CN104912352B - Viewing aircraft, viewing system and ball curtain viewing arenas - Google Patents
Viewing aircraft, viewing system and ball curtain viewing arenas Download PDFInfo
- Publication number
- CN104912352B CN104912352B CN201510362931.0A CN201510362931A CN104912352B CN 104912352 B CN104912352 B CN 104912352B CN 201510362931 A CN201510362931 A CN 201510362931A CN 104912352 B CN104912352 B CN 104912352B
- Authority
- CN
- China
- Prior art keywords
- viewing
- retractor device
- platform
- aircraft
- runing rest
- 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.)
- Active
Links
Landscapes
- Displays For Variable Information Using Movable Means (AREA)
- Illuminated Signs And Luminous Advertising (AREA)
Abstract
The invention provides a kind of viewing aircraft, viewing system and ball curtain viewing arenas, the viewing aircraft includes the flight frame, fixed point support and retractor device to fixed viewing people standing place, the fixed point support is rotatably connected by a rotary shaft parallel to the viewing platform with the flight frame, the retractor device is configured to rotate around the rotary shaft by flight frame described in the telescopic drive of straight line, and the fixed point support is fixed on the viewing platform；The retractor device flexible stroke of different time, speed and acceleration during the movie playback are obtained according to the exercise in advance analysis of personnel's different time in the film played, so that during movie playback, the motion simultaneously match of personnel in the motion of the retractor device and film.
Description
Technical field
The present invention relates to viewing equipment, more particularly to a kind of viewing aircraft, the viewing system based on the viewing aircraft,
And the ball curtain viewing arenas based on the viewing system.
Background technology
Since film occurs, motion picture technique is maked rapid progress, and from noiseless to sound, from black and white to color, generated and is turned over
It covers the change on ground.With the innovation of motion picture technique, the main place showed a film is used as --- cinema, its technology is also continuous
Update, panorama movie theatre, three-dimensional movie theatre, palace theatres and ball-type movie theatre etc. arise.
Wherein, ball screen cinema is main is made up of ball-type screen and viewing platform two parts, and existing viewing platform is mostly adopted
With fixed ground or domatic (inclined-plane) watching mode, using this watching mode, because diverse location is relative on viewing platform
Differed in the position of ball curtain and angle, this leverages the effect of viewing experience.
Meanwhile, on the viewing platform of some type movie theatres, various seats can be arranged, in order to produce movement effects, some seats
Chair can even do what is rocked, however, seat limits what viewing mode was necessarily seated in itself, this also to cause seat
Chair its rotational angle when producing movement effects is small range, is severely limited；No matter from rotational angle or transport
Flowing mode, it can not be all met needed for the effect of simulated flight.
The content of the invention
How the technical problem to be solved in the present invention is so that viewing equipment meets the effect of simulated flight.
In order to solve this technical problem, the invention provides a kind of viewing aircraft, on viewing platform, including with
To fix the flight frame, fixed point support and retractor device of viewing people standing place, the fixed point support is by one parallel to institute
The rotary shaft for stating viewing platform is rotatably connected with the flight frame, and the retractor device is configured to by the flexible of straight line
The flight frame is driven to be rotated around the rotary shaft, the fixed point support is fixed on the viewing platform；
The retractor device flexible stroke of different time, speed and acceleration foundation during movie playback are played
Film in the exercise in advance analysis of personnel's different time obtain so that during movie playback, the retractor device
Motion and film in personnel motion simultaneously match.
Optionally, the rotation angle range of the flight frame is at least 0-90 degree.
Optionally, described viewing aircraft also includes runing rest, and the flight frame is fixedly connected with runing rest, institute
Retractor device is stated to rotate around the rotary shaft by runing rest described in the telescopic drive of straight line, so realize the flight frame around
The rotation of the rotary shaft.
Optionally, one end of the retractor device is rotatably connected with the runing rest, the other end and the viewing platform
Rotatable connection, and axis of rotation is each parallel to the viewing platform.
