CN208553102U - A kind of amusement facility and Ferris Wheel and flying tower by double closed-loop control system holding cockpit level - Google Patents
A kind of amusement facility and Ferris Wheel and flying tower by double closed-loop control system holding cockpit level Download PDFInfo
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- CN208553102U CN208553102U CN201820872684.8U CN201820872684U CN208553102U CN 208553102 U CN208553102 U CN 208553102U CN 201820872684 U CN201820872684 U CN 201820872684U CN 208553102 U CN208553102 U CN 208553102U
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Abstract
The utility model relates to a kind of amusement facilities that cockpit level is kept by double closed-loop control system, and the cockpit of its opposite movement is provided on bracket, and driving cockpit is provided between bracket and cockpit relative to the mobile benchmark motor of bracket and adjustment motor；The amusement facility further includes the double closed-loop control system for controlling cockpit relative to ground holding level, the double closed-loop control system respectively detects the driving speed of benchmark motor and adjustment motor by velocity measuring encoder A and velocity measuring encoder B, the driving speed of real-time monitoring adjustment motor, keep it identical as the driving speed holding of benchmark motor, constitute speed closed loop, it realizes that speed sync follows, reduces level correction caused by speed accumulation error；In addition, controller carries out horizontal detection to cockpit by the analog quantity inclination angle detection sensor of three Redundancy Designs, and cockpit is moved carry out PID adjusting according to testing result, constitute horizontal closed-loop control, realizes level correction.
Description
[technical field]
The invention is related to a kind of amusement facility, especially a kind of to keep cockpit level by double closed-loop control system
Amusement facility.
[background technique]
In industry of travelling, the amusement facilities such as Ferris Wheel and flying tower with the development of economy, in more and more places
It comes into operation.And with the improvement of people's life quality, the comfortableness and security to cockpit also have higher requirement, cockpit
Therefore it is also required to be updated the replacement.
Traditional sightseeing cabin, majority only rely on cockpit self gravity and passenger's gravity using the adaptive technology of gravity
To keep cockpit holding horizontal.This technology without other power due to participating in, if unbalance loading situation occurs in cabin interior passenger, cockpit is just
100% level is not can guarantee, and external force resistance jamming performance is weak.
In order to preferably keep cockpit level, also there is the technology for increasing linear motor to cockpit, provide drive for cockpit rotation
Power, to overcome the unbalance loading of cockpit and the influence of External force interference.But the control system of cockpit rotation in the prior art is using horizontal
Closed-loop control carries out level correction, which belongs to Speed open-loop control mode, the actual speed of cockpit and skyscraping ring by
In influenced by unbalance loading situation and motor slip ratio and can not precise synchronization, there are driving speed is poor, resulting accumulation is missed
Difference can cause cockpit to tilt, and make the frequent operation control of the horizontal closed-loop control system of cockpit, and Yi Yinqi overshoot concussion influences to take body
It tests.
In addition, traditional flying tower cockpit generally uses at least two promotion power sources, since there are cockpit unbalance loading or electricity
Machine revolutional slip etc. influences, and the promotion speed between multiple promotion power sources is made not can guarantee the mistake for unanimously causing cockpit in promotion
It is easy to appear unhorizontal situation in journey, therefore designs a unbalance loading and motor slip ratio of capable of actively eliminating to actual speed
Influence, guarantee that cockpit relative to the amusement facility of ground holding level is the invention urgent problem to be solved.
[summary of the invention]
To solve the above problems, the invention, which provides one kind, controls cockpit movement by double closed-loop control system, it can
The influence of unbalance loading and motor slip ratio to actual speed is actively eliminated, guarantees that cockpit is set relative to horizontal the travelling of ground holding
It applies.
