CN106284110A - Airplane parking area and control system thereof - Google Patents
Airplane parking area and control system thereof Download PDFInfo
- Publication number
- CN106284110A CN106284110A CN201610877179.8A CN201610877179A CN106284110A CN 106284110 A CN106284110 A CN 106284110A CN 201610877179 A CN201610877179 A CN 201610877179A CN 106284110 A CN106284110 A CN 106284110A
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- China
- Prior art keywords
- parking area
- airplane parking
- unmanned plane
- motor
- fixed
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- 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.)
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Classifications
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- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01F—ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
- E01F3/00—Landing stages for helicopters, e.g. located above buildings
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Toys (AREA)
Abstract
The present invention relates to a kind of airplane parking area; including housing; described enclosure interior is fixed with bedplate; ball limiting plate it is fixed with inside described bedplate; it is fixed with ball in described ball limiting plate; described ball limiting plate is provided with landing plate; described ball limiting plate bottom is fixed with traction apparatus; described casing peripheral is provided with several holes; a push rod is fixed each via elastic device in described hole; described push rod can be slided in described hole, and described traction apparatus draws described landing plate and described push rod by pull rope.The control system of airplane parking area of the present invention; including controller; several pressure transducers being arranged on landing plate and be connected with described controller communication; inside described controller, the unmanned plane to arbitrary model is respectively provided with control motor number, motor rotating cycle, complete machine weight and head towards parameter; described controller is electrically connected with motor, for controlling the rotation of described motor.
Description
Technical field
The present invention relates to a kind of unmanned plane stop device, particularly to a kind of airplane parking area and control system thereof.
Background technology
At present, the airplane parking area on market, effect is only used for parking unmanned plane, it is impossible to the position that modulation unmanned plane is stopped
Put.
Summary of the invention
It is an object of the invention to provide a kind of airplane parking area, after unmanned plane drops on landing plate, no matter it is positioned at airplane parking area
On what position, by motor, the second pull rope is discharged so that the elastic device of elastic shrinkage discharges, elastic device
Elastic force drives four push rods to promote to centre position so that landing plate slides on ball, is parked in the unmanned plane on landing plate
It is pushed to centre position, airplane parking area, after unmanned plane flies away, by spring and the traction of the first pull rope so that landing plate is multiple
Position.
It is a further object of the present invention to provide the control system of a kind of airplane parking area, by the unmanned plane of different model is set
Different control motor number, motor rotating cycle (varying in size according to unmanned plane, control long putt), complete machine weight and machines
Head is towards parameter, after unmanned plane landing, when the force value sum of all pressure transducers detection is more than the certain value of complete machine weight,
Controller controls motor so that push rod promotes to unmanned plane direction, and unmanned plane is pushed to centre position, airplane parking area.
One airplane parking area of the present invention, parks and is pushed into by unmanned plane center, airplane parking area for unmanned plane, including housing, described
Enclosure interior is fixed with bedplate, is fixed with ball limiting plate inside described bedplate, fixing in described ball limiting plate
Being provided with ball, described ball limiting plate is provided with landing plate, and described ball limiting plate bottom is fixed with traction apparatus, described shell
Body periphery is provided with several holes, fixes a push rod each via elastic device in described hole so that described push rod can be described
Sliding in hole, described traction apparatus draws described landing plate and described push rod by pull rope.
Further, described traction apparatus includes the motor being fixed on described ball limiting plate bottom, described bedplate week
While be provided with four the first fixed pulleys, described motor end is provided with four first pull ropes, and described first pull rope is fixed by first
Pulley is connected to four angles of landing plate, and described motor end is additionally provided with four second pull ropes, and described second pull rope passes through
Four push rods of described hole traction.
Further, described push rod is provided with the second fixed pulley, described second pull rope pressure away from described casing center one end
On described second fixed pulley, guide and reduce the pull strength of described second pull rope for described second pull rope.
Further, described first pull rope and described second pull rope are spaced from each other, two-by-two in 45 degree of angles.
Further, described elastic device is spring.
Further, described hole is square hole, and described push rod is T-bar.
Further, fixing on the housing by spring bottom described landing plate.
A kind of control system of above-mentioned airplane parking area, including controller, be arranged at landing plate on and with described controller communication
Several pressure transducers connected, inside described controller unmanned plane to arbitrary model be respectively provided with control motor number,
Motor rotating cycle, complete machine weight and head are towards parameter, and described controller is electrically connected with motor, is used for controlling described motor
Rotation.
