CN106178553B - Circle in the air the cockpit swing mechanism of movie theatre - Google Patents
Circle in the air the cockpit swing mechanism of movie theatre Download PDFInfo
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- CN106178553B CN106178553B CN201610792881.4A CN201610792881A CN106178553B CN 106178553 B CN106178553 B CN 106178553B CN 201610792881 A CN201610792881 A CN 201610792881A CN 106178553 B CN106178553 B CN 106178553B
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- cockpit
- backboard
- electric cylinders
- hanger
- bearing
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- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63J—DEVICES FOR THEATRES, CIRCUSES, OR THE LIKE; CONJURING APPLIANCES OR THE LIKE
- A63J25/00—Equipment specially adapted for cinemas
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- Holders For Apparel And Elements Relating To Apparel (AREA)
Abstract
The present invention provides a kind of cockpit swing mechanism for the movie theatre that circles in the air, including backboard, the second rotation axis, third rotation axis, the first electric cylinders and the second electric cylinders；Backboard is flexibly connected by the second shaft with cockpit hanger, and cockpit is flexibly connected by third shaft with backboard；Wherein, the second shaft is set in parallel with backboard, and third shaft is vertical setting with backboard；The outer sleeve of first electric cylinders is arranged on the first bearing, and the outer sleeve of the first electric cylinders is flexibly connected with the first bearing, and the first bearing is fixed on backboard, and the external part of the first electric cylinders is flexibly connected with cockpit；Second electric cylinders are arranged on the second bearing, and the second electric cylinders are flexibly connected with the second bearing, and the second bearing is fixed on cockpit hanger, and the external part of the second electric cylinders is flexibly connected with backboard.Cockpit can be carried out on cockpit hanger it is front and rear rotate and left-right rotation, allow spectators while fully impression extremely powerful ball curtain movie and television contents, can also undergo the excitement that vacantly flies by.
Description
Technical field
The invention belongs to movie theatre technical fields of circling in the air, and in particular to a kind of cockpit swing mechanism for the movie theatre that circles in the air.
Background technology
The movie theatre that circles in the air is a kind of emerging special efficacy amusement film, and spectators take the lifting seat controlled by big machinery system
To movie theatre center in the air, picture is projected huge hemisphere screen by high-definition digital projector by extraordinary fish eye lens, from
The visibility region of the spectators crown to underfooting is all surrounded completely by grand mute, in the abundant extremely powerful ball curtain of impression
While movie and television contents, can also undergo the excitement that vacantly flies by.In addition to 4D movie theatres, huge curtain vault curtain shadow can be reached
The effect of institute can also add in the telegraphy interactive device such as simulated flight mechanism on this basis, allow spectators' body under the environment of safety
Test circle in the air, interactive recreation and other effects.
The invention of Patent No. CN201420422166.8 provides a kind of seat that circles in the air of flight movie theatre, the seat that circles in the air
Chair includes：Fixed frame, balancing stand, adjustable shelf, at least one driving mechanism, several seats；The fixed frame by balancing stand and
Each driving mechanism connects adjustable shelf, and each seat is set on adjustable shelf；The driving mechanism includes drive mechanism body and sets
At least one elastic mechanism being placed in beside the drive mechanism body.The seat that circles in the air of flight movie theatre proposed by the present invention, each
The both sides of electric cylinder respectively with a power-assisted tension spring, can effectively mitigate the power consumption of cylinder, reduce the power configuration of seat；By equipment self-weight
Operation power consumption switch to the lossless load of tension spring, low-energy environment-friendly by the load of actuating unit.The seat that circles in the air employs more
Driving mechanism, complicated, the frequency of failure is high, and manufactures of high cost.
Invention content
The object of the present invention is to provide a kind of cockpit swing mechanisms for the movie theatre that circles in the air, and simple in structure, cockpit is in cockpit hanger
On front and rear can rotate and left-right rotation.
