CN206233649U - Swing aerial arenas - Google Patents
Swing aerial arenas Download PDFInfo
- Publication number
- CN206233649U CN206233649U CN201621319143.XU CN201621319143U CN206233649U CN 206233649 U CN206233649 U CN 206233649U CN 201621319143 U CN201621319143 U CN 201621319143U CN 206233649 U CN206233649 U CN 206233649U
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- CN
- China
- Prior art keywords
- support arm
- swing
- cockpit
- aerial
- base
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- Power-Operated Mechanisms For Wings (AREA)
Abstract
The utility model discloses a kind of swing aerial arenas, it includes the arc curtain that interview room, two be arranged in interview room be symmetrical set, the base being arranged between two arcs curtain, is fixedly installed in the middle of base upper end and waves bearing, a support arm, the support arm middle part is articulated in waves bearing upper end, so that the support arm left and right sides can carry out teetering for seesaw type;The left and right sides of the support arm is respectively connected with two rows towards the cockpit of arc curtain;The support arm left and right sides carries out teetering for seesaw type, thus can true representation flight movie theatre intermediate item the experience effect for taking off and falling so that the spectators in cockpit have cognition sense on the spot in person;And video display had when falling jump out of the building the impression of machine so that the utility model combine video display jump out of the building two projects of machine and flight movie theatre the characteristics of and viewing impression.
Description
Technical field
The utility model is related to a kind of deduction system, more particularly to a kind of swing aerial arenas.
Background technology
With the improvement of living standards, requirement more and more higher of the people to amusement and recreation activity, common cinema's viewing
Pattern lacks effect true to nature so that spectators cannot have cognition sense on the spot in person, so as to can less meet demand.
Utility model content
The purpose of this utility model is to provide a kind of swing aerial arenas.
To achieve the above object, the technical scheme that the utility model is used is:
A kind of swing aerial arenas, including an interview room, two being symmetrical set of being arranged in the interview room
Arc curtain, the base being arranged between two arc curtain, be fixedly installed in the middle of the base upper end wave bearing, one
Brace, support arm middle part be articulated in it is described wave bearing upper end so that the support arm left and right sides can carry out seesaw
Formula is teetered, and the support arm and described being waved be provided with for driving the support arm left and right sides between bearing
Under wave and the wabbler mechanism of swing angle can be controlled;The left and right sides of the support arm is respectively connected with two rows towards described
The cockpit of arc curtain, the two rows cockpit is connected to the both sides up and down of the support arm.
The upper end at the support arm or so two ends is provided with adjustable for height overhead gage, and the overhead gage is located at the cockpit
Between arc curtain.
The left and right sides of the base is respectively connected with L-shaped lower baffle plate, and the L-shaped lower baffle plate includes lateral part and from institute
The vertical section that lateral part side up extends is stated, lateral part opposite side is connected with the base.
The lateral part opposite side is rotatably connected with the base, and between the L-shaped lower baffle plate and the base
The drive device for driving the L-shaped lower baffle plate rotation is provided with, when the drive device drives the L-shaped lower baffle plate up
When rotation to the vertical section is located at vertical state, the lateral part is located at the lower section in lower row seat cabin, and vertical section is located at
Between the lower row seat cabin and arc curtain.
The first control for controlling to be rotated before and after row's cockpit is provided with described in each row between cockpit and the support arm
Device processed.
The for controlling row's cockpit pitching type rotation is additionally provided with described in each row between cockpit and the support arm
Two control devices.
Support base is fixedly installed on the support arm, the chair back of the row cockpit is rearwardly extending before being both secured to one
On pole, the first control device is set to motor, and described motor one end is rotatably connected in the support base, the motor
Motor shaft be fixedly connected with the pole;The second control device is set to hydraulic cylinder, and described hydraulic cylinder one end is fixed and connected
It is connected on the support base, the piston rod of hydraulic cylinder is fixedly connected on the motor.
Support arm upper end both sides are set to inclined-plane.
The interview room rear side is provided with upper and lower two access way, wherein an access way and support arm middle part upper end
Communicate, another access way is communicated with the base upper surface.
Under the control of the wabbler mechanism, the maximum angle that the support arm both sides swing up and down is 20 degree.