Optionally, one end of the retractor device is rotatably connected with the runing rest, and axis of rotation is parallel to described
Viewing platform；
The retractor device connects the runing rest and the mode of viewing platform is further configured to：
During the retractor device stretching motion, one end of the retractor device is by pushing or pull on the rotation
Turn support to rotate around the rotary shaft, the other end of the retractor device is slided or rolled along the viewing platform.
Optionally, the runing rest is provided with track, and the other end of the retractor device rotates with the viewing platform
Connection, and axis of rotation is parallel to the viewing platform；
The retractor device connects the runing rest and the mode of viewing platform is further configured to：
During the retractor device stretching motion, one end of the retractor device can be slided along the track
Or roll, and drive the runing rest to be revolved around the rotary shaft by pushing or pull on the track in slip or rolling
Turn.
Optionally, the retractor device connects the runing rest and the mode of viewing platform is further configured to：
During the retractor device stretching motion：
When one end of the retractor device is slided or rolled along the track, driven by pushing or pull on the track
The runing rest is moved to rotate around the rotary shaft；
When one end of the retractor device is in head end or the end of the track, by pushing or pull on the track
The runing rest is driven to be rotated around the rotary shaft.
Optionally, a side surface of the runing rest is curved surface, and the track is arranged along the curved surface.
Optionally, the safe fixed mechanism of back of the body formula, the safe fixed mechanism of back of the body formula and institute are also equipped with the flight frame
State and positioning framework is formed after flight bridge joint is closed, the positioning framework from up, down, left, right, before and after direction to be fixed thereon sight
The position of actor or actress.
Optionally, it is also equipped with head-up display on the flight frame.
Optionally, the safe fixed mechanism of back of the body formula is also equipped with the flight frame, the safe fixed mechanism is aobvious with looking squarely
Show that device is located at the positive and negative both sides of the flight frame respectively.
Optionally, the fixed point support is supported in the downside of the flight frame.
Optionally, pedal is also equipped with the flight frame, and position of the pedal on the flight frame is adjustable.
Present invention also offers a kind of viewing system, including Stewart Platform mechanism and the viewing flight described at least one
Device, the Stewart Platform mechanism at least includes all magnificent telecontrol equipment of six axle histories and the viewing platform, the viewing platform by
The all magnificent telecontrol equipment driving lifting of the six axles history, translation are with rotating, and the viewing aircraft is on the viewing platform.
Present invention also offers bulb curtain viewing arenas, including spherical screen and described viewing system, the viewing
System is located in the spherical screen.
Optionally, the spherical screen is configured to when the flight frame rotates, the display picture on the spherical screen
Matching change occurs therewith for the position in face.Invention introduces flight frame, fixed point support and retractor device, replaced using flight frame
Seat so that viewing people can be no longer limited to the viewing that is seated, this causes its rotation for being adapted to larger even full angle
Transhipment is dynamic, on this basis, and the present invention is pinpointed and fulcrum using pinpointing support and is provided for the rotation of flight frame, eventually through stretching
The telescopic action of device drives the flight frame rotation.
Brief description of the drawings
Fig. 1 is the schematic diagram of ball curtain viewing arenas in the embodiment of the present invention 1；
Fig. 2 is the schematic diagram of viewing aircraft in the embodiment of the present invention 1；
Fig. 3 is the schematic diagram of viewing aircraft in the embodiment of the present invention 2；
Fig. 4 is the schematic diagram of viewing aircraft in the embodiment of the present invention 3；
Fig. 5 is the schematic diagram of viewing aircraft in the embodiment of the present invention 4；
Fig. 6 and Fig. 7 are the effect schematic diagrames of the middle orbit of the embodiment of the present invention 1 to 4；
Fig. 8 is the schematic diagram of viewing aircraft in the embodiment of the present invention 5；
The all magnificent telecontrol equipment of the axle histories of 1- six；2- viewing platforms；3- viewing aircraft；31- flight framves；32- retractor devices；
321- rollers；33- pinpoints support；34- runing rests；35- carries on the back the safe fixed mechanism of formula；36- tracks；361- tracks outer ring；
362- track inner rings；363- orbital pass；37- head-up displays；38- mats；39- pedals；The spherical screens of 4-.