The technical solution adopted by the present invention is：
Circle in the air the cockpit swing mechanism of movie theatre, including backboard, the second rotation axis, third rotation axis, the first electric cylinders and second
Electric cylinders；Backboard is arranged between cockpit and cockpit hanger, and backboard is flexibly connected by the second rotation axis with cockpit hanger, and cockpit leads to
Third rotation axis is crossed to be flexibly connected with backboard；Wherein, the second rotation axis is set in parallel with backboard, and third rotation axis is in backboard
It is vertically arranged；The outer sleeve of first electric cylinders is arranged on the first bearing, and the outer sleeve of the first electric cylinders and the first bearing activity connect
It connects, the first bearing is fixed on backboard, and the external part of the first electric cylinders is flexibly connected with cockpit；Second electric cylinders are arranged on the second bearing
On, and the second electric cylinders are flexibly connected with the second bearing, the second bearing is fixed on cockpit hanger, the external part and the back of the body of the second electric cylinders
Plate is flexibly connected.
Wherein, connecting rod is provided between cockpit hanger and backboard, one end of connecting rod is flexibly connected with backboard, connecting rod
The other end be provided with kidney slot, the first screw is fixed on cockpit hanger, the first screw is located in kidney slot.
Wherein, multiple arcs limiting slot is provided on backboard, the cockpit back side is fixed with multiple second screws, second spiral shell
The corresponding arc-shaped limit slot of nail, and second screw is located in an arc-shaped limit slot.
The beneficial effects of the invention are as follows：
1st, cockpit can carry out front and rear rotation and left-right rotation on cockpit hanger, and spectators is allowed fully to experience great shock
While the ball curtain movie and television contents of power, the excitement that vacantly flies of can also undergoing is by bringing better 4D viewings to experience.
2. cockpit swing mechanism of the present invention is provided with rotary spacing component, by setting multiple arcs on cockpit backboard
Limiting slot, and including embedded screw, position-limiting action is played to the left-right rotation of cockpit, while between cockpit hanger and backboard
Kidney slot is provided in connecting rod, position-limiting action is played to the front and rear rotation of cockpit by embedded fixing screws, prevents from controlling
The rotation angle excessive harm caused by spectators is caused during device failure；In case of off-axis, moreover it is possible to prevent cockpit from falling.
Description of the drawings
Fig. 1 is the structure diagram that movie theatre cockpit system is arranged on steel construction that circles in the air；
Fig. 2 is the A portions enlarged drawing of Fig. 1；
Fig. 3 is the structure diagram of cockpit linear moving apparatus, cockpit hanger and cockpit；
Fig. 4 is the structure diagram of speed reducer, the first motor and hand crank；
Fig. 5 is the B portions enlarged drawing of Fig. 4；
Fig. 6 is that turnover panel and cockpit platform is protected to be arranged on the structure diagram on steel construction；
Fig. 7 is the structure diagram for protecting turnover panel, supporting rack and propulsive mechanism；
Fig. 8 is the structure diagram of pushing mechanism；
Fig. 9 is the structure diagram of cockpit swing mechanism, cockpit hanger and cockpit；
Figure 10 is the structure diagram that backboard is arranged on cockpit hanger；
Figure 11 is cockpit kinetic control system structure diagram.
In figure：1- cockpit hangers, 2- support plates, the first rotation axis of 3-, 4- first gears, 5- speed reducers, 6- racks, 7- prevent
Guard bar, 8- mounting bases, 9- walking support wheels, 10- bearing blocks, 11- cockpits, 12- steel constructions, 13- backboards, the second rotation axis of 14-,
15- third rotation axis, the first electric cylinders of 16-, the second electric cylinders of 17-, the first bearings of 18-, the second bearings of 19-, the first motors of 20-, 21-
Hand crank, 22-1. protection turnover panels, 22-2. supporting racks, 22-3. guide rails, 22-4. transmission shafts, 22-5. idler wheels, 22-6. second
Motor, 22-7. stents, 22-8. second gears, 22-9. third gears, 22-10. connecting shaft holes, 21-1. handles, 21-2. are bent
Handle, 21-3. manual shafts, 21-4. fixed seats, 21-5. casings, 23- cockpit platforms, 25. second power input shafts, 26. grooves,
27. convex block, 28. connecting rods, 29. kidney slots, 30. first screws, 31. arc-shaped limit slots, 32. second screws, 33. safety pressures
Thick stick, 34. movable rods, 35. controllers, 36. scram buttons, 50. main control units, 51. cockpits linear movement control unit, 52.