The beneficial effects of the utility model are:The symmetrically arranged arc curtain in left and right two is formed as double parantheses huge curtains of shape so that
Viewing effect is more preferable;And support arm is with centre as fulcrum, the left and right sides carries out teetering for seesaw type, so that can real table
The existing experience effect for taking off and falling of flight movie theatre intermediate item, and effect is very true to nature so that in the cockpit of the support arm left and right sides
Spectators have cognition sense on the spot in person;Additionally, video display are had when falling jumping out of the building the impression of machine, that is to say, that this practicality is new
Type combine video display jump out of the building two projects of machine and flight movie theatre the characteristics of and viewing impression, in this way, the experience sense of spectators is more preferably.
Brief description of the drawings
Fig. 1 is the schematic perspective view of the swing aerial arenas of the utility model;
Fig. 2 is the floor map one of the swing aerial arenas of the utility model;
Fig. 3 is the floor map two of the swing aerial arenas of the utility model;
Fig. 4 is the top view of the swing aerial arenas of the utility model;
Fig. 5 is the enlarged diagram according to part A in Fig. 2.
Specific embodiment
As shown in Fig. 1,2,3,4,5, the swing aerial arenas of the utility model includes an interview room 1, is arranged at the sight
See in room 1 the two arc curtains 2 being symmetrical set, the base 3 being arranged between the two arcs curtain 2, be fixedly installed on institute
State and wave bearing 4, a support arm 5 in the middle of the upper end of base 3, the middle part of the support arm 5 be articulated in it is described wave the upper end of bearing 4,
So as to the left and right sides of the support arm 5 can carry out teetering for seesaw type(Direction as shown by the arrows in figure 2), and the support
Arm 5 and described being waved be provided between bearing 4 for driving the left and right sides of the support arm 5 to teeter and can control angle of oscillation
The wabbler mechanism of degree(It is not shown);The left and right sides of the support arm 5 is provided with two rows towards the seat of arc curtain 2
Cabin 6, the two rows cockpit 6 is connected to the both sides up and down of the support arm 5.
The rear side of the interview room 1 is provided with upper and lower two access way 7, wherein in an access way 7 and the support arm 5
Portion upper end is communicated, and another access way 7 is communicated with the upper surface of the base 3.In the present embodiment, on the centre of the support arm 5
End is fixed with a supporting plate 51, and the rear end of the supporting plate 51 extends to backward to be connected with the access way 7 of top;The base
3 rear sides are extended to backward to be connected with the access way 7 of downside.
The upper end at the two ends of the support arm 5 or so is provided with adjustable for height overhead gage 8, and the overhead gage 8 is located at described
Between cockpit 6 and arc curtain 2.In the present embodiment, preferably, the overhead gage 8 includes being fixedly connected on the support arm 5
The fixed plate 81 at end and can the portable plate 82 that moves up and down of relatively described fixed plate 81.Up move the work of the overhead gage 8
Dynamic plate 82 is located at the upside of fixed plate 81, so that overhead gage 8 is adjusted to whole height state higher;It is past to move down
The portable plate 82 of the dynamic overhead gage 8 is located at the downside of fixed plate 81 so that the reduction of the whole height of overhead gage 8.Can use
Any feasible known features realize that portable plate 82 is moved up and down with the relative of fixed plate 81.In other embodiments, on described
Baffle plate 8 may be alternatively provided as two folding top and the bottom, it is not necessary to when using, and upper part is folded into lower partial left side or the right side
Side, reduces the whole height of overhead gage 8;When needing to use, lower upper is partly located in expansion, so that upper gear
Plate 8 is adjusted to whole height state higher.
The left and right sides of the base 3 is respectively connected with L-shaped lower baffle plate 9, the L-shaped lower baffle plate 9 include lateral part 91 with
And the vertical section 92 up extended from the side of the lateral part 91, the opposite side of the transverse part 92 is connected with the base 3.
In the present embodiment, the opposite side of the lateral part 91 is rotatably connected with the base 3, and the L-shaped lower baffle plate 9 with it is described
The drive device for driving the rotation of L-shaped lower baffle plate 9 is provided between base 3(It is not shown), when the drive device is driven
Move the L-shaped lower baffle plate 9 up rotate to the vertical section 92 be located at vertical state when, the lateral part 91 be located at lower row
The lower section of cockpit 6, vertical section 92 is located between the lower row seat cabin 6 and arc curtain 2 (state as shown in Figure 2).In this implementation
In example, the drive device is set to hydraulic cylinder, and described hydraulic cylinder one end is fixedly connected on the base, the piston rod of hydraulic cylinder
It is connected to the lateral part 91.In other embodiments, the drive device can also use other feasible known features.
