CN106215436B - A kind of viewing system for the movie theatre that circles in the air - Google Patents
A kind of viewing system for the movie theatre that circles in the air Download PDFInfo
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- CN106215436B CN106215436B CN201610792884.8A CN201610792884A CN106215436B CN 106215436 B CN106215436 B CN 106215436B CN 201610792884 A CN201610792884 A CN 201610792884A CN 106215436 B CN106215436 B CN 106215436B
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- cockpit
- hanger
- rotation
- rotation axis
- backboard
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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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- Seats For Vehicles (AREA)
Abstract
The present invention provides a kind of viewing system for the movie theatre that circles in the air, including steel construction, cockpit, cockpit hanger, protection turnover panel, cockpit linear moving apparatus, cockpit swing mechanism and controller；Cockpit hanger is flexibly connected by cockpit linear moving apparatus with steel construction, and cockpit linear moving apparatus is arranged on the top of cockpit hanger；Cockpit hanger is connect by cockpit swing mechanism with cockpit, and cockpit swing mechanism can make cockpit carry out front-rear direction rotation and left and right directions rotation on cockpit hanger；Cockpit and cockpit hanger can be caused to move linearly back and forth on steel construction under the drive of cockpit linear moving apparatus and cause cockpit front and rear rotation and left-right rotation on cockpit hanger；Spectators are allowed while fully impression extremely powerful ball curtain movie and television contents, the excitement that vacantly flies of can also undergoing is by bringing better 4D viewings to experience.
Description
Technical field
The invention belongs to movie theatre technical fields of circling in the air, and in particular to a kind of viewing system 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 existing movie theatre that circles in the air is broadly divided into screen system and cockpit system, and existing cockpit system design structure is more multiple
Miscellaneous, particularly degree of freedom platform needs multiple cylinders to be adjusted, increases the manufacture cost of cockpit system, Er Qiezuo significantly
The safety measure of cabin system is less, is susceptible to safety accident, for example suddenly after power-off, cockpit system runs out of steam, and can not return
Return support platform, personnel do not fasten seat belts cockpit start, lack safety system the defects of.And due to complicated dimension
It protects very inconvenient, a large amount of manpower is needed to be operated, the more wasteful time.
Invention content
Simple in structure the object of the present invention is to provide a kind of cockpit system for the movie theatre that circles in the air, convenient for safeguarding, security system is complete
It is kind, it is easy to operate, and better 4D viewings can be brought to experience to spectators.
The technical solution adopted by the present invention is as follows：
A kind of viewing system for the movie theatre that circles in the air, including steel construction, cockpit, cockpit platform, cockpit hanger, cockpit linear movement
Device, cockpit swing mechanism and controller；The cockpit platform is arranged in the middle part of steel construction, and positioned at the lower section of cockpit；It is described
Cockpit hanger is flexibly connected by cockpit linear moving apparatus with steel construction, and cockpit linear moving apparatus is arranged on cockpit hanger
Top；Cockpit hanger is connect by cockpit swing mechanism with cockpit, and the cockpit swing mechanism can make cockpit on cockpit hanger
Carry out front-rear direction rotation and left and right directions rotation；
Control unit that the controller includes main control unit and the cockpit that is connect respectively with main control unit moves linearly and
Cockpit revolution rotation control unit；The cockpit linear movement control unit control cockpit linear moving apparatus makes cockpit before
After move linearly；The cockpit revolution rotation control unit control cockpit swing mechanism causes the front and rear rotation of cockpit and left/right rotation
It is dynamic.
In the viewing system of the above-mentioned movie theatre that circles in the air, the protection turnover panel for being arranged on cockpit platform front end is further included, described is anti-
Shield turnover panel is connect with cockpit platform activity；The protection turnover panel back side is provided with pushing mechanism；Branch is fixed on the steel construction
Support is fixed with guide rail on supporting rack；Pushing mechanism is flexibly connected with guide rail.
In the viewing system of the above-mentioned movie theatre that circles in the air, pushing mechanism includes stent, the second motor, transmission shaft, is located at transmission shaft
The idler wheel at both ends；The second motor fixation is located on stent, and the stent is fixed on the top at the protection turnover panel back side, described
Second gear is arranged on the output shaft of second motor, the transmission shaft is threaded through on stent, and is arranged on the transmission shaft
Third gear, the second gear are engaged with third gear, and the idler wheel is located in guide rail.