Protect turnover panel rotation control unit, 53. cockpits revolution rotation control unit, 54. emergency stop control units, the control of 55. movable rods
Unit, 56. contact sensors, 57. solenoid valves, 58. Buffer Units.
Specific embodiment
As shown in Figs. 1-5, a kind of viewing system for the movie theatre that circles in the air, including steel construction 12, cockpit 11, cockpit platform 23, seat
Cabin hanger 1, cockpit linear moving apparatus, cockpit swing mechanism and controller 35；Cockpit hanger 1 is moved by cockpit straight line of the present invention
Dynamic device is flexibly connected with steel construction 12, and cockpit linear moving apparatus is arranged on the top of cockpit hanger 1；Cockpit hanger 1 passes through
Cockpit swing mechanism is connect with cockpit 11, and cockpit swing mechanism can make cockpit 11 carry out front-rear direction rotation on cockpit hanger 1
It is rotated with left and right directions；In addition, 12 middle part of steel construction is equipped with cockpit platform 23, cockpit platform 23 is located at the lower section of cockpit 11, seat
The front end of cabin platform 23 is flexibly connected with protection turnover panel 22-1.
As depicted in figs. 1 and 2, cockpit linear moving apparatus includes 1, two 2 and first rotation axis of support plate of cockpit hanger
3；The top of cockpit hanger 1 is provided with the first rotation axis 3, and the both ends of the first rotation axis 3 are respectively arranged with first gear 4, and first
Rotation axis 3 is mounted on speed reducer 5, and driving device drives the first rotation axis 3 to rotate by speed reducer 5, driving device first
Motor 20 and hand crank 21, speed reducer 5, the first motor 20 and hand crank 21 are fixed on the top of cockpit hanger 1；Two branch
Fagging 2 is located at the both sides of cockpit hanger 1 respectively, and rack 6 is fixed in every support plate 2；First tooth at 3 both ends of the first rotation axis
Wheel 4 engages respectively with the rack 6 in two support plates 2.Also, the both ends of the first rotation axis 3 are mounted on bearing block 10, bearing
Seat 10 is fixed on cockpit hanger 1.
There are four ends for 1 top surface of cockpit hanger, and each end is both provided with fender rod 7 and limiting device；The one of fender rod 7
End is fixed on cockpit hanger 1, and the other end is pressed on rack 6.Limiting device includes a mounting base 8 and two walking support wheels
9, two walking support wheels 9 are in setting up and down in mounting base 8, and support plate 2 is clipped between two walking support wheels 9 up and down；Peace
Dress seat 8 is fixed on cockpit hanger 1.
As shown in figures 1 and 3, cockpit 11 is suspended on the lower section of cockpit hanger 1, and two support plates 2 are fixed on the movie theatre that circles in the air
Steel construction 12 on, cockpit 11 is suspended from aerial.
The operation principle of cockpit linear moving apparatus is：Driving device drives the first rotation axis 3 to rotate by speed reducer 5,
The first gear 4 at the both ends of the first rotation axis 3 also and then rotates, and realizes that first gear 4 moves linearly on rack 6, and afterwards the
One rotation axis 3 and first gear 4 also just drive entire cockpit hanger 1 and cockpit 11 straight line back and forth between two support plates 2
It is mobile.Four end sets, four fender rods 7 in 1 top surface of cockpit hanger, fender rod 7 is pressed on rack 6, in cockpit hanger 1
In moving process, fender rod 7 also and then rotates, and the effect of fender rod 7 is to support entire cockpit hanger 1 and cockpit 11, makes seat
Cabin hanger 1 hangs over uniform force between two support plates, prevents cockpit hanger 1 from play up and down occurring in moving process.It is present
Four ends of 1 top surface of cabin hanger also set up limiting device, and support plate 2 is clipped between two walking support wheels 9 up and down, in cockpit
In 1 moving process of hanger, all walking support wheels 9 also and then rotate, and the effect one of walking support wheel 9 is to play support to make
With another is the track for preventing first gear 4 from deviating from rack 6 in rotation process, and there are one be that can also prevent cockpit
Play up and down occurs in moving process for hanger 1.