To achieve the above object, the invention provides the following technical solutions:
A kind of amusement facility keeping cockpit level by double closed-loop control system, including bracket are arranged on the bracket
There is the cockpit of its opposite movement, driving cockpit first driving mechanism mobile relative to bracket is provided between the bracket and cockpit
With the second driving mechanism, first driving mechanism includes the benchmark electricity for giving driving speed relative to support motion as cockpit
Machine, second driving mechanism include the adjustment motor that identical driving speed is kept with the benchmark motor；The amusement facility is also
Horizontal double closed-loop control system is kept relative to ground including controlling the cockpit, the double closed-loop control system includes:
Velocity measuring encoder A, for detecting the driving speed of the benchmark motor；
Velocity measuring encoder B, for detecting the driving speed of the adjustment motor；
Benchmark motor driver, for driving the work of the benchmark motor；
Motor driver is adjusted, for driving the work of the adjustment motor；
Controller, for receiving the signal of the velocity measuring encoder A and velocity measuring encoder B, the speed
The detection speed of encoder A is detected as reference speed, the detection speed of the velocity measuring encoder B whether with benchmark
Speed is identical, and when different, the controller drives the adjustment motor acceleration-deceleration to carry out by the adjustment motor driver
Adjustment keeps the driving speed of the adjustment motor identical as the driving speed holding of benchmark motor；
Inclination angle detection sensor for detecting the inclination angle between cockpit and ground, and transfers data to controller, when inclining
When angle exceeds preset value, the controller drives the adjustment motor acceleration-deceleration to be adjusted by the adjustment motor driver
It is whole, make the cockpit relative to ground holding level.
Preferably, it is further defined in that the inclination angle detection sensor at least provided with three, is adopted respectively
With the analog quantity inclination angle detection sensor of different manufacturers.
A kind of Ferris Wheel keeping cockpit level by double closed-loop control system, including bracket are provided on the bracket
The skyscraping ring to rotate to it, around the cockpit outer ring that several synchronous rotations are distributed with, the cockpit on the skyscraping ring
It is provided with the cockpit of its opposite movement in outer ring, driving skyscraping ring is provided between the bracket and skyscraping ring and is turned relative to bracket
It is anti-relative to skyscraping ring same angular velocity to be provided with driving cockpit for the first dynamic driving mechanism between the cockpit outer ring and cockpit
To the second driving mechanism of rotation, first driving mechanism includes giving driving speed relative to holder pivots as skyscraping ring
Benchmark motor, second driving mechanism includes the adjustment motor that identical driving speed is kept with the benchmark motor；This rubs
Its ring further includes the double closed-loop control system for controlling the cockpit relative to ground holding level, the double closed-loop control system packet
It includes:
Velocity measuring encoder A, for detecting the velocity of rotation of the benchmark motor；
Velocity measuring encoder B, for detecting the velocity of rotation of the adjustment motor；
Benchmark motor driver, for driving the work of the benchmark motor；
Motor driver is adjusted, for driving the work of the adjustment motor；
Master controller, for controlling the work of the benchmark motor driver and receiving the velocity measuring encoder A's
Signal, and the revolving speed for feeding back information to the benchmark motor driver to guarantee the skyscraping ring is consistent with setting speed, it will
The speed of the velocity measuring encoder A detection is as reference speed；
Cockpit Control Unit, for controlling the work of the adjustment motor driver and receiving the velocity measuring encoder B
Signal, whether the detection speed of the velocity measuring encoder B identical as reference speed, when different, the controller
It drives the adjustment motor acceleration-deceleration to be adjusted by the adjustment motor driver, makes the driving speed of the adjustment motor
It spends identical as the driving speed holding of benchmark motor；
Inclination angle detection sensor for detecting the inclination angle between cockpit and ground, and transfers data to controller, when inclining
When angle exceeds preset value, the controller drives the adjustment motor acceleration-deceleration to be adjusted by the adjustment motor driver
It is whole, make the cockpit relative to ground holding level.
Preferably, it is further defined in that the velocity measuring encoder A is arranged on the skyscraping ring,
The velocity measuring encoder B and the distribution of inclination angle detection sensor are arranged on the cockpit.
Preferably, it is further defined in that the inclination angle detection sensor at least provided with three, is adopted respectively
With the analog quantity inclination angle detection sensor of different manufacturers.