In the viewing system of the above-mentioned movie theatre that circles in the air, the cockpit linear moving apparatus includes two support plates and the first rotation
Axis；First rotation axis is arranged on the top of cockpit hanger, and the both ends of the first rotation axis are respectively arranged with first gear, and first
Speed reducer is provided in rotation axis, speed reducer is fixed on cockpit hanger；Two support plates are respectively positioned at cockpit hanger
Both sides are fixed with rack in every support plate；The first gear at the first rotation axis both ends respectively with the rack in two support plates
Engagement.
In the viewing system of the above-mentioned movie theatre that circles in the air, four ends of cockpit hanger top surface are respectively fixed with fender rod；It is described
One end of fender rod is fixed on cockpit hanger, and the other end is pressed on rack.
In the viewing system of the above-mentioned movie theatre that circles in the air, four ends of cockpit hanger top surface are respectively arranged with limiting device；Institute
State limiting device and include a mounting base and two walking support wheels, two walking support wheels in setting up and down in mounting base,
Support plate is clipped between two walking support wheels up and down；The mounting base is fixed on cockpit hanger.
In the viewing system of the above-mentioned movie theatre that circles in the air, the first power input shaft and the input of the second power are provided on speed reducer
Axis；First power input shaft is connect with the first motor, and hand crank is provided in front of the second power input shaft.
In the viewing system of the above-mentioned movie theatre that circles in the air, cockpit swing mechanism include backboard, the second rotation axis, third rotation axis,
First electric cylinders and the second electric cylinders；The backboard is arranged between cockpit and cockpit hanger, and backboard passes through the second rotation axis and cockpit
Hanger is flexibly connected, and cockpit is flexibly connected by third rotation axis with backboard；Wherein, the second rotation axis is set with backboard in parallel
It puts, third rotation axis is vertical setting with backboard；The outer sleeve of first electric cylinders is arranged on the first bearing, and the first electric cylinders is outer
Sleeve 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；The
Two 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,
The external part of second electric cylinders is flexibly connected with backboard.
In the viewing system of the above-mentioned movie theatre that circles in the air, connecting rod, one end of connecting rod are provided between cockpit hanger and backboard
It is flexibly connected with backboard, the other end of connecting rod is provided with kidney slot, and the first screw, the first screw position are fixed on cockpit hanger
In in kidney slot.
In the viewing system of the above-mentioned movie theatre that circles in the air, multiple arcs limiting slot is provided on backboard, the cockpit back side is fixed with more
A second screw, second screw corresponds to an arc-shaped limit slot, and second screw is located in an arc-shaped limit slot.
Beneficial effects of the present invention are as follows：
1st, the present invention provides three-dimensional motion modes, and cockpit and cockpit hanger can be caused in cockpit linear moving apparatus
It moves linearly back and forth on steel construction under drive, and sight can be allowed so that cockpit front and rear rotation and left-right rotation on cockpit hanger
Crowd while fully impression extremely powerful ball curtain movie and television contents, can also undergo the excitement that vacantly flies by,
Better 4D viewings is brought to experience.
2nd, cockpit linear moving apparatus of the invention, there is provided electronic and manual two ways to drive cockpit hanger and seat
Cabin moves linearly on steel construction, even if the power supply failed, by that also cockpit can be made to be moved on steel construction manually；Simultaneously in power failure
In the case of, can cockpit be reset to by initial position by hand cranking handle and left, it is ensured that the safety of spectators.
3. the present invention is provided with protection turnover panel in the front of cockpit linear moving apparatus, can be as desired by second
Digging and resetting for protection turnover panel is realized in the control of motor；Before spectators watch film, protection turnover panel is overturn forward to vertical position,
Spectators climb up cockpit platform by the ladder on steel construction, are then sitting on the seat of cockpit and prepare viewing film, there is protection
The protection of turnover panel can prevent away cockpit platform under spectators' pendant on cockpit platform；After spectators sit straight on the seat, film
Broadcasting starts, and protection turnover panel, which is turned over, leans against the top of guide rail.In addition it is reasonable to be provided between pushing mechanism and protection turnover panel
Angle so that thrust used is smaller during protection turnover panel overturning, reduces the output power of the second motor.
