thrust of the cables 270 to movable pulley component 260, and value of thrust can be transferred to signal feedback device 282, believe
Number feedback device 282 can feed back to value of thrust control terminal 100.
Wherein, control terminal 100 sends control signal according to control instruction and value of thrust.The control that i.e. control terminal 100 is sent
The shadow for the value of thrust that signal is fed back by the control instruction and signal feedback device 282 of the state of flight for controlling unmanned plane 20 simultaneously
Ring.For example, when control terminal 100 sends control unmanned plane 20 control instruction that rises or advance, and signal feedback device 282 is anti-
During the value of thrust increase that the movable pulley component 260 that the tensiometer 284 of feedback detects is subject to, control terminal 100 just issues drive component
230 motor 232 rotates so that the control signal that cable 270 discharges from tumbler 240 (i.e. unwrapping wire)；Work as control terminal
100 send the control instruction that control unmanned plane 20 declines or retreated, and the tensiometer 284 that signal feedback device 282 feeds back detects
To the value of thrust that is subject to of movable pulley component 260 reduce when, control terminal 100 just issues 232 turns of the motor of drive component 230
Move so that cable 270 is wrapped in the control signal of tumbler 240 (i.e. take-up)；And only when the drawing that signal feedback device 282 feeds back
The value of thrust increase or reduce that the movable pulley component 260 that power meter 284 detects is subject to, without the control for controlling unmanned plane 20 to fly
During system instruction, control terminal 100 would not send control signal to the motor 232 of drive component 230.
The electric power supply control system 10 of above-mentioned unmanned plane at least has the advantage that：
The drive component 230 of the electric power supply control system 10 of above-mentioned unmanned plane can according to the control signal that control terminal is sent come
Tumbler 240 is driven to rotate, one end of cable 270 is used to electrically connect with unmanned plane 20, and the other end bypasses fixed pulley assembly successively
250th, electrically connected after movable pulley component 260 and tumbler 240 with Power Supply Assembly 210, tumbler 240 rotates and twines cable 270
It is wound on tumbler 240, or cable 270 is discharged from tumbler 240, while cable 270 is pulled movable pulley component
260 slide towards first direction, and pull force calculation component 280 can produce an elastic pulling force towards second direction, second direction
With first direction on the contrary, so that pull force calculation component 280 can detect value of thrust of the cable 270 to movable pulley component 260, and drawing
Value of thrust can be transferred to control terminal 100 by power detection components 280, and control terminal 100 need to be according to control instruction and value of thrust two
Individual parameter judges whether to send control signal to control whether drive component 230 works, so as to control turning for tumbler 240
Dynamic, controlling cable 270 is wound around on tumbler 240, i.e. take-up, still makes the one end of cable 270 away from tumbler 240 towards remote
Direction from tumbler 240 is moved, i.e. unwrapping wire, and only when signal feedback device 282 feed back the movable pulley component 260 detected by
Arrive value of thrust increase or reduce, without control unmanned plane 20 fly control instruction when, control terminal 100 would not give driving
Component 230 sends control signal, not only realizes the folding and unfolding of intelligent control cable 270, additionally it is possible to it is excessive to be effectively prevented from unwrapping wire
Or take-up not in time caused 270 tangled up and knotted of cable the problem of, it is more safe.
Each technical characteristic of embodiment described above can be combined arbitrarily, to make description succinct, not to above-mentioned reality
Apply all possible combination of each technical characteristic in example to be all described, as long as however, the combination of these technical characteristics is not deposited
In contradiction, the scope that this specification is recorded all is considered to be.
Embodiment described above only expresses the several embodiments of the present invention, and its description is more specific and detailed, but simultaneously
Can not therefore it be construed as limiting the scope of the patent.It should be pointed out that come for one of ordinary skill in the art
Say, without departing from the inventive concept of the premise, various modifications and improvements can be made, these belong to the protection of the present invention
Scope.Therefore, the protection domain of patent of the present invention should be determined by the appended claims.