Embodiment
Below with reference to Fig. 1 to Fig. 4, the viewing aircraft that is provided by three embodiments the present invention, viewing system and
Ball curtain viewing arenas is described in detail, and it is optional embodiment of the present invention, it is believed that those skilled in the art are not
Change in the range of present invention spirit and content, it can be modified and polished.
The many embodiments of the present invention provide a kind of viewing aircraft 3, on viewing platform 2, refer to Fig. 2 to Fig. 4,
Including the flight frame 31, fixed point support 33 and retractor device 32 to fixed viewing people standing place, the fixed point support 33 leads to
Cross a rotary shaft parallel to the viewing platform 2 to be rotatably connected with the flight frame 31, the retractor device 32 is configured
Into that can be rotated by flight frame 31 described in the telescopic drive of straight line around the rotary shaft, the fixed point support 33 is fixed at institute
State on viewing platform 2.
Invention introduces flight frame 31, fixed point support 33 and retractor device 32, seat is instead of using flight frame 31, is made
The viewing that is seated can be no longer limited to by obtaining viewing people, and this causes its rotary motion for being adapted to larger even full angle,
On the basis of this, present invention utilization pinpoints support 33 and provides fixed point and fulcrum for the rotation of flight frame 31, eventually through retractor device
32 telescopic action drives the flight frame 31 to rotate.
In the present invention, flexible stroke, speed and the acceleration of retractor device different time during movie playback
Exercise in advance analysis according to personnel's different time in the film played is obtained, so that during movie playback, institute
State the motion of retractor device and the motion simultaneously match of personnel in film.This process can generally be protected by being programmed to
The broadcasting of card film is promoted with the control moved under same time shaft according to advance programming.Here to personnel in film
The ex ante analysis of motion, is primarily referred to as moving the motion of key person, in other words leading role, such as fortune of superman in superman's film
Dynamic, the motion chivalrous to steel is analyzed in the chivalrous film of steel, and this analysis can be simulative calculation, according to suffered by personage
Power and real-time attitudes vibration, carry out simulative calculation, are applied to after conversion in the stretching motion of retractor device.
For further, for the film of many leading role's pictures, if such as steel is chivalrous and superman is in same picture, viewing
Personnel even can actively select one of them to realize motion.Certainly, this should also be considered as a kind of improvement on the basis of the present invention.
It should be appreciated that the concrete mode no matter programmed why, as long as being applied to this thinking, its be exactly the present invention make every effort to guarantor
One of scheme of shield, can't introduce during physical simulation different parameter because of it and algorithm just departs from the guarantor of the present invention
Protect scope.
Further, in most embodiment of the invention, described viewing aircraft 3 also includes runing rest 34,
The flight frame 31 is fixedly connected with runing rest 34, and the retractor device 32 passes through runing rest described in the telescopic drive of straight line
34 around rotary shaft rotation, and then realizes rotation of the flight frame 31 around the rotary shaft.
The present invention mainly makes every effort to protect large-scale rotation, for example, at least 0-90 degree, to realize big attitudes vibration, produces example
Such as the extensive change of pitch attitude, rather than the vibrations of low-angle in the prior art, implement therefore, the of the invention and present invention is many
Example has all been done specifically and rich in innovation essence in terms of the part of motion, realization action sync section and personnel's viewing posture is realized
The improvement of god, it has overturned the pattern of the existing viewing that is seated, but is become a kind of viewing mould of comprehensive synchronous experience
Formula.
Embodiment 1
It refer in Fig. 2, the viewing aircraft 3 of the present embodiment, the runing rest 34 is provided with track 36, described flexible
The other end of device 32 is rotatably connected with the viewing platform 2, and axis of rotation is parallel to the viewing platform 2；
The retractor device 32 connects the runing rest 34 and the mode of viewing platform 2 is further configured to：
During the stretching motion of retractor device 32, one end of the retractor device 32 can be along the track
36 slide or roll, and drive the runing rest 34 around described by pushing or pull on the track 36 in slip or rolling
Rotary shaft rotates.