A kind of flying tower keeping cockpit level by double closed-loop control system, including bracket are provided on the bracket
The cockpit of its opposite elevating movement is provided with the first drive of the opposite bracket lifting moving of driving cockpit between the bracket and cockpit
Motivation structure and the second driving mechanism, first driving mechanism include giving lifting speed relative to support motion as cockpit
Benchmark motor, second driving mechanism include the adjustment motor that identical lifting speed is kept with the benchmark motor；The flight
Tower further includes the double closed-loop control system for controlling the cockpit relative to ground holding level, the double closed-loop control system packet
It includes:
Velocity measuring encoder A, for detecting the lifting speed of the benchmark motor；
Velocity measuring encoder B, for detecting the lifting speed of the adjustment motor；
Benchmark motor driver, for driving the work of the benchmark motor；
Motor driver is adjusted, for driving the work of the adjustment motor；
Controller, for receiving the signal of the velocity measuring encoder A and velocity measuring encoder B, the speed
The detection speed of encoder A is detected as reference speed, the detection speed of the velocity measuring encoder B whether with benchmark
Speed is identical, and when different, the controller drives the adjustment motor acceleration-deceleration to carry out by the adjustment motor driver
Adjustment keeps the driving speed of the adjustment motor identical as the driving speed holding of benchmark motor；
Inclination angle detection sensor for detecting the inclination angle between cockpit and ground, and transfers data to controller, when inclining
When angle exceeds preset value, the controller drives the adjustment motor acceleration-deceleration to be adjusted by the adjustment motor driver
It is whole, make the cockpit relative to ground holding level.
Preferably, it is further defined in that the inclination angle detection sensor at least provided with three, is adopted respectively
With the analog quantity inclination angle detection sensor of different manufacturers.
The beneficial effect of the invention is: the cockpit of its opposite movement, cockpit are provided on the bracket of the invention
Keep horizontal relative to ground by double closed-loop control system, which passes through velocity measuring encoder A and speed
Degree detection encoder B respectively detects the driving speed of benchmark motor and adjustment motor, and real-time monitoring adjusts the drive of motor
Dynamic speed, keeps it identical as the driving speed holding of benchmark motor, constitutes speed closed loop, realizes that speed sync follows, reduces speed
Spend level correction caused by accumulated error；
In addition, controller carries out horizontal detection to cockpit by the analog quantity inclination angle detection sensor of three Redundancy Designs,
And cockpit is moved carry out PID adjusting according to testing result, horizontal closed-loop control is constituted, realizes level correction.Horizontal closed loop and
The double closed-loop control system that speed closed loop collective effect is constituted, is able to maintain cockpit speed sync, horizontal stable.
[Detailed description of the invention]
Fig. 1 is the structural schematic diagram of Ferris Wheel；
Fig. 2 is the structural schematic diagram of cockpit in Fig. 1；
Fig. 3 is the functional-block diagram of the double closed-loop control system of Ferris Wheel；
Fig. 4 is the structural schematic diagram of flying tower；
Fig. 5 is the functional-block diagram of the double closed-loop control system of flying tower.
[specific embodiment]
The invention is described in further detail below in conjunction with the drawings and specific embodiments:
A kind of amusement facility keeping cockpit level by double closed-loop control system, including bracket 1 are set on the bracket 1
It is equipped with the cockpit 3 of its opposite movement, driving cockpit 3 is provided between the bracket 1 and cockpit 3 relative to the first of the movement of bracket 1
Driving mechanism and the second driving mechanism, first driving mechanism include moving given driving speed relative to bracket 1 as cockpit 3
The benchmark motor of degree, second driving mechanism include the adjustment motor that identical driving speed is kept with the benchmark motor；It should
Amusement facility further includes the double closed-loop control system for controlling the cockpit 3 relative to ground holding level, the double-closed-loop control
System includes:
Velocity measuring encoder A, for detecting the driving speed of the benchmark motor；
Velocity measuring encoder B, for detecting the driving speed of the adjustment motor；
Benchmark motor driver, for driving the work of the benchmark motor；
Motor driver is adjusted, for driving the work of the adjustment motor；
Controller, for receiving the signal of the velocity measuring encoder A and velocity measuring encoder B, the speed
The detection speed of encoder A is detected as reference speed, the detection speed of the velocity measuring encoder B whether with benchmark
Speed is identical, and when different, the controller drives the adjustment motor acceleration-deceleration to carry out by the adjustment motor driver
Adjustment keeps the driving speed of the adjustment motor identical as the driving speed holding of benchmark motor；Speed closed loop is constituted, is adjusted in real time
The driving speed of the whole motor of control realizes that speed sync follows, reduces level correction caused by speed accumulation error；
Inclination angle detection sensor for detecting the inclination angle between cockpit 3 and ground, and transfers data to controller, when
When inclination angle exceeds preset value, if inclination angle is more than 1 °, the controller drives the adjustment electricity by the adjustment motor driver
Machine acceleration-deceleration is adjusted, and constitutes horizontal closed-loop control, makes the cockpit 3 relative to ground holding level.