Claims (10)
1. a kind of electric power supply control system of unmanned plane, can be powered to unmanned plane, and the state of flight of the unmanned plane is can control, its
It is characterised by, the electric power supply control system of the unmanned plane includes control terminal and administration of power supply, and the control terminal can produce control institute
The control instruction of the state of flight of unmanned plane is stated, and the control terminal can also send the control for the work for controlling the administration of power supply
Signal, the administration of power supply can give the unmanned plane to power, and the administration of power supply includes：
Power Supply Assembly；
Support；
Drive component, it is fixed on the support, the drive component can receive the control signal, and can be according to the control
Signal works；
Tumbler, it is rotatably installed on the support, and is connected with the drive component, so that the drive component
The tumbler can be driven to rotate；
Fixed pulley assembly, it is rotatably installed on the support；
Movable pulley component, can relatively described bracket slide；
Cable, one end are used to bypass the fixed pulley assembly, the running block successively with the unmanned mechatronics, the other end
Electrically connected after part and the tumbler with the Power Supply Assembly, wherein, the tumbler rotates and makes the cable winds in institute
State on tumbler, or the cable is discharged from the tumbler, while the cable is pulled the movable pulley component
Slided towards first direction；
Pull force calculation component, it is fixedly connected with the movable pulley component, the pull force calculation component can produce one towards second party
To elastic pulling force, the second direction is opposite to the first direction, so that the pull force calculation component can detect the line
Cable is to the value of thrust of the movable pulley component, and the value of thrust can be fed back to the control terminal by the pull force calculation component；
Wherein, the control terminal sends the control signal according to the control instruction and the value of thrust.
2. the electric power supply control system of unmanned plane according to claim 1, it is characterised in that the drive component includes driving
Motor and the gear being fixedly connected with the output shaft of the motor, the motor can receive the control signal, and
The pinion rotation can be driven according to the control signal, the tumbler is meshed with the gear, so that the gear can
The tumbler is driven to rotate.
3. the electric power supply control system of unmanned plane according to claim 2, it is characterised in that the tumbler includes：
Shaft-like connecting portion, rotationally it is arranged in the support；
First round plate, regularly it is sheathed on the shaft-like connecting portion, the edge of first round plate and the gear phase
Engagement；
Second round plate, regularly it is sheathed on the shaft-like connecting portion, and and interval setting relative with first round plate.
4. the electric power supply control system of unmanned plane according to claim 3, it is characterised in that the support includes two intervals
And the first supporting plate and the second supporting plate being oppositely arranged, the shaft-like connecting portion are rotationally arranged in first supporting plate
With second supporting plate, the shaft-like connecting portion is the hollow stem of both ends open, is offered on the shaft-like connecting portion and institute
State the via that shaft-like connecting portion is connected, one section between first round plate and second round plate of the via
On the shaft-like connecting portion, first round plate is located at the shaft-like connecting portion and passed on one end of first supporting plate,
The cable close to one end of the Power Supply Assembly pass through the via after from the shaft-like connecting portion close to first disk
The opening of the one end in portion passes.
5. the electric power supply control system of unmanned plane according to claim 1, it is characterised in that the movable pulley component includes leading
Rail, sliding block, fixed mount and movable pulley, the guide rail extend along the first direction, and the slide block set is located on the guide rail, and
Along the guide rail bearing of trend slidably, the fixed mount is fixed on the sliding block, and the movable pulley is rotatably fixed
In on the fixed mount, the one end of the cable away from the unmanned plane bypasses the fixed pulley assembly, the movable pulley and institute
Electrically connected after stating tumbler with the Power Supply Assembly.
6. the electric power supply control system of unmanned plane according to claim 1, it is characterised in that positioned at the fixed pulley assembly and
One section of cable between the movable pulley component and one section of institute between the movable pulley component and the tumbler
It is parallel to state cable.
7. the electric power supply control system of unmanned plane according to claim 1, it is characterised in that the drive component and the drawing
Power detection components electrically connect with the Power Supply Assembly.
8. the electric power supply control system of unmanned plane according to claim 1, it is characterised in that the pull force calculation component includes
Signal feedback device and the tensiometer being fixedly connected with the signal feedback device, the tensiometer are consolidated with the movable pulley component
Fixed connection, the tensiometer provides an elastic pulling force towards the second direction to the slip wheel assembly, so that the drawing
Power meter can detect value of thrust of the cable to the movable pulley component, and the value of thrust can be transferred to the signal feedback
The value of thrust can be fed back to control terminal by device, the signal feedback device.