Further, when the unmanned plane of a certain model is to be landed, the selected one group of control arranged well in the controller
Motor number processed, motor rotating cycle, complete machine weight and head are towards parameter, when described unmanned plane drops to described airplane parking area
After, described controller detects the force value of each pressure transducer, when the force value sum of each pressure transducer is more than described complete machine
During the certain value of weight, controller judges that unmanned plane drops in airplane parking area adjustable extent, and then, controller is mutual with unmanned plane
Communication, it is determined that whether unmanned plane shuts down, head towards and poised state, when unmanned plane shut down, head is towards accurately and for balance
During state, described controller controls electric machine rotation, drives pushrod movement, discharges the second pull rope, makes landing plate sliding on ball
Dynamic, when push rod arrives precalculated position, detect the force value of each pressure transducer, when the force value of each pressure transducer is in setting
In the range of, it is determined that unmanned plane playbacks.
Further, when push rod arrives precalculated position, the force value of each pressure transducer is detected, when each pressure transducer
Force value is not in the range of setting, and controller controls motor reversal, restPoses, the most again push rod is pushed into pre-determined bit
Put.
Compared with prior art, beneficial effects of the present invention:
1) the airplane parking area structure of the present invention, after unmanned plane drops on landing plate, what position being positioned on airplane parking area regardless of it
Putting, discharged by the second pull rope by motor so that the elastic device of elastic shrinkage discharges, the elastic force of elastic device drives
Four push rods promote to centre position so that landing plate slides on ball, and the unmanned plane being parked on landing plate is pushed to stop
Centre position, machine level ground, after unmanned plane flies away, by spring and the traction of the first pull rope so that landing sheet reset；
2) control system of the present invention, by setting different control motor number, motor to the unmanned plane of different model
Rotating cycle (varying in size according to unmanned plane, control long putt), complete machine weight and head land towards parameter, unmanned plane
After, when the force value sum of all pressure transducers detection is more than the certain value of complete machine weight, controller controls motor so that push away
Bar promotes to unmanned plane direction, and unmanned plane is pushed to centre position, airplane parking area.
Accompanying drawing explanation
For the technical scheme being illustrated more clearly that in the embodiment of the present invention, below by use required in embodiment
Accompanying drawing is briefly described, it should be apparent that, the accompanying drawing in describing below is some embodiments of the present invention, for this area
From the point of view of those of ordinary skill, on the premise of not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings.
Fig. 1 is airplane parking area of the present invention detonation configuration schematic diagram.
Fig. 2 is airplane parking area of the present invention control system flow chart.
Detailed description of the invention
In order to make the purpose of the present invention, technical scheme and advantage clearer, below in conjunction with drawings and Examples, right
The present invention is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the present invention, not
For limiting the present invention.
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 known as " being connected to " another element, and it can
To be directly to another element or to may be simultaneously present centering elements.
Also, it should be noted the orientation term such as left and right, upper and lower in the embodiment of the present invention, it it is only relative concept each other
Or with the normal operating condition of product as reference, and should not be regarded as restrictive.
The embodiment of the present invention one, as it is shown in figure 1, a kind of airplane parking area, parks for unmanned plane and unmanned plane is pushed into shutdown
Center, level ground, including housing 7, the internal bedplate 9 that is fixed with of described housing 7, it is spacing that described bedplate 9 inside is fixed with ball
Plate 6, is fixed with ball 5 in described ball limiting plate 6, described ball limiting plate 6 is provided with landing plate 3, and described ball is spacing
Plate 6 lower middle position is fixed with motor 2, and described housing 7 periphery is provided with four holes 71, each via elasticity in described hole 71
Device (mark) fixes a push rod 1 so that described push rod 1 can slide in described hole 71.
Ball 5 is arranged in ball limiting plate 6, does not comes off, and can roll in ball limiting plate 6.Landing plate 3 can be
Slide on ball 5.
Described bedplate 9 periphery is provided with four the first fixed pulleys 91, and described motor 2 end is provided with four first pull ropes 8,
Described first pull rope 8 is connected to four angles of landing plate 3 by the first fixed pulley 91.First pull rope 8 is for bedplate 9
Reset.
The reset mode of another kind of bedplate 9, is fixed on described housing 7 by spring 4 by bottom described landing plate 3,
Elastic force by spring 4, it is possible to so that bedplate 9 resets.
The reset mode of both the above bedplate 9 can be used in conjunction with, it is also possible to is used alone.
Described motor 2 end is additionally provided with four second pull ropes (mark), and described second pull rope is led by described hole
Draw four push rods；Described push rod 1 is provided with the second fixed pulley 11 away from one end, described housing 7 center, and described second pull rope is pressed on
On described second fixed pulley 11, guide and reduce the pull strength of described second pull rope for described second pull rope (owing to sliding
Friction becomes rolling friction, and frictional force is little, and therefore required pull strength is little).