Furthermore, the inclination angle detection sensor is at least provided with three, in the present embodiment, the inclination angle inspection
There are three survey sensor is arranged altogether, including inclination angle detection sensors A, inclination angle detection sensor B and inclination angle detection sensor C, point
Not Cai Yong different manufacturers analog quantity inclination angle detection sensor, can prevent because use same model sensor, lead to multiple biographies
Sensor effectively improves the stability of the control system because same problem breaks down simultaneously.Controller is sensed according to inclination angle detection
The testing result of device carries out PID adjusting to the movement of cockpit 3, realizes level correction.In the present embodiment, the benchmark motor and
Adjusting motor can be using linear motor in the prior art or alternating current generator etc., and the controller can be used in the prior art
PLC or single-chip microcontroller, the benchmark motor driver and adjustment motor driver use servo-driver in the prior art, described
Transmission data are carried out by Industrial Ethernet between controller and benchmark motor driver, controller and adjustment motor driver
Exchange.
As shown in attached drawing 1, attached drawing 2, attached drawing 3, a kind of Ferris Wheel keeping cockpit level by double closed-loop control system, packet
Include bracket 1, be provided with the skyscraping ring 2 to rotate to it on the bracket 1, on the skyscraping ring 2 around be distributed with it is several and its
The cockpit outer ring 4 of synchronous rotation, band moving-base cockpit outer ring 4 is along 2 axis rotation of skyscraping ring, the cockpit outer ring when skyscraping ring 2 revolves
It is provided with the cockpit 3 of its opposite movement in 4, driving skyscraping ring 2 is provided between the bracket 1 and skyscraping ring 2 relative to bracket 1
It is identical relative to skyscraping ring 2 to be provided with driving cockpit 3 for first driving mechanism of rotation between the cockpit outer ring 4 and cockpit 3
Counter-rotational second driving mechanism of angular speed, first driving mechanism include rotating as skyscraping ring 2 relative to bracket 1
The benchmark motor of given driving speed, second driving mechanism includes the tune that identical driving speed is kept with the benchmark motor
Whole motor；The skyscraping ring further includes the double closed-loop control system for controlling the cockpit 3 relative to ground holding level, by double
Closed-loop control system can guarantee that cockpit 3 is rotated backward with skyscraping ring 2 with same angular velocity, actively eliminate load and motor slip
Influence of the rate to actual speed, to keep horizontal control process more stable.
Furthermore, the double closed-loop control system includes:
Velocity measuring encoder A, for detecting the velocity of rotation of the benchmark motor；
Velocity measuring encoder B, for detecting the velocity of rotation of the adjustment motor；
Benchmark motor driver, for driving the work of the benchmark motor；
Motor driver is adjusted, for driving the work of the adjustment motor；
Master controller, for controlling the work of the benchmark motor driver and receiving the velocity measuring encoder A's
Signal, and the revolving speed for feeding back information to the benchmark motor driver to guarantee the skyscraping ring 2 is consistent with setting speed, it will
The speed of the velocity measuring encoder A detection is as reference speed；
Cockpit Control Unit, for controlling the work of the adjustment motor driver and receiving the velocity measuring encoder B
Signal, whether the detection speed of the velocity measuring encoder B identical as reference speed, when different, the controller
It drives the adjustment motor acceleration-deceleration to be adjusted by the adjustment motor driver, makes the driving speed of the adjustment motor
It spends identical as the driving speed holding of benchmark motor；
Inclination angle detection sensor for detecting the inclination angle between cockpit 3 and ground, and transfers data to controller, when
When inclination angle exceeds preset value, if inclination angle is more than 1 °, the controller drives the adjustment electricity by the adjustment motor driver
Machine acceleration-deceleration is adjusted, and makes the cockpit 3 relative to ground holding level.