4. support plate is clipped in the support that walks up and down by the cockpit linear moving apparatus of the present invention using rack pinion
Wheel is intermediate, and gear is prevented to be detached from rack, the upper and lower of cockpit is caused to alter jump；Increase fender rod behind support wheel simultaneously, cockpit moves
Fender rod also and then rotates during dynamic, plays a supporting role, can cause uniform force between two support plates, equally play
Make the effect that cockpit operates steadily.
5. the present invention position appropriate at support plate both ends increases Buffer Unit, the progress to cockpit linear moving apparatus
The limiting of position is moved forward and backward, once controller breaks down, cockpit touches buffering first beyond the range run, support wheel
On component, failure is had occurred support wheel, the fender rod behind support wheel can equally touch Buffer Unit so that cockpit is thorough
Bottom is braked, and is played the role of dual fail-safe, is avoided the generation of peril.Simultaneously because touching is Buffer Unit, can prevent
Cockpit emergency stop is injured caused by passenger.
6. the cockpit swing mechanism of the present invention is provided with rotary spacing component, by setting multiple arcs on cockpit backboard
Shape limiting slot, and including embedded screw, position-limiting action is played to the left-right rotation of cockpit, while between cockpit hanger and backboard
Connecting rod on be provided with kidney slot, 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 processed；In case of off-axis, moreover it is possible to prevent cockpit from falling.
7. the present invention is provided with safety Crowbar Pressing and Electromgnetic seat belt on cockpit, distinguish on safety Crowbar Pressing and Electromgnetic seat band
It is provided with the solenoid valve of control folding condition；According to the viewing system mode for the movie theatre that circles in the air, electricity is controlled using power on/off mode
Magnet valve realizes opening or closing for bolt, and realization automatically controls, so as to playing protective action, prevent program carry out in spectators will
Switch is artificial to be opened, it is ensured that the safety of viewing personnel.
8. the steel construction of the present invention is fixedly connected using several horizontal and vertical supporting rods staggeredly by hinge, increase
The stability of carrying, while the side of steel construction is provided with the revolution people row order ladder of large area, which connects firmly with steel construction
Together, bottom area and stability of equilibrium are increased, it is ensured that will not when manned because centre-of gravity shift due to topple over.
9. the present invention is controlled before and after the linear reciprocating motion of cockpit linear moving apparatus, cockpit by controller and left and right
Rotation and the overturning of protection turnover panel, safe, high degree of automation is easy to operate, and there is provided emergency stops in the controller to press
Button, in case of emergency brake in time.
Description of the drawings
Fig. 1 is the structure diagram that movie theatre cockpit system is arranged on steel construction of the invention 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 of the present invention, cockpit hanger and cockpit；
Fig. 4 is the structure diagram of speed reducer of the present invention, the first motor and hand crank；
Fig. 5 is the B portions enlarged drawing of Fig. 4；
Fig. 6 is the structure diagram that protection turnover panel and cockpit platform of the invention are arranged on steel construction；
Fig. 7 is the structure diagram of present invention protection turnover panel, supporting rack and propulsive mechanism；
Fig. 8 is the structure diagram of pushing mechanism in the present invention；
Fig. 9 is the structure diagram of cockpit swing mechanism of the present invention, cockpit hanger and cockpit；
Figure 10 is the structure diagram that backboard of the present invention is arranged on cockpit hanger；
Figure 11 is control system architecture schematic diagram of the present invention.