Described first pull rope and described second pull rope are spaced from each other, two-by-two in 45 degree of angles.
Described elastic device is spring.
Described hole is square hole, and described push rod is T-bar.
The motor of the present invention, can be a motor, it is also possible to be several motors.Such as the first pull rope and the second traction
Rope is controlled by two different motors respectively.
In four second pull ropes of four push rods 1 of traction, two relative second pull ropes are by a motor control
System, another two relative second pull ropes of group are controlled by another motor, can control the promotion order of four push rods 1, with
The working effect making push rod 1 is more preferable.
A kind of control system of above-mentioned airplane parking area, including controller, be arranged at landing plate on and with described controller communication
Several pressure transducers connected, inside described controller unmanned plane to arbitrary model be respectively provided with control motor number,
Motor rotating cycle, complete machine weight and head are towards parameter, and described controller is electrically connected with motor, is used for controlling described motor
Rotation.
As in figure 2 it is shown, when the unmanned plane of a certain model is to be landed, the selected one group of control arranged well in the controller
Motor number processed, motor rotating cycle, complete machine weight and head are towards parameter, when described unmanned plane drops to described airplane parking area
After, described controller detects the force value of each pressure transducer, when the force value sum of each pressure transducer is more than described complete machine
During the certain value of weight, controller judges that unmanned plane drops in airplane parking area adjustable extent, and then, controller is mutual with unmanned plane
Communication, it is determined that whether unmanned plane shuts down, head towards and poised state, when unmanned plane shut down, head is towards accurately and for balance
During state, described controller controls electric machine rotation, drives pushrod movement, discharges the second pull rope, makes landing plate sliding on ball
Dynamic, when push rod arrives precalculated position, detect the force value of each pressure transducer, when the force value of each pressure transducer is in setting
In the range of, it is determined that unmanned plane playbacks.
After described unmanned plane drops to described airplane parking area, described controller detects the force value of each pressure transducer, and
Whether each force value of detection equalizes and (sets each range of pressure values in control system, when force value is not in setting value further
In the range of time, it is determined that for unbalanced), when force value is unbalanced, revise parameter, control driven by motor pushrod movement the most again.
When by multiple driven by motor push rod, when push rod arrives precalculated position, detect the force value of each pressure transducer, when
The force value of each pressure transducer is not in the range of setting, and controller controls motor reversal, restPoses, and will the most again
Push rod promotes order to be pushed into precalculated position by other.
The foregoing is only presently preferred embodiments of the present invention, not in order to limit the present invention, all essences in the present invention
Any amendment, equivalent or the improvement etc. made within god and principle, should be included within the scope of the present invention.
Claims (10)
1. an airplane parking area, parks for unmanned plane and unmanned plane is pushed into center, airplane parking area, it is characterised in that including housing,
Described enclosure interior is fixed with bedplate, is fixed with ball limiting plate, in described ball limiting plate inside described bedplate
Being fixed with ball, described ball limiting plate is provided with landing plate, and described ball limiting plate bottom is fixed with traction apparatus, institute
State casing peripheral and be provided with several holes, in described hole, fix a push rod each via elastic device so that described push rod can be
Sliding in described hole, described traction apparatus draws described landing plate and described push rod by pull rope.
Airplane parking area the most according to claim 1, it is characterised in that it is spacing that described traction apparatus includes being fixed on described ball
The motor of plate bottom, described bedplate periphery is provided with four the first fixed pulleys, and described motor end is provided with four first pull ropes,
Described first pull rope is connected to four angles of landing plate by the first fixed pulley, and described motor end is additionally provided with four second and leads
Messenger, described second pull rope draws four push rods by described hole.
Airplane parking area the most according to claim 2, it is characterised in that described push rod is provided with away from described casing center one end
Two fixed pulleys, described second pull rope is pressed on described second fixed pulley, guides for described second pull rope and reduces described
The pull strength of two pull ropes.
Airplane parking area the most according to claim 2, it is characterised in that described first pull rope and described second pull rope are mutual
Spaced apart, two-by-two in 45 degree of angles.
Airplane parking area the most according to claim 1, it is characterised in that described elastic device is spring.
Airplane parking area the most according to claim 1, it is characterised in that described hole is square hole, described push rod is T-bar.
Airplane parking area the most according to claim 1, it is characterised in that be fixed on described shell by spring bottom described landing plate
On body.