Due to the revolving speed of the output revolving speed not necessarily lam-oil skyscraping ring of skyscraping ring driving mechanism, in order to more accurately to skyscraping
The revolving speed of ring is detected, and the outermost of skyscraping ring 2, relatively close cockpit 3, detection is arranged in the velocity measuring encoder A
Revolving speed it is more accurate.The velocity measuring encoder B and the distribution of inclination angle detection sensor are arranged on the cockpit 3.The sight
Vehicle of looking at further includes Ferris Wheel master control system, and the Ferris Wheel master control system includes being electrically connected with the benchmark motor driver
Main controller, transmission data are carried out by Industrial Ethernet between the main controller and controller and are exchanged.Furthermore,
Ethernet switch is electrically connected with wireless access point, and realization controller is same with Ferris Wheel master control system wireless network communication
When, it is also convenient for entering access or regulatory process using wireless device users.
The Ferris Wheel is by the horizontal level inclination for detecting Real-time Feedback driving motor, and controller is according to inclination angle size to drive
The revolving speed of dynamic motor is adjusted, and to achieve the purpose that inclination angle reduces, realizes passive horizontal control effect；By to car speed
Real-time detection feedback, controller is adjusted the revolving speed of driving motor, reaches speed sync according to the size of speed difference
Purpose；Due to speed sync, reduce the generation of system inclination angle difference, to realize actively horizontal control effect.
As shown in attached drawing 4, attached drawing 5, a kind of flying tower keeping cockpit level by double closed-loop control system, including bracket
1, it is provided with the cockpit 3 of its opposite elevating movement on the bracket 1, driving cockpit 3 is provided between the bracket 1 and cockpit 3
The first driving mechanism and the second driving mechanism of opposite 1 lifting moving of bracket, first driving mechanism include being used as cockpit 3
The benchmark motor of given lifting speed is moved relative to bracket 1, second driving mechanism includes keeping with the benchmark motor
The adjustment motor of identical lifting speed；The flying tower further includes the two close cycles for controlling the cockpit 3 relative to ground holding level
Control system, the double closed-loop control system include:
Velocity measuring encoder A, for detecting the lifting speed of the benchmark motor；
Velocity measuring encoder B, for detecting the lifting speed of the adjustment motor；
Benchmark motor driver, for driving the work of the benchmark motor；
Motor driver is adjusted, for driving the work of the adjustment motor；
Controller, for receiving the signal of the velocity measuring encoder A and velocity measuring encoder B, the speed
The detection speed of encoder A is detected as reference speed, the detection speed of the velocity measuring encoder B whether with benchmark
Speed is identical, and when different, the controller drives the adjustment motor acceleration-deceleration to carry out by the adjustment motor driver
Adjustment keeps the driving speed of the adjustment motor identical as the driving speed holding of benchmark motor；
Inclination angle detection sensor for detecting the inclination angle between cockpit 3 and ground, and transfers data to controller, when
When inclination angle exceeds preset value, if inclination angle is more than 1 °, the controller drives the adjustment electricity by the adjustment motor driver
Machine acceleration-deceleration is adjusted, and makes the cockpit 3 relative to ground holding level.
In the present embodiment, the motors such as hoist engine in the prior art can be used in benchmark motor and adjustment motor, pass through steel
Cord component band moving-base cockpit is gone up and down.Velocity measuring encoder A can be correspondingly arranged at benchmark motor by steel wire rope component with
The junction that cockpit 3 connects, velocity measuring encoder B can be correspondingly arranged at adjustment motor and be connected by steel wire rope component and cockpit 3
It realizes that speed sync follows by detecting the lifting speed of 3 different location of cockpit, reduces speed accumulation error in the junction connect
Caused level correction.