Before spectators enter cockpit 6, overhead gage 8 is adjusted to whole height state higher;L described in Driven by Hydraulic Cylinder
Shape lower baffle plate rotate so that the L-shaped lower baffle plate 9 rotate to the vertical section 92 be located at vertical state when, the transverse part
Divide 91 lower sections for being located at lower row seat cabin 6, now, overhead gage 8 can be as passage and guardrail in order to support with L-shaped lower baffle plate 9
Spectators take a seat into cockpit 6;After the completion of taking a seat, the whole height of overhead gage 8 is turned down, L-shaped lower baffle plate 9 is past described in Driven by Hydraulic Cylinder
Lower rotation so that L-shaped lower baffle plate 9 is overall near base(State as shown in Figure 3), so that overhead gage 8 and L-shaped lower baffle plate 9 not shadow
The visual field of spectators is rung, and after L-shaped lower baffle plate 9 down rotate, moreover it is possible to the lower row seat cabin 6 for avoiding and swinging up and down produces interferes.
In other embodiments, the opposite side of lateral part 91 of the L-type lower baffle plate 9 is fixedly connected on the base 3, institute
Lower section of the lateral part 91 positioned at lower row seat cabin 6 is stated, vertical section 92 is located between the lower row seat cabin 6 and arc curtain 2.Preferably
, the vertical section 92 is equally arranged to adjustable for height pattern with overhead gage 8.Using this structure, then branch must be waved
Seat 4 has certain height, is so just avoided that L-shaped lower baffle plate 9 produces interference with the lower row seat cabin 6 for swinging up and down.
In the present embodiment, preferably, under the control of the wabbler mechanism, the both sides of the support arm 5 swing up and down
Maximum angle is 20 degree.The wabbler mechanism can be any known feasible structure, as long as it can drive the both sides of the support arm 5
Teeter and can control swing angle.
In the present embodiment, it is provided between cockpit 6 and the support arm 5 described in each row for controlling the row seat
The first control device 61 of rotation before and after cabin 6.
Preferably, being additionally provided between cockpit 6 and the support arm 5 described in each row for controlling the row cockpit 6
The second control device 62 of pitching type rotation.
In the present embodiment, support base 52 is fixedly installed on the support arm 5, the chair back of the row cockpit 6 is solid
Before one on rearwardly extending pole 63, the first control device 61 is set to motor, the rotatable company in motor one end
The support base 52 is connected to, the motor shaft of the motor is fixedly connected with the pole 63.Set the direction of motor shaft rotation
With angle, so that when motor works, motor shaft rotation, so as to drive rotation before and after the row cockpit.The second control dress
Put 62 and be set to hydraulic cylinder, described hydraulic cylinder one end is fixedly connected on the support base 52, the piston rod of hydraulic cylinder is fixed and connected
The motor is connected to, so that during hydraulic cylinder works, the flexible of piston rod can drive the motor shaft to rotate up and down, so that one
Row's cockpit 6 carries out pitching type rotation up and down therewith.
In other embodiments, the first control device 61 and second control device 62 can be any known feasible
Device, as long as its one row's cockpit of control 6 can the rotation of the pitching type of opposed support structure 5, front and rear rotation.
After spectators take a seat, whole audience light contract fully, with the action of background music and the wabbler mechanism, arc curtain 2
Start image occur, spectators' aircraft that can feel to be seated flies to have gone up sky, then coordinates wabbler mechanism, first control device 61 and second
Cockpit 6 is various waves rotation for the control of control device 62, and spectators can more realize the various enjoyment of middle fly on high.
In sum, the symmetrically arranged arc in left and right two curtain 2 is formed as double parantheses huge curtains of shape so that viewing effect is more preferable;
And support arm 5, with centre as fulcrum, the left and right sides carries out teetering for seesaw type, so that can true representation flight movie theatre class
The experience effect for taking off and falling of project, and effect is very true to nature so that the spectators in the left and right sides cockpit 6 of support arm 5 have body
Face the cognition sense in its border;Additionally, video display are had when falling jumping out of the building the impression of machine, that is to say, that the utility model combines shadow
The characteristics of depending on two projects of the machine of jumping out of the building and flight movie theatre and viewing are experienced, in this way, the experience sense of spectators is more preferably;First control
The setting of device 61 and second control device 62 so that the rotation mode of cockpit 6 is more, so that experience sense is stronger, more feels true;
And because the maximum angle that the both sides of support arm of the present utility model 5 swing up and down is 20 degree, so that maximum drop is up to 2.8 meters,
It is bigger than traditional flight movie theatre drop, so that better;The left and right sides of support arm 5 is respectively provided with two row's cockpits 6 per side, so that
More spectators can disposably be accommodated.