How relevant track 36 works, and refer to Fig. 6 and Fig. 7, and this gives a kind of feasible program, embodiment
2 to 4 also admissible such a schemes, form the space rolled for roller 321, this is between track inner ring 362 and track outer ring 361
For orbital pass 363, only illustrated with direction in scheming, as retractor device 32 is flexible, track outer ring can be promoted on 321 pairs of roller
361, the lower stretchy track inner ring 362 of 321 pairs of roller, so that by promoting and pulling track 36 to realize the drawing to runing rest 34
Dynamic and promotion.
Fig. 2 is refer to, the retractor device 32 connects the runing rest 34 and the mode of viewing platform 2 is further matched somebody with somebody
It is set to：
During the retractor device stretching motion：
When one end of the retractor device 32 is slided or rolled along the track 36, by pushing or pull on the rail
Road 36 drives the runing rest to be rotated around the rotary shaft；
It is described by pushing or pull on when one end of the retractor device 32 is in head end or the end of the track 36
Track 36 drives the runing rest 34 to be rotated around the rotary shaft.Specifically, in figure, track 36 is that have beginning and end
, in the present embodiment, when one end row to the beginning and end of retractor device, there is not track stroke, be now further continued for lifting,
Because retractor device is rotatably connected with viewing platform 2, the rotation of runing rest still can be pushed or pull on.
In the present embodiment, a side surface of the runing rest 34 is curved surface, and the track is arranged along the curved surface.This
It is curve to mean that the present embodiment middle orbit, and the effect of this curve is make it that the angle of rotation, fluctuating may be more
Sample, gives more real viewing experience, the axle center of each camber line of the curved surface should be parallel to the rotary shaft, the present embodiment
Which kind of curve is not limited is, every to have used curve to be exactly one of details arrangement of the present embodiment scheme described herein,
This arrangement is entirely that those skilled in the art can implement according to effects of demand.
Embodiment 2
Fig. 3 is refer to, the present embodiment and the main distinction of embodiment 1 are：In the present embodiment, the track is straight line rail
Road.It can be seen that, no matter the surface configuration of runing rest 34 why, the shape of deployment rails is why thereon, be all the present invention make every effort to guarantor
One of scheme of shield, according to the demand of different rotates effes, it may occur to persons skilled in the art that further how to go arrangement
The shape of track, in other words, the part of this in present invention thing is introduced in itself by track, especially transports the straight line of itself and retractor device 2
It is dynamic to be combined, so as to realize rotation, answer right and wrong it will be apparent that its absolutely not and those skilled in the art's foundation prior art can be with
Expect.
Embodiment 3
Fig. 4 is refer to, the present embodiment and the main distinction of embodiment 1 are：In the present embodiment, the retractor device 32
One end is rotatably connected with the runing rest 34, and axis of rotation is parallel to the viewing platform 2；
The retractor device 32 connects the runing rest and the mode of viewing platform is further configured to：
During the retractor device stretching motion, one end of the retractor device 32 is described by pushing or pull on
Runing rest 34 is rotated around the rotary shaft, and the other end of the retractor device 32 is slided or rolled along the viewing platform 2.
In other words, Examples 1 and 2, using the tie point of retractor device 32 and runing rest 34 as dynamic point, the present embodiment is then
It is as fixed point, to regard the tie point of itself and viewing platform 2 as dynamic point using its tie point with runing rest 34.Further,
Can on viewing platform 2 deployment rails (not shown), to guide the slip or rolling at the end of retractor device 32.
In addition to above description, three above embodiment, and most of embodiments of the invention also have following arrangement：
It refer to Fig. 2 to Fig. 4, flight frame 31 is rotated in several embodiments, at least 0-90 degree, by each portion
The further design of part size and dimension, for example, increase the length of fixed point support 33, increase the upper rail of viewing platform 2 in embodiment 3
The length in road, changes shape of Examples 1 and 2 middle orbit etc., even the structure of three above embodiment signal, also completely
The rotation of 0-180 degree scopes, even 0-360 degree can be realized.