Claims (7)
1. a kind of amusement facility for keeping cockpit level by double closed-loop control system, including bracket (1), on the bracket (1)
It is provided with the cockpit (3) of its opposite movement, driving cockpit (3) is provided between the bracket (1) and cockpit (3) with respect to bracket
(1) mobile the first driving mechanism and the second driving mechanism, first driving mechanism include as cockpit (3) relative to bracket
(1) the benchmark motor of given driving speed is moved, second driving mechanism includes driving identical as the benchmark motor holding
The adjustment motor of speed；It is characterized in that it further includes controlling the cockpit (3) to keep horizontal two close cycles control relative to ground
System processed, the double closed-loop control system include:
Velocity measuring encoder A, for detecting the driving speed of the benchmark motor；
Velocity measuring encoder B, for detecting the driving speed of the adjustment motor；
Benchmark motor driver, for driving the work of the benchmark motor；
Motor driver is adjusted, for driving the work of the adjustment motor；
Controller, for receiving the signal of the velocity measuring encoder A and velocity measuring encoder B, the velocity measuring
The detection speed of encoder A as reference speed, the detection speed of the velocity measuring encoder B whether with reference speed
Identical, when different, the controller drives the adjustment motor acceleration-deceleration to be adjusted by the adjustment motor driver,
Keep the driving speed of the adjustment motor identical as the driving speed holding of benchmark motor；
Inclination angle detection sensor for detecting the inclination angle between cockpit (3) and ground, and transfers data to controller, when inclining
When angle exceeds preset value, the controller drives the adjustment motor acceleration-deceleration to be adjusted by the adjustment motor driver
It is whole, so that the cockpit (3) is kept horizontal relative to ground.
2. the amusement facility according to claim 1 for keeping cockpit level by double closed-loop control system, it is characterised in that
The analog quantity inclination angle detection sensor of different manufacturers is respectively adopted at least provided with three in the inclination angle detection sensor.
3. a kind of Ferris Wheel for keeping cockpit level by double closed-loop control system, including bracket (1) is set on the bracket (1)
It is equipped with the skyscraping ring (2) to rotate to it, surround the cockpit outer ring that several synchronous rotations are distributed on the skyscraping ring (2)
(4), it is provided with the cockpit (3) of its opposite movement in the cockpit outer ring (4), is arranged between the bracket (1) and skyscraping ring (2)
The first driving mechanism for having driving skyscraping ring (2) to rotate relative to bracket (1), sets between the cockpit outer ring (4) and cockpit (3)
Driving cockpit (3) is equipped with relative to counter-rotational second driving mechanism of skyscraping ring (2) same angular velocity, first driving machine
Structure includes the benchmark motor for rotating given driving speed relative to bracket (1) as skyscraping ring (2), the second driving mechanism packet
Include the adjustment motor that identical driving speed is kept with the benchmark motor；It is characterized in that it further includes controlling the cockpit (3)
Horizontal double closed-loop control system is kept relative to ground, the double closed-loop control system includes:
Velocity measuring encoder A, for detecting the velocity of rotation of the benchmark motor；
Velocity measuring encoder B, for detecting the velocity of rotation of the adjustment motor；
Benchmark motor driver, for driving the work of the benchmark motor；
Motor driver is adjusted, for driving the work of the adjustment motor；
Master controller, for controlling the work of the benchmark motor driver and receiving the signal of the velocity measuring encoder A,
And the revolving speed for feeding back information to the benchmark motor driver to guarantee the skyscraping ring (2) is consistent with setting speed, by institute
The speed of velocity measuring encoder A detection is stated as reference speed；
Cockpit Control Unit, for controlling the work of the adjustment motor driver and receiving the letter of the velocity measuring encoder B
Number, whether the detection speed of the velocity measuring encoder B is identical as reference speed, and when different, the controller passes through
The adjustment motor driver drives the adjustment motor acceleration-deceleration to be adjusted, make the adjustment motor driving speed and
The driving speed of benchmark motor keeps identical；
Inclination angle detection sensor for detecting the inclination angle between cockpit (3) and ground, and transfers data to controller, when inclining
When angle exceeds preset value, the controller drives the adjustment motor acceleration-deceleration to be adjusted by the adjustment motor driver
It is whole, so that the cockpit (3) is kept horizontal relative to ground.