In addition, for the limiting for be moved forward and backward position to cockpit linear moving apparatus, controller 35 is avoided to occur
The track of cockpit linear moving apparatus abjection rack 6 causes danger during failure, in the appropriate position at the both ends of two support plates 2
Four Buffer Units 58 are respectively provided with, when cockpit linear moving apparatus is moved to restraining position, Buffer Unit 58 can hinder
Walking support wheel 9 moves on, so as to avoid the rectilinear orbit of the abjection operation of cockpit 11, it is ensured that the safety of viewing personnel.
Simultaneously in this case even if walk support wheel 9 break down, then Buffer Unit 58 can touch walk support wheel 9 behind
Fender rod 7, equally play the role of to cockpit 11 be moved forward and backward position limiting, play dual fail-safe.Buffer Unit 58 can be adopted
With increasing flexible rubber bar or carrying the metal bar of spring below, when support wheel 9 or fender rod 7 are touched, rise
To the effect of buffering, the unexpected emergency stop of cockpit is avoided.
In addition, the driving device of driving the first rotation axis 3 rotation is the first motor 20 and hand crank 21, using electronic and
Manual two ways drives the first rotation axis 3 to rotate, afterwards so that cockpit hanger 1 and cockpit 11 12 straight lines on steel construction move
It is dynamic；When having electricity, the work of the first motor 20 drives the first rotation axis 3 to rotate by speed reducer 5, if had a power failure, the first motor 20 is not
It can start, shake hand crank 21 so that speed reducer 5 drives the first rotation axis 3 to rotate.Specific structure is that speed reducer 5 uses
Worm Wheel System, two end axis of worm screw are stretched out outside cabinet, the two end axis namely the first power input shaft and second moves
Power input shaft 25；First motor 20 is connect with the first power input shaft, and the second power input shaft 25 leaves unused and same with worm screw when flat
Step rotation.As shown in figure 4, hand crank 21 includes handle 21-1, crank 21-2 and manual shaft 21-3；One end of manual shaft 21-3
It is fixedly connected with one end of crank 21-2, the other end of crank 21-2 is fixedly connected with handle 21-1；Handle 21-1 and manual shaft
21-3 is set in parallel, and crank 21-2 is vertical setting with manual shaft 21-3.1 top of cockpit hanger is further fixed on fixed seat 21-
Hole is provided on 4, fixed seat 21-4；Manual shaft 21-3 passes through the hole on fixed seat 21-4, and manual shaft 21-3 matches with interporal lacuna
It closes.As shown in figure 5, setting fluted 26 on the second power input shaft 25 outside speed reducer 5, manual shaft 21-3's is another
End be provided with casing 21-5, the opening of casing 21-5 faces the second power input shaft 25, be provided on casing 21-5 inner walls with
26 matched convex block 27 of groove.
When having electricity, the first motor 20 works, and drives the rotation of the first power input shaft, and the first power input shaft drives deceleration again
The worm screw rotation of machine 5, drives worm gear to realize retarded motion afterwards, and the second power input shaft 25 is idle and is rotated synchronously with worm screw,
Speed reducer 5 drives the first rotation axis 3 to rotate, and the first gear 4 at the both ends of the first rotation axis 3 also and then rotates, and realizes the first tooth
Wheel 4 moves linearly on rack 6, and the first rotation axis 3 and first gear 4 also just drive entire cockpit hanger 1 and cockpit afterwards
11 move linearly back and forth between two support plates 2.If had a power failure, the first motor 20 cannot start, and hold handle 21-1 by hand
Moving axis 21-3 is pushed inward so that casing 21-5 is sleeved on the second power input shaft 25, and convex block 27 is made to be embedded in corresponding groove
In 26, thus hand crank 21 is connected on the second power input shaft 25；After in connection, hand crank 21 is shaken, the
Two power input shafts 25 rotate, and drive the worm screw rotation of speed reducer 5, worm gear are driven to realize retarded motion afterwards, speed reducer 5 drives
First rotation axis 3 rotates, and the first gear 4 at the both ends of the first rotation axis 3 also and then rotates, and realizes first gear 4 on rack 6
Linear movement, the first rotation axis 3 and first gear 4 also just drive entire cockpit hanger 1 and cockpit 11 in two supports afterwards
It moves linearly back and forth between plate 2.By the setting of the dual power input shafts of speed reducer 5, make the rotation of the first rotation axis 3 realize
Even if having a power failure, cockpit hanger 1 and cockpit 11 can be also made by manual actuation in two supports for electronic and manual two kinds of type of drive
It is moved between plate 2.When having electricity, manual shaft 21-3 is not connect with the second power input shaft 25, and casing 21-5 is allowed to be detached from the second power
Input shaft 25.