Fig. 2 be refer to Fig. 4, the safe fixed mechanism 35 of back of the body formula, the back of the body formula safety are also equipped with the flight frame 31
Fixed mechanism 35 forms positioning framework after being engaged with the flight frame 31, the positioning framework be used to from upper and lower, left and right, it is preceding,
Rear is to the position for being fixed thereon viewing people.Flight simulation is realized because the present invention is put forth effort on, the demand of its anglec of rotation can reach
To 360 degree, this, which means that, needs to provide safeguard protection for each orientation, carries out position and fixes.
Head-up display 37 (Head Up Display), the head-up display 37 (Head are also equipped with the flight frame
Up Display), abbreviation HUD, to show consulting, provides viewing experience together with screen, for example, it is well known that
In the chivalrous film of steel, leading role is in the armor it can be seen that the floating picture of a display data, the head-up display 37 just can be with
To show that these data are seeked advice from.The safe fixed mechanism is located at positive and negative the two of the flight frame respectively with head-up display
Side.When in use, viewing person lies prone on flight frame 31, and front can see the picture on head-up display 37, and the back side is by back of the body formula
Safe fixed mechanism 35 is protected.
The fixed point support 33 is supported in the downside of the flight frame 31.
Pedal 39 is also equipped with the flight frame 31, and position of the pedal 39 on the flight frame 31 is adjustable.
With the different demands for the height for adapting to different people.
Embodiment 4
Fig. 7 is refer to, the present embodiment is the further configuration of embodiment 1, is essentially consisted in：The formation of track 36 one is ellipse
Round ring-type, using the stretching motion of retractor device 2, the rotation angle range that can cause the flight frame is 0-360 degree.When
So, however it is not limited to oval shape, in order to realize the rotation of 360 degree of scopes, the shape of track 36 can be configured specifically, and
It is not limited to shown in Fig. 5.
Embodiment 5
It refer to Fig. 8
The difference of the present embodiment and above example is essentially consisted in：One end of the retractor device 32 and the runing rest
34 rotatable connections, the other end is rotatably connected with the viewing platform 2, and axis of rotation is each parallel to the viewing platform 2.Stretch
The two ends of compression apparatus 32 are respectively relative to runing rest 34 and the position of viewing platform 2 is fixed.Further, in the present embodiment,
360 degree of rotation can be realized on this basis.
Based on the viewing aircraft in similar 5 embodiments above, present invention also offers a kind of viewing system and ball curtain
Viewing arenas.By taking embodiment 1 as an example, Fig. 1 is refer to, it provides a kind of viewing system, including Stewart Platform mechanism and extremely
Viewing aircraft 3 described in few one, the Stewart Platform mechanism at least includes all magnificent telecontrol equipment 1 of six axle histories and the sight
Shadow platform 2, the viewing platform 2 drives lifting, translation with rotating by all magnificent telecontrol equipment 1 of the six axles history, and the viewing flies
Row device 3 is on the viewing platform 2.Further, bulb curtain viewing arenas, including spherical screen 4 and institute are additionally provided
The viewing system stated, the viewing system is located in the spherical screen 4.
The spherical screen 4 may be configured to when the flight frame rotates, the display picture on the spherical screen 4
Position occur therewith matching change.
In summary from the point of view of technical scheme, when designing spherical screen 4, viewing platform assumes that being designed as 4 meters multiplies 4 meters of square
Size, carries 38 to 10, viewing aircraft, the visual field that viewing person views and admires is concentrated mainly on optimal vision area above, and its visual angle is 10
Degree, 10-20 degree is instantaneous vision area (it can be seen that object in the short time) in addition, and 20-30 degree is that (know has thing to exist to dynamic vision area
It is dynamic), can be provided close to using spherical screen or cover the full visual field view and admire impression, view and admire feeling of immersion for increasing and have larger effect
Really.The rotation maximum angle (level, vertical) of the viewing platform of the present invention is about 20 degree, thus the spherical screen visual field we be scheduled on
110-120 degree can meet this requirement.Separately due to reducing the constriction viewed and admired, ball curtain views and admires distance and is not less than 4 meters, in the present invention
6 meters are positioned in many embodiments can look after passenger by platform.