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, the present invention provides a kind of viewing system for the movie theatre that circles in the air, including steel construction 12, cockpit 11, cockpit
Platform 23, cockpit hanger 1, cockpit linear moving apparatus, cockpit swing mechanism and controller 35；Cockpit hanger 1 is straight by cockpit
Line mobile 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
It is connect by cockpit swing mechanism with cockpit 11, cockpit swing mechanism can make cockpit 11 carry out front-rear direction on cockpit hanger 1
Rotation and left and right directions rotation；In addition, 12 middle part of steel construction is equipped with cockpit platform 23, cockpit platform 23 is located under cockpit 11
Side, the front end of cockpit platform 23 are 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, the first rotation axis 3
The first gear 4 at both ends also and then rotate, realize that first gear 4 moves linearly on rack 6,3 He of the first rotation axis afterwards
First gear 4 also just drives entire cockpit hanger 1 and cockpit 11 to move linearly back and forth between two support plates 2.In cockpit
Four end sets, four fender rods 7 of 1 top surface of hanger, fender rod 7 is pressed on rack 6, in 1 moving process of cockpit hanger,
Fender rod 7 also and then rotates, and the effect of fender rod 7 is to support entire cockpit hanger 1 and cockpit 11, hangs over cockpit hanger 1
Uniform force between two support plates prevents cockpit hanger 1 from play up and down occurring in moving process.In 1 top surface of cockpit hanger
Four ends also set up limiting device, support plate 2 is clipped between two walking support wheels 9 up and down, is moved through in cockpit hanger 1
Cheng Zhong, all walking support wheels 9 also and then rotate, and the effect one of walking support wheel 9 is to play a supporting role, another
It is the track for preventing first gear 4 from deviating from rack 6 in rotation process, there are one be that can also prevent cockpit hanger 1 in movement
Play up and down occurs in the process.
In addition, for the limiting for be moved forward and backward position to cockpit linear moving apparatus, controller 35 is avoided to occur
Cockpit linear moving apparatus deviates from the track of rack 6 and causes danger during failure, in the appropriate location at the both ends of two support plates 2
Place is respectively provided with four Buffer Units 58, and when cockpit linear moving apparatus is moved to restraining position, Buffer Unit 58 can hinder
Walking support wheel 9 is hindered to move on, so as to avoid the rectilinear orbit of the abjection operation of cockpit 11, it is ensured that the safety of viewing personnel
Property.Simultaneously in this case even if walk support wheel 9 break down, then Buffer Unit 58 can touch walk support wheel 9
Fender rod 7 below equally plays the role of being moved forward and backward cockpit 11 limiting of position, plays dual fail-safe.Buffer Unit 58
The metal bar for increasing flexible rubber bar or carrying spring below can be used, once support wheel 9 or fender rod 7 are touched
When, play the role of buffering, avoid the unexpected emergency stop of cockpit.
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 initial angle of 23 front end of cabin platform is also 30 ° to 45 °, and preferred angle is 40 °, when can make protection turnover panel 22-1 overturnings in this way
Thrust used is smaller, reduces the output power of the second motor 22-6
As shown in Figure 9 and Figure 10, cockpit swing mechanism includes backboard 13, the second rotation axis 14, third rotation axis 15, first
16 and second electric cylinders 17 of electric cylinders；Backboard 13 is arranged between cockpit 11 and cockpit hanger 1, backboard 13 by the second rotation axis 14 with
Cockpit hanger 1 is flexibly connected, and cockpit 11 is flexibly connected by third rotation axis 15 with backboard 13；Wherein, the second rotation axis 14 with
Backboard 13 is set in parallel, and third rotation axis 15 is vertical setting with backboard 13；The outer sleeve of first electric cylinders 16 is arranged on first
On 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 fixed on backboard 13, the
The external part of one electric cylinders 16 is flexibly connected with cockpit 11；Second electric cylinders 17 are arranged on the second bearing 19, and the second electric cylinders 17 with
Second bearing 19 is flexibly connected, and the second bearing 19 is fixed on cockpit hanger 1, external part and 13 activity of backboard of the second electric cylinders 17
Connection.
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 of the present invention can cause cockpit 11 and cockpit
Hanger 1 moves linearly back and forth under the drive of cockpit linear moving apparatus on steel construction 12, and cockpit 11 can be caused in cockpit
Front and rear rotation and left-right rotation on hanger 1 allow spectators may be used also while fully impression extremely powerful ball curtain movie and television contents
With the excitement that vacantly flies of undergoing by better 4D viewings is brought to experience.The linear movement of cockpit linear moving apparatus,
The rotation of cockpit 11 and the overturning of protective fence ontology 22-1 are 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 50 linear movement
Control unit 51, protection turnover panel rotation control unit 52, cockpit revolution rotation control unit 53, emergency stop control unit 54 and activity
Connecting rod control unit 55；Cockpit linear movement control unit 51 is electrically connected with the first motor 20, controls cockpit linear moving apparatus
Cockpit is made to be moved along tandem；Protection turnover panel rotation control unit 52 is electrically connected with the second motor 22-6, control protection turnover panel
22 spin upside down；Cockpit revolution rotation control unit 53 is electrically connected with the first electric cylinders 16 and the second electric cylinders 17, control cockpit revolution
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 emergency
Under press to prevent unexpected generation；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 realized using programmable logic array PLC,
Other each control units are then realized using conventional drive module.For example cockpit linear movement control unit 51, protection are turned over
Plate rotation control unit 52, cockpit revolution rotation control unit 53, emergency stop control unit 54 and movable rod control unit 55 are equal
For relay.By taking cockpit moves linearly control unit 51 as an example, linear movement control pulse is sent out by PLC, is driven corresponding
Relay is closed so that the first motor 20 is powered, and the linear moving apparatus movement of control cockpit makes cockpit be moved along tandem.