8. the control system according to airplane parking area described in any one of claim 1 to 7, it is characterised in that include controller, if
Several pressure transducers being placed on landing plate and be connected with described controller communication, to arbitrary model inside described controller
Unmanned plane be respectively provided with control motor number, motor rotating cycle, complete machine weight and head towards parameter, described controller with
Motor is electrically connected with, for controlling the rotation of described motor.
The control system of airplane parking area the most according to claim 8, it is characterised in that when the unmanned plane of a certain model to land
Time, selected good arranged one group of control motor number, motor rotating cycle, complete machine weight and head in the controller towards
Parameter, after described unmanned plane drops to described airplane parking area, described controller detects the force value of each pressure transducer, when each pressure
When the force value sum of force transducer is more than the certain value of described complete machine weight, controller judgement unmanned plane drops to airplane parking area can
In the range of tune, then, controller and the mutual communication of unmanned plane, it is determined that whether unmanned plane shuts down, head towards and poised state, when
Unmanned plane is shut down, head towards accurately and when be poised state, described controller controls electric machine rotation, drive pushrod movement, releases
Put the second pull rope, make landing plate slide on ball, when push rod arrives precalculated position, detect the pressure of each pressure transducer
Value, when the force value of each pressure transducer is in the range of setting, it is determined that unmanned plane playbacks.
The control system of airplane parking area the most according to claim 9, it is characterised in that when push rod arrives precalculated position, and detection is each
The force value of pressure transducer, when the force value of each pressure transducer is not in the range of setting, controller controls motor reversal,
RestPose, the most again push rod is pushed into precalculated position.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610877179.8A CN106284110B (en) | 2016-09-30 | 2016-09-30 | Airplane parking area and its control system and control method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610877179.8A CN106284110B (en) | 2016-09-30 | 2016-09-30 | Airplane parking area and its control system and control method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106284110A true CN106284110A (en) | 2017-01-04 |
| CN106284110B CN106284110B (en) | 2018-10-26 |
Family
ID=57717620
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610877179.8A Active CN106284110B (en) | 2016-09-30 | 2016-09-30 | Airplane parking area and its control system and control method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106284110B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108316166A (en) * | 2017-01-16 | 2018-07-24 | 广东博达机场建设实业有限公司 | A kind of electric rotary type helideck |
| CN108657456A (en) * | 2018-06-27 | 2018-10-16 | 深圳市多翼创新科技有限公司 | Rackwork |
| CN108674685A (en) * | 2018-05-18 | 2018-10-19 | 云南电网有限责任公司电力科学研究院 | A kind of shaft tower apron |
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| JP2001073322A (en) * | 1999-09-08 | 2001-03-21 | Shin Meiwa Ind Co Ltd | Uninhabited mid-to-high-rise building equipped with separate installation-type heliport |
| CN203845022U (en) * | 2014-04-28 | 2014-09-24 | 赵子滨 | Automation platform for providing service for routing inspection unmanned plane |
| CN205295974U (en) * | 2016-01-13 | 2016-06-08 | 徐海涛 | Unmanned aerial vehicle intelligence air park |
| US9387940B2 (en) * | 2010-11-09 | 2016-07-12 | Colorado Seminary Which Owns And Operates The University Of Denver | Intelligent self-leveling docking system |
| CN206220000U (en) * | 2016-09-30 | 2017-06-06 | 深圳市天域智能有限公司 | Airplane parking area |
-
2016
- 2016-09-30 CN CN201610877179.8A patent/CN106284110B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2001073322A (en) * | 1999-09-08 | 2001-03-21 | Shin Meiwa Ind Co Ltd | Uninhabited mid-to-high-rise building equipped with separate installation-type heliport |
| US9387940B2 (en) * | 2010-11-09 | 2016-07-12 | Colorado Seminary Which Owns And Operates The University Of Denver | Intelligent self-leveling docking system |
| CN203845022U (en) * | 2014-04-28 | 2014-09-24 | 赵子滨 | Automation platform for providing service for routing inspection unmanned plane |
| CN205295974U (en) * | 2016-01-13 | 2016-06-08 | 徐海涛 | Unmanned aerial vehicle intelligence air park |
| CN206220000U (en) * | 2016-09-30 | 2017-06-06 | 深圳市天域智能有限公司 | Airplane parking area |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108316166A (en) * | 2017-01-16 | 2018-07-24 | 广东博达机场建设实业有限公司 | A kind of electric rotary type helideck |
| CN108674685A (en) * | 2018-05-18 | 2018-10-19 | 云南电网有限责任公司电力科学研究院 | A kind of shaft tower apron |
| CN108657456A (en) * | 2018-06-27 | 2018-10-16 | 深圳市多翼创新科技有限公司 | Rackwork |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106284110B (en) | 2018-10-26 |
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