During viewing person's standing position, visual angle is 0 degree of level, and about -15 degree during prostrate, human eye vertical visual field good area is 30 degree,
Therefore determine that the ball curtain visual field can obtain the property of at least 30 degree vertical visual fields when+35 to -45 spend to cover standing position and prostrate state certainly
Energy.
It can be seen that, ball curtain is changed using visual field when specification foundation visually-perceptible scope, platform rotating property, prostrate and standing position
To determine that ball curtain distance, ball curtain radius of curvature, horizontal view angle determine ball curtain width, vertical angle of view determines ball curtain height.
In order to provide parameter to viewing platform 2 and retractor device 32, it can be realized according to following algorithm：
Motion Cueing algorithms：The algorithm be typically used in flight simulation, this kind of simulator of racing simulation it
With.By passenger in Virtual Space to the power (acceleration) being subject to for moving (flight), using the translation of platform, rotate come mould
Intend producing.For this theater, Moviemaking company is outer in itself except the film for making broadcasting, additionally needs and provides in film
In, the kinematic parameter at leading role visual angle is supplied to motion commissioning staff to take exercises analysis, and then to six axle histories all China's telecontrol equipments
Action carries out calculating conversion.
About the rotation of viewing aircraft, there is provided include meter to motion commissioning staff for the attitude parameter of leading role in itself of still needing
Calculate conversion.
In summary, invention introduces flight frame, fixed point support and retractor device, seat is instead of using flight frame,
Viewing people is allowd to be no longer limited to the viewing that is seated, this causes its rotary motion for being adapted to larger even full angle,
On this basis, present invention utilization pinpoints support and provides fixed point and fulcrum for the rotation of flight frame, eventually through retractor device
Telescopic action drives the flight frame rotation.
Claims (15)
1. a kind of viewing aircraft, on viewing platform, it is characterised in that：Including flying to fixed viewing people standing place
Row frame, fixed point support and retractor device, the fixed point support by a rotary shaft parallel to the viewing platform with it is described
Flight frame is rotatably connected, and the retractor device is configured to by flight frame described in the telescopic drive of straight line around the rotation
Axle is rotated, and the fixed point support is fixed on the viewing platform；
The retractor device shadow that the flexible stroke of different time, speed and acceleration foundation are played during movie playback
The exercise in advance analysis of personnel's different time is obtained in piece, so that during movie playback, the fortune of the retractor device
The dynamic motion simultaneously match with personnel in film,
The safe fixed mechanism of back of the body formula is also equipped with the flight frame, the safe fixed mechanism of back of the body formula is closed with the flight bridge joint
After form positioning framework, the positioning framework is used to the position that viewing people is fixed thereon from up, down, left, right, before and after direction.
2. viewing aircraft as claimed in claim 1, it is characterised in that：The rotation angle range of the flight frame is at least 0-
90 degree.
3. viewing aircraft as claimed in claim 1, it is characterised in that：Also include runing rest, the flight frame and rotation
Support is fixedly connected, and the retractor device is rotated by runing rest described in the telescopic drive of straight line around the rotary shaft, and then
Realize rotation of the flight frame around the rotary shaft.
4. viewing aircraft as claimed in claim 3, it is characterised in that：One end of the retractor device and the runing rest
Rotatable connection, the other end is rotatably connected with the viewing platform, and axis of rotation is each parallel to the viewing platform.
5. viewing aircraft as claimed in claim 3, it is characterised in that：One end of the retractor device and the runing rest
Rotatable connection, and axis of rotation is parallel to the viewing platform；
The retractor device connects the runing rest and the mode of viewing platform is further configured to：
During the retractor device stretching motion, one end of the retractor device is by pushing or pull on the rotation branch
Frame is rotated around the rotary shaft, and the other end of the retractor device is slided or rolled along the viewing platform.