As shown in fig. 6,12 middle part of steel construction is equipped with cockpit platform 23, cockpit platform 23 is located at the lower section of cockpit 11, cockpit
The front end of platform 23 is flexibly connected with protection turnover panel 22-1.Protection turnover panel 22-1 mainly plays protective action.As shown in fig. 7, protection
The turnover panel 22-1 back sides are provided with pushing mechanism；Supporting rack 22-2 is fixed on steel construction 12, guide rail is fixed on supporting rack 22-2
22-3；Pushing mechanism is flexibly connected with guide rail 22-3, and the pushing mechanism pumps on guide rail 22-3, and drives
The movable end of protection turnover panel 22-1 is spun upside down；Particularly, during promotion the both ends of pushing mechanism along guide rail 22-
3 are moved, and in a state that pushing mechanism does not work, protection turnover panel 22-1 rides over the top of guide rail 22-3, when the machine of promotion
When structure moves upwards, protection turnover panel 22-1 leaves the top of guide rail 22-3, overturns, turns over upwards under the promotion of pushing mechanism
Turn rear protecting turnover panel 22-1 and form angle with cockpit platform 23.Before spectators watch film, protection turnover panel 22-1 is dug forward to perpendicular
Straight position, spectators climb up cockpit platform 23 by the ladder on steel construction 12, are then sitting on the seat of cockpit 11 and prepare viewing
Film has the protection of protection turnover panel 22-1, can prevent away cockpit platform 23 under spectators' pendant on cockpit platform 23；Treat spectators
After all sitting straight on the seat, film broadcasting starts, and protection turnover panel 22-1 turns over, and leans against the top of guide rail 22-3.
As shown in figure 8, pushing mechanism includes stent 22-7, the second motor 22-6, transmission shaft 22-4, is located at transmission shaft 22-4
The idler wheel 22-5 at both ends；Second motor 22-6 fixations are located on stent 22-7, and stent 22-7 is fixed on the protection turnover panel 22-1 back sides
Top, be arranged with second gear 22-8 on the output shaft of the second motor 22-6, transmission shaft 22-4 is threaded through on stent 22-7, and
It is arranged with third gear 22-9, second gear 22-8 on transmission shaft 22-4 to engage with third gear 22-9, idler wheel 22-5 is located at
In guide rail 22-3, and moved back and forth in guide rail 22-3.Stent 22-7 overturns for protection turnover panel 22-1 to be pushed to realize, idler wheel
22-5 is equipped with rough rubber bumps, main effect be when being moved in guide rail 22-3 increase with guide rail 22-3 it
Between frictional force, be not in skidding situation.Within a particular process, the second motor 22-6 at work, starts band
The output shaft of dynamic second motor 22-6 rotates forward, and the output shaft of second motor 22-6 drives second gear 22-8 rotations, because of second
Gear 22-8 is engaged with third gear 22-9, therefore third gear 22-9 can also rotate, and third gear 22-9 is set in biography
On moving axis 22-4, transmission shaft 22-4 rotations are driven, transmission shaft 22-4 drives idler wheel 22-5 to be moved upwards in guide rail 22-3 again, into
And the movable end of protection turnover panel 22-1 is pushed to move upwards, realize being flipped up for protection turnover panel 22-1；As the second motor 22-6
Reversion, idler wheel 22-5 are moved downward on guide rail 22-3, realize the reset of protection turnover panel 22-1.Further for transmission shaft
Minimum friction forces between 22-4 and stent 22-7, in transmission shaft 22-4 and stent 22-7 by being set on transmission shaft 22-4
Bearing connection.In addition, the angle between guide rail 22-3 and supporting rack 22-2 is 30 ° to 45 °, and then protect turnover panel 22-1 and seat
The acute angle of the initial angle of 23 front end of cabin platform is 30 ° to 45 °, and preferred angle is 40 °, and protection turnover panel 22-1 can in this way turned over
Thrust used is smaller when turning, and reduces the output power of the second motor 22-6.