In the present embodiment, preferably, the upper end both sides of the support arm 5 are set to inclined-plane, so as to be sitting in upper row seat cabin 6
The pin of spectators steps on hanging less than the upper surface of support arm 5, and after the rotation of L-shaped lower baffle plate 9 is gone down, the sight of the row's of sitting down cockpit 3
Many pin are also hanging, in this way, spectators have all the more seating to jump out of the building machine and the experience sense of aircraft.
Be left and right with where two arc curtain 2 in the description of above-mentioned orientation, after being where access way 7, with it is described enter
Go out passage 7 corresponding for preceding.
Claims (10)
1. a kind of swing aerial arenas, it is characterised in that:Including an interview room, be arranged in the interview room it is two or so right
Claim the arc for setting curtain, the base being arranged between the two arcs curtain, be fixedly installed on waving in the middle of the base upper end
Bearing, a support arm, support arm middle part be articulated in it is described wave bearing upper end so that the support arm left and right sides can be entered
Row seesaw type teeters, and the support arm and described waving be provided between bearing left for driving the support arm
Right both sides teeter and can control the wabbler mechanism of swing angle;The left and right sides of the support arm is respectively connected with two rows
Towards the cockpit of arc curtain, the two rows cockpit is connected to the both sides up and down of the support arm.
2. swing aerial arenas according to claim 1, it is characterised in that:The upper end at the support arm or so two ends sets
Adjustable for height overhead gage is equipped with, the overhead gage is located between the cockpit and arc curtain.
3. swing aerial arenas according to claim 1, it is characterised in that:The left and right sides of the base is respectively connected with
L-shaped lower baffle plate, the L-shaped lower baffle plate includes lateral part and the vertical section up extended from the lateral part side,
The lateral part opposite side is connected with the base.
4. swing aerial arenas according to claim 3, it is characterised in that:The lateral part opposite side and the bottom
Seat is rotatably connected, and the drive for driving the L-shaped lower baffle plate rotation is provided between the L-shaped lower baffle plate and the base
Dynamic device, when the drive device driving L-shaped lower baffle plate up rotates is located at vertical state to the vertical section, institute
Lower section of the lateral part positioned at lower row seat cabin is stated, vertical section is located between the lower row seat cabin and arc curtain.
5. swing aerial arenas according to claim 1, it is characterised in that:Cockpit described in each row and the support arm
Between be provided with for control row's cockpit before and after rotate first control device.
6. swing aerial arenas according to claim 5, it is characterised in that:Cockpit described in each row and the support arm
Between be additionally provided with for control row's cockpit pitching type rotation second control device.
7. swing aerial arenas according to claim 6, it is characterised in that:Support is fixedly installed on the support arm
Seat, the chair back of the row cockpit is both secured on pole rearwardly extending before, and the first control device is set to motor,
Described motor one end is rotatably connected in the support base, and the motor shaft of the motor is fixedly connected with the pole;Described
Two control devices are set to hydraulic cylinder, and described hydraulic cylinder one end is fixedly connected on the support base, and the piston rod of hydraulic cylinder is consolidated
Surely it is connected to the motor.
8. the swing aerial arenas according to claim 1 or 2 or 4 or 6 or 7, it is characterised in that:The support arm upper end
Both sides are set to inclined-plane.
9. swing aerial arenas according to claim 8, it is characterised in that:The interview room rear side is provided with upper and lower two
Access way, wherein an access way and the support arm middle part upper end communicate, another access way and the base upper surface
Communicate.
10. swing aerial arenas according to claim 9, it is characterised in that:Under the control of the wabbler mechanism, institute
It is 20 degree to state the maximum angle that support arm both sides swing up and down.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201621319143.XU CN206233649U (en) | 2016-12-01 | 2016-12-01 | Swing aerial arenas |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201621319143.XU CN206233649U (en) | 2016-12-01 | 2016-12-01 | Swing aerial arenas |
Publications (1)
Publication Number | Publication Date |
---|---|
CN206233649U true CN206233649U (en) | 2017-06-09 |
Family
ID=58978756
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201621319143.XU Expired - Fee Related CN206233649U (en) | 2016-12-01 | 2016-12-01 | Swing aerial arenas |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN206233649U (en) |
-
2016
- 2016-12-01 CN CN201621319143.XU patent/CN206233649U/en not_active Expired - Fee Related
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170609 Termination date: 20211201 |
|
CF01 | Termination of patent right due to non-payment of annual fee |