9. the electric power supply control system of unmanned plane according to claim 1, it is characterised in that the Power Supply Assembly includes outer
Shell, generator and rectifier, power interface and current output interface are installed on the shell, the generator regularly houses
In in the shell, the rectifier electrically connects with the generator, the power interface, the current output interface, institute
Cable is stated to electrically connect with the current output interface.
10. the electric power supply control system of unmanned plane according to claim 9, it is characterised in that the Power Supply Assembly also includes
Rechargeable battery, the rechargeable battery are regularly contained in the shell, and equal with the rectifier, the current output interface
Electrical connection.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201610695150.8A CN107757942A (en) | 2016-08-19 | 2016-08-19 | The electric power supply control system of unmanned plane |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610695150.8A CN107757942A (en) | 2016-08-19 | 2016-08-19 | The electric power supply control system of unmanned plane |
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| CN107757942A true CN107757942A (en) | 2018-03-06 |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN109383800A (en) * | 2018-09-30 | 2019-02-26 | 江苏师范大学 | A kind of accurate dispenser of express delivery take-away |
| CN110254740A (en) * | 2019-05-08 | 2019-09-20 | 广州中国科学院先进技术研究所 | A kind of electric capstan device for multi-functional unmanned plane |
| WO2021126071A1 (en) * | 2019-12-18 | 2021-06-24 | Avetics Global Pte. Ltd. | A tether management system and method |
| CN113753255A (en) * | 2021-08-25 | 2021-12-07 | 洛阳北方企业集团有限公司 | Novel ground mooring flying device of gyroplane |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104743129A (en) * | 2015-03-12 | 2015-07-01 | 西南科技大学 | Automatic lock line winding and unwinding device for mooring unmanned aerial vehicle |
| CN105173105A (en) * | 2015-08-04 | 2015-12-23 | 徐州创航科技有限公司 | Automatic cable coiling and uncoiling device used for mooring unmanned plane aircraft |
| CN105752337A (en) * | 2016-02-26 | 2016-07-13 | 北京计算机技术及应用研究所 | Automatic take-up and payoff control system for mooring unmanned plane |
| CN205931306U (en) * | 2016-08-19 | 2017-02-08 | 深圳航天旭飞科技有限公司 | Unmanned aerial vehicle's power supply control system |
-
2016
- 2016-08-19 CN CN201610695150.8A patent/CN107757942A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104743129A (en) * | 2015-03-12 | 2015-07-01 | 西南科技大学 | Automatic lock line winding and unwinding device for mooring unmanned aerial vehicle |
| CN105173105A (en) * | 2015-08-04 | 2015-12-23 | 徐州创航科技有限公司 | Automatic cable coiling and uncoiling device used for mooring unmanned plane aircraft |
| CN105752337A (en) * | 2016-02-26 | 2016-07-13 | 北京计算机技术及应用研究所 | Automatic take-up and payoff control system for mooring unmanned plane |
| CN205931306U (en) * | 2016-08-19 | 2017-02-08 | 深圳航天旭飞科技有限公司 | Unmanned aerial vehicle's power supply control system |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109383800A (en) * | 2018-09-30 | 2019-02-26 | 江苏师范大学 | A kind of accurate dispenser of express delivery take-away |
| CN110254740A (en) * | 2019-05-08 | 2019-09-20 | 广州中国科学院先进技术研究所 | A kind of electric capstan device for multi-functional unmanned plane |
| WO2021126071A1 (en) * | 2019-12-18 | 2021-06-24 | Avetics Global Pte. Ltd. | A tether management system and method |
| US20220380186A1 (en) * | 2019-12-18 | 2022-12-01 | Avetics Global Pte. Ltd. | Tether management system and method |
| EP4077199A4 (en) * | 2019-12-18 | 2023-09-06 | Avetics Global Pte. Ltd. | A tether management system and method |
| CN113753255A (en) * | 2021-08-25 | 2021-12-07 | 洛阳北方企业集团有限公司 | Novel ground mooring flying device of gyroplane |
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