As shown in Figure 9 and Figure 10, cockpit swing mechanism provided by the invention includes backboard 13, the second rotation axis 14, third
Rotation axis 15, the first electric cylinders 16 and the second electric cylinders 17；Backboard 13 is arranged between cockpit 11 and cockpit hanger 1, and backboard 13 passes through
Second rotation axis 14 is flexibly connected with cockpit hanger 1, and cockpit 11 is flexibly connected by third rotation axis 15 with backboard 13；Wherein,
Second rotation axis 14 is set in parallel with backboard 13, and third rotation axis 15 is vertical setting with backboard 13；Outside first electric cylinders 16
Sleeve is arranged on the first bearing 18, and the outer sleeve of the first electric cylinders 16 is flexibly connected with the first bearing 18, and the first bearing 18 is solid
It is scheduled on backboard 13, the external part of the first electric cylinders 16 is flexibly connected with cockpit 11；Second electric cylinders 17 are arranged on the second bearing 19,
And second electric cylinders 17 be flexibly connected with the second bearing 19, the second bearing 19 is fixed on cockpit hanger 1, the stretching of the second electric cylinders 17
End is flexibly connected with backboard 13.
As shown in figure 9, connecting rod 28 is provided between cockpit hanger 1 and backboard 13, one end and the backboard 13 of connecting rod 28
Flexible connection, the other end of connecting rod 28 are provided with kidney slot 29, the first screw 30, the first screw are fixed on cockpit hanger 1
30 are located in kidney slot 29.As shown in Figure 10, multiple arcs limiting slot 31 is provided on backboard 13,11 back side of cockpit is fixed with more
A second screw 32, second screw 32 correspond to an arc-shaped limit slot 31, and second screw 32 is located at an arc
In limiting slot 31.
The operation principle of cockpit swing mechanism is：Second electric cylinders 17 are flexible so that backboard 13 is around the second rotation axis 14
Front and rear rotation, also just band moving-base cockpit 11 realizes front and rear rotation to backboard 13, and in rotation process, the first screw 30 and kidney slot 29 are right
Position-limiting action is played in the front and rear rotation of backboard 13；First electric cylinders 16 are flexible so that cockpit 11 is realized around third rotation axis 15
Left-right rotation, in rotation process, the second screw 32 and arc-shaped limit slot 31 play position-limiting action to the left-right rotation of cockpit 11.
In addition, being additionally provided with safety Crowbar Pressing 33 and Electromgnetic seat belt on cockpit 11, safety Crowbar Pressing 33 passes through movable rod 34
It is flexibly connected with cockpit 11；The solenoid valve of control folding condition is separately provided on safety Crowbar Pressing 33 and Electromgnetic seat band
57, and according to the viewing system mode for the movie theatre that circles in the air, opening or closing for solenoid valve 57 is controlled using power on/off mode, in fact
It now automatically controls, while the folding condition of solenoid valve 57 is judged by contact sensor 56, so as to play protective action, it is ensured that see
The safety of actor or actress person.Solenoid valve 57 is Electromagnetic bolt or electromagnetic lock.
Above-mentioned all structures are all provided on steel construction 12, and steel construction 12 includes several vertical supporting rods, several horizontal strokes
To supporting rod, connecting angle iron, the both ends of transverse support bar are fixedly connected with the both ends of vertical supporting rod by connecting angle iron, in horizontal stroke
Several vertical supporting rods are similarly provided among to supporting rod, more enhances stability, makes steel construction 12 so more
Stablize.The side of steel construction 12 is provided with revolution ladder, above and below spectators, and has the function of to stablize support.