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 (9)
1. a kind of viewing system for the movie theatre that circles in the air, it is characterised in that：Including steel construction (12), cockpit (11), cockpit platform (23),
Cockpit hanger (1), cockpit linear moving apparatus, cockpit swing mechanism and controller (35)；The cockpit platform (23) is arranged on
In the middle part of steel construction (12), and positioned at the lower section of cockpit (11)；The cockpit hanger (1) passes through cockpit linear moving apparatus and steel knot
Structure (12) is flexibly connected, and cockpit linear moving apparatus is arranged on the top of cockpit hanger (1)；Cockpit hanger (1) is returned by cockpit
Rotation mechanism is connect with cockpit (11), and the cockpit swing mechanism can make cockpit (11) carry out front-rear direction on cockpit hanger (1)
Rotation and left and right directions rotation；
The cockpit linear movement control that the controller (35) is connect including main control unit (50) and respectively with main control unit (50)
Unit (51) processed and cockpit revolution rotation control unit (53)；The cockpit linear movement control unit (51) controls cockpit straight
Line mobile device makes cockpit (11) be moved along tandem；The cockpit revolution rotation control unit (53) controls cockpit revolution
Mechanism causes the front and rear rotation of cockpit (11) and left-right rotation；
The protection turnover panel (22-1) for being arranged on cockpit platform (23) front end is further included, the protection turnover panel (22-1) is put down with cockpit
Platform (23) is flexibly connected；Described protection turnover panel (22-1) back side is provided with pushing mechanism；Branch is fixed on the steel construction (12)
Support (22-2) is fixed with guide rail (22-3) on supporting rack (22-2)；Pushing mechanism is flexibly connected with guide rail (22-3)；
Safety Crowbar Pressing (33) is additionally provided on cockpit (11), safety Crowbar Pressing (33) passes through movable rod (34) and cockpit (11) activity
Connection.
2. the viewing system for the movie theatre that circles in the air according to claim 1, it is characterised in that：The pushing mechanism includes stent
(22-7), the second motor (22-6), transmission shaft (22-4), the idler wheel (22-5) for being located at transmission shaft (22-4) both ends；Described
Two motors (22-6) fixation is located on stent (22-7), and the stent (22-7) is fixed on the upper of protection turnover panel (22-1) back side
Portion is arranged with second gear (22-8) on the output shaft of second motor (22-6), and the transmission shaft (22-4) is threaded through
On stent (22-7), and third gear (22-9) is arranged on the transmission shaft (22-4), the second gear (22-8) and the
Three gears (22-9) engage, and the idler wheel (22-5) is in guide rail (22-3).
3. the viewing system for the movie theatre that circles in the air according to claim 1, it is characterised in that：The cockpit linear moving apparatus includes
Two support plates (2) and the first rotation axis (3)；First rotation axis (3) is arranged on the top of cockpit hanger (1), first turn
The both ends of moving axis (3) are respectively arranged with first gear (4), and speed reducer (5) is provided in the first rotation axis (3), and speed reducer (5) is solid
It is scheduled on cockpit hanger (1)；Two support plates (2) are respectively on the both sides of cockpit hanger (1), every support plate (2)
It is fixed with rack (6)；The first gear (4) at the first rotation axis (3) both ends is nibbled respectively with the rack (6) on two support plates (2)
It closes.