4. the Ferris Wheel according to claim 3 for keeping cockpit level by double closed-loop control system, it is characterised in that institute
It states velocity measuring encoder A to be arranged on the skyscraping ring (2), the velocity measuring encoder B and inclination angle detection sensor point
Cloth is arranged on the cockpit (3).
5. the Ferris Wheel according to claim 3 for keeping cockpit level by double closed-loop control system, it is characterised in that institute
Inclination angle detection sensor is stated at least provided with three, the analog quantity inclination angle detection sensor of different manufacturers is respectively adopted.
6. a kind of flying tower for keeping cockpit level by double closed-loop control system, including bracket (1) is set on the bracket (1)
It is equipped with the cockpit (3) of its opposite elevating movement, driving cockpit (3) is provided between the bracket (1) and cockpit (3) with respect to bracket
(1) the first driving mechanism and the second driving mechanism of lifting moving, first driving mechanism include as cockpit (3) relative to
Bracket (1) moves the benchmark motor of given lifting speed, and second driving mechanism includes identical as the benchmark motor holding
The adjustment motor of lifting speed；It is characterized in that it further includes controlling the cockpit (3) to close relative to the double of ground holding level
Ring control system, the double closed-loop control system include:
Velocity measuring encoder A, for detecting the lifting speed of the benchmark motor；
Velocity measuring encoder B, for detecting the lifting speed of the adjustment motor；
Benchmark motor driver, for driving the work of the benchmark motor；
Motor driver is adjusted, for driving the work of the adjustment motor；
Controller, for receiving the signal of the velocity measuring encoder A and velocity measuring encoder B, the velocity measuring
The detection speed of encoder A as reference speed, the detection speed of the velocity measuring encoder B whether with reference speed
Identical, when different, the controller drives the adjustment motor acceleration-deceleration to be adjusted by the adjustment motor driver,
Keep the driving speed of the adjustment motor identical as the driving speed holding of benchmark motor；
Inclination angle detection sensor for detecting the inclination angle between cockpit (3) and ground, and transfers data to controller, when inclining
When angle exceeds preset value, the controller drives the adjustment motor acceleration-deceleration to be adjusted by the adjustment motor driver
It is whole, so that the cockpit (3) is kept horizontal relative to ground.
7. the flying tower according to claim 6 for keeping cockpit level by double closed-loop control system, it is characterised in that institute
Inclination angle detection sensor is stated at least provided with three, the analog quantity inclination angle detection sensor of different manufacturers is respectively adopted.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820872684.8U CN208553102U (en) | 2018-06-06 | 2018-06-06 | A kind of amusement facility and Ferris Wheel and flying tower by double closed-loop control system holding cockpit level |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820872684.8U CN208553102U (en) | 2018-06-06 | 2018-06-06 | A kind of amusement facility and Ferris Wheel and flying tower by double closed-loop control system holding cockpit level |
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| Publication Number | Publication Date |
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| CN208553102U true CN208553102U (en) | 2019-03-01 |
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| CN201820872684.8U Active CN208553102U (en) | 2018-06-06 | 2018-06-06 | A kind of amusement facility and Ferris Wheel and flying tower by double closed-loop control system holding cockpit level |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108635865A (en) * | 2018-06-06 | 2018-10-12 | 中山市金马科技娱乐设备股份有限公司 | A kind of amusement facility keeping cockpit level by double closed-loop control system |
| CN113244634A (en) * | 2021-06-28 | 2021-08-13 | 浙江南方文旅科技股份有限公司 | Novel control system of flying kiss recreation facility |
-
2018
- 2018-06-06 CN CN201820872684.8U patent/CN208553102U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108635865A (en) * | 2018-06-06 | 2018-10-12 | 中山市金马科技娱乐设备股份有限公司 | A kind of amusement facility keeping cockpit level by double closed-loop control system |
| CN113244634A (en) * | 2021-06-28 | 2021-08-13 | 浙江南方文旅科技股份有限公司 | Novel control system of flying kiss recreation facility |
| CN113244634B (en) * | 2021-06-28 | 2024-05-07 | 浙江南方文旅科技股份有限公司 | Novel control system of flying kiss recreation facility |
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