In the movie theatre that circles in the air, when spectators are sitting in viewing film in cockpit 11, since spectators hang on aerial, place oneself in the midst of
Among spherical screen, in order to which spectators is allowed to have feeling on the spot in person, cockpit system can cause cockpit 11 and cockpit hanger 1 to exist
It moves linearly back and forth on steel construction 12 under the drive of cockpit linear moving apparatus, and can cause cockpit 11 on cockpit hanger 1
Front and rear rotation and left-right rotation allow spectators while fully impression extremely powerful ball curtain movie and television contents, can also be personal
The excitement that vacantly flies is experienced by better 4D viewings is brought to experience.The linear movement of cockpit linear moving apparatus, cockpit 11
Rotation and the overturning of protection turnover panel 22-1 all controlled by controller 35.
As shown in figure 11, controller 35 includes main control unit 50 and the cockpit being connect respectively with main control unit linear movement control
Unit 51 processed, protection turnover panel rotation control unit 52, cockpit revolution rotation control unit 53, emergency stop control unit 54 and activity are even
Bar control unit 55；Cockpit linear movement control unit 51 is electrically connected with the first motor 20, and control cockpit linear moving apparatus makes
Cockpit is moved along tandem；Protection turnover panel rotation control unit 52 is electrically connected with the second motor 22-6, control protection turnover panel 22-
1 spins upside down；Cockpit revolution rotation control unit 53 is electrically connected respectively with the first electric cylinders 16 and the second electric cylinders 17, and control cockpit returns
Rotation mechanism causes the front and rear rotation of cockpit 11 and left-right rotation；Emergency stop control unit 54 is electrically connected with scram button 36, in urgent feelings
It presses to prevent unexpected generation under condition；Movable rod control unit 55 is then according to viewing system mode and contact sensor 56
Output signal, to control the unlatching of solenoid valve 57 and closure.Wherein main control unit 50 is real using programmable logic array PLC
Existing, other each control units are then realized using conventional drive module.Such as cockpit linear movement control unit 51, protection
Turnover panel rotation control unit 52, cockpit revolution rotation control unit 53, emergency stop control unit 54 and movable rod control unit 55
It is relay.By taking cockpit moves linearly control unit 51 as an example, linear movement control pulse is sent out by PLC, corresponding to driving
Relay be closed so that the first motor 20 is powered, and control cockpit linear moving apparatus movement makes cockpit be moved along tandem
It is dynamic.
The workflow of controller 35 is：
1. controller 35 controls the second motor 22-6 to rotate by the way that turnover panel is protected to rotate control unit 52, make protection turnover panel
22-1 is overturn forward to vertical position, and spectators climb up cockpit platform 23 by the ladder on steel construction 12.
2. when spectators are seated in the seat of cockpit 11, controller 35 controls movable rod by movable rod control unit 55
34 put down, and safety Crowbar Pressing 33, which is kept off, plays a protective role to spectators before spectators, and the solenoid valve 57 on safety Crowbar Pressing 33 is closed, and see
Crowd oneself buckles Electromgnetic seat belt again, and the solenoid valve 57 on Electromgnetic seat band is closed；Then safety Crowbar Pressing 33 and electromagnetism are arranged on
Contact sensor 56 on safety belt sends a signal to controller 35.
After 3. controller 35 receives the signal of contact sensor 56, it is single that controller 35 turns round rotation control by cockpit again
Member 53 controls the second electric cylinders 17 to act so that cockpit 11 lifts.