4. the viewing system for the movie theatre that circles in the air according to claim 3, it is characterised in that：The four of cockpit hanger (1) top surface
A end is respectively fixed with fender rod (7)；One end of the fender rod (7) is fixed on cockpit hanger (1), and the other end is pressed in tooth
On item (6).
5. the viewing system for the movie theatre that circles in the air according to claim 3, it is characterised in that：The four of cockpit hanger (1) top surface
A end is respectively arranged with limiting device；The limiting device includes a mounting base (8) and two and walks support wheels (9), and two
It is a walking support wheel (9) in setting up and down in mounting base (8), support plate (2) be clipped in up and down two walking support wheel (9) it
Between；The mounting base (8) is fixed on cockpit hanger (1).
6. the viewing system for the movie theatre that circles in the air according to claim 3, it is characterised in that：Is provided on the speed reducer (5)
One power input shaft and the second power input shaft (25)；First power input shaft is connect with the first motor (20), and the second power is defeated
Enter and be provided with hand crank (21) in front of axis (25).
7. the viewing system for the movie theatre that circles in the air according to claim 1, it is characterised in that：The cockpit swing mechanism includes 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) sets
It puts between cockpit (11) and cockpit hanger (1), backboard (13) is connected by the second rotation axis (14) and cockpit hanger (1) activity
It connects, cockpit (11) is flexibly connected by third rotation axis (15) with backboard (13)；Wherein, the second rotation axis (14) and backboard (13)
It is set in parallel, third rotation axis (15) is vertical setting with backboard (13)；The outer sleeve of first electric cylinders (16) is arranged on first
On 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 fixed on the back of the body
On plate (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) on, and the second electric cylinders (17) are flexibly connected with the second bearing (19), and the second bearing (19) is fixed on cockpit hanger (1),
The external part of second electric cylinders (17) is flexibly connected with backboard (13).
8. the viewing system for the movie theatre that circles in the air according to claim 7, it is characterised in that：The cockpit hanger (1) and backboard
(13) connecting rod (28) is provided between, one end of connecting rod (28) is flexibly connected with backboard (13), connecting rod (28) it is another
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)
It is interior.
9. the viewing system for the movie theatre that circles in the air according to claim 7, it is characterised in that：It is provided on the backboard (13) multiple
Arc-shaped limit slot (31), cockpit (11) back side are fixed with multiple second screws (32), and second screw (32) corresponds to an arc
Shape limiting slot (31), and second screw (32) is in an arc-shaped limit slot (31).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610792884.8A CN106215436B (en) | 2016-08-31 | 2016-08-31 | A kind of viewing system for the movie theatre that circles in the air |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610792884.8A CN106215436B (en) | 2016-08-31 | 2016-08-31 | A kind of viewing system for the movie theatre that circles in the air |
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| Publication Number | Publication Date |
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| CN106215436A CN106215436A (en) | 2016-12-14 |
| CN106215436B true CN106215436B (en) | 2018-07-03 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201610792884.8A Active CN106215436B (en) | 2016-08-31 | 2016-08-31 | A kind of viewing system for the movie theatre that circles in the air |
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Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN108854115A (en) * | 2018-09-18 | 2018-11-23 | 深圳市鑫美幻想工程有限公司 | A kind of safe flight ball curtain formula movie theatre |
| CN109381876B (en) * | 2018-10-31 | 2024-06-18 | 浙江圣邦游乐装备有限公司 | Flight cinema with multi-degree-of-freedom aerial overlook flight device |
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| CN104133491A (en) * | 2014-07-29 | 2014-11-05 | 上海恒润数字科技股份有限公司 | Multi-degree-of-freedom flight seat of flight cinema, and control system and method of multi-degree-of-freedom flight seat of flight cinema |
| CN204364901U (en) * | 2014-12-30 | 2015-06-03 | 深圳市远望淦拓科技有限公司 | A kind of flight movie theatre multidimensional seat |
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| JP2006187537A (en) * | 2005-01-07 | 2006-07-20 | Okamura Corp | Leg frame structure of chair |
| CN104133491A (en) * | 2014-07-29 | 2014-11-05 | 上海恒润数字科技股份有限公司 | Multi-degree-of-freedom flight seat of flight cinema, and control system and method of multi-degree-of-freedom flight seat of flight cinema |
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| CN106215436A (en) | 2016-12-14 |
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