4. controller 35 controls the second motor 22-6 rotations by the way that turnover panel is protected to rotate control unit 52 again so that protection is turned over
Plate 22-1 turns over leans against the top of guide rail 22-3 to initial position, that is, protection turnover panel 22-1；
5. controller 35 controls the first motor 20 to rotate by cockpit linear movement control unit 51 so that the first rotation axis
3 rotations, entire cockpit hanger 1 are moved ahead to motion picture screen direction with moving-base cockpit 11 until stopping；
6. film starts, controller 35 turns round rotation control unit 53 control the according to programme content and sound effect by cockpit
One electric cylinders 16 and the second electric cylinders 17 act so that cockpit 11 is front and rear and left-right rotation；
After 7. film is watched, controller 35 turns round rotation control unit 53 by cockpit and controls the first electric cylinders 16 and the
Two electric cylinders 17 act so that the reset of cockpit 11 returns to initial position；
8. controller 35 controls the first motor 20 to rotate backward by cockpit linear movement control unit 51 so that first turn
Moving axis 3 rotates backward, and entire cockpit hanger 1 is retreated with moving-base cockpit 11 to initial position；
9. controller 35 controls the second motor 22-6 to rotate backward by the way that turnover panel is protected to rotate control unit 52 so that protection
Turnover panel 22-1 is overturn forward to vertical position, is in 90 ° of angles with cockpit platform 23；
The second electric cylinders 17 is controlled to act 10. controller 35 turns round rotation control unit 53 by cockpit so that cockpit 11 is put
Under；
11. last, controller 35 controls movable rod control unit 55 to power off, on safety Crowbar Pressing 33 and Electromgnetic seat band
Solenoid valve 57 is opened, and spectators lift safety Crowbar Pressing 33, and spectators oneself open Electromgnetic seat belt, leave seat, and pass through
Cockpit platform 23 and ladder reach ground.
If burst accident, presses emergency stop push button 36, controller 35 controls movable rod 34, the first motor 20, the
One electric cylinders 16, the second electric cylinders 17 and the second motor 22-6 stoppings action.
Claims (3)
1. the cockpit swing mechanism for the movie theatre that circles in the air, it is characterised in that：Including backboard (13), the second rotation axis (14), third rotation
Axis (15), the first electric cylinders (16) and the second electric cylinders (17)；The backboard (13) be arranged on cockpit (11) and cockpit hanger (1) it
Between, backboard (13) is flexibly connected by the second rotation axis (14) with cockpit hanger (1), and cockpit (11) passes through third rotation axis (15)
It is flexibly connected with backboard (13)；Wherein, the second rotation axis (14) is set in parallel with backboard (13), third rotation axis (15) and the back of the body
Plate (13) is vertical setting；The outer sleeve of first electric cylinders (16) is arranged on the first bearing (18), and the first electric cylinders (16) is outer
Sleeve is flexibly connected with the first bearing (18), and the first bearing (18) is fixed on backboard (13), the external part of the first electric cylinders (16)
It is flexibly connected with cockpit (11)；Second electric cylinders (17) are arranged on the second bearing (19), and the second electric cylinders (17) and the second bearing
(19) it is flexibly connected, the second bearing (19) is fixed on cockpit hanger (1), and the external part and backboard (13) of the second electric cylinders (17) are living
Dynamic connection；Cockpit platform (23) is provided with below cockpit (11), the front end of cockpit platform (23) and protection turnover panel (22-1) are living
Dynamic connection.
2. the cockpit swing mechanism for the movie theatre that circles in the air according to claim 1, it is characterised in that：The cockpit hanger (1) and the back of the body
Connecting rod (28) is provided between plate (13), one end of connecting rod (28) is flexibly connected with backboard (13), connecting rod (28) it is another
One end is provided with kidney slot (29), the first screw (30) is fixed on cockpit hanger (1), the first screw (30) is positioned at kidney slot
(29) in.
3. the cockpit swing mechanism for the movie theatre that circles in the air according to claim 1, it is characterised in that：It is provided on the backboard (13)
Multiple arcs limiting slot (31), cockpit (11) back side are fixed with multiple second screws (32), second screw (32) corresponding one
A arc-shaped limit slot (31), and second screw (32) is in an arc-shaped limit slot (31).
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| CN106178553B true CN106178553B (en) | 2018-07-03 |
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| CN110570743B (en) * | 2019-09-29 | 2022-03-25 | 苏州安全精灵智能科技有限公司 | Eye safety experience equipment and safety experience system |
| CN111745758B (en) * | 2020-06-19 | 2021-12-03 | 李林琴 | Washboard processingequipment |
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| CN106178553A (en) | 2016-12-07 |
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