6. viewing aircraft as claimed in claim 3, it is characterised in that：The runing rest is provided with track, described flexible
The other end of device is rotatably connected with the viewing platform, and axis of rotation is parallel to the viewing platform；
The retractor device connects the runing rest and the mode of viewing platform is further configured to：
During the retractor device stretching motion, one end of the retractor device can be slided or roll along the track
It is dynamic, and drive the runing rest to be rotated around the rotary shaft by pushing or pull on the track in slip or rolling.
7. viewing aircraft as claimed in claim 6, it is characterised in that：The retractor device connects the runing rest and sight
The mode of shadow platform is further configured to：
During the retractor device stretching motion：
When one end of the retractor device is slided or rolled along the track, institute is driven by pushing or pull on the track
Runing rest is stated to rotate around the rotary shaft；
When one end of the retractor device is in head end or the end of the track, driven by pushing or pull on the track
The runing rest rotates around the rotary shaft.
8. viewing aircraft as claimed in claim 6, it is characterised in that：One side surface of the runing rest is curved surface, institute
Track is stated to arrange along the curved surface.
9. viewing aircraft as claimed in claim 1, it is characterised in that：Head-up display is also equipped with the flight frame.
10. viewing aircraft as claimed in claim 9, it is characterised in that：Back of the body formula is also equipped with the flight frame solid safely
Determine mechanism, the safe fixed mechanism is located at the positive and negative both sides of the flight frame with head-up display respectively.
11. viewing aircraft as claimed in claim 1, it is characterised in that：The fixed point support is supported in the flight frame
Downside.
12. viewing aircraft as claimed in claim 1, it is characterised in that：Pedal is also equipped with the flight frame, and it is described
Position of the pedal on the flight frame is adjustable.
13. a kind of viewing system, it is characterised in that：Including Stewart Platform mechanism and at least one such as claim 1 to 12 times
Viewing aircraft described in one of meaning, the Stewart Platform mechanism at least includes all magnificent telecontrol equipment of six axle histories and the viewing
Platform, the viewing platform is by all magnificent telecontrol equipment driving lifting of the six axles history, translation with rotating, and the viewing aircraft is set
In on the viewing platform.
14. bulb curtain viewing arenas, it is characterised in that：Including spherical screen and at least one sight as claimed in claim 13
Shadow system, the viewing system is located in the spherical screen.
15. ball curtain viewing arenas as claimed in claim 14, it is characterised in that：The spherical screen is configured to fly when described
When row frame rotates, matching change occurs therewith for the position of the display picture on the spherical screen.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510362931.0A CN104912352B (en) | 2015-06-25 | 2015-06-25 | Viewing aircraft, viewing system and ball curtain viewing arenas |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510362931.0A CN104912352B (en) | 2015-06-25 | 2015-06-25 | Viewing aircraft, viewing system and ball curtain viewing arenas |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104912352A CN104912352A (en) | 2015-09-16 |
| CN104912352B true CN104912352B (en) | 2017-08-08 |
Family
ID=54081748
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510362931.0A Active CN104912352B (en) | 2015-06-25 | 2015-06-25 | Viewing aircraft, viewing system and ball curtain viewing arenas |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104912352B (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102016107239A1 (en) * | 2016-04-19 | 2017-10-19 | Simtec Systems Gmbh | ride |
| CN105797407A (en) * | 2016-05-11 | 2016-07-27 | 大连博跃科技发展有限公司 | Dynamic standing armchair |
| CN106353961A (en) * | 2016-11-14 | 2017-01-25 | 墨宝股份有限公司 | VR experience device, spherical simulator and audio-visual system thereof |
| CN110085088B (en) * | 2019-06-05 | 2021-01-26 | 南京奔联软件科技有限公司 | Small airplane riding simulation detection system for airport |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204754340U (en) * | 2015-06-25 | 2015-11-11 | 新字多媒体技术开发（上海）有限公司 | See shadow aircraft, see shadow system and ball curtain sight film and drama field |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2332451Y (en) * | 1998-04-02 | 1999-08-11 | 刘敬平 | Six-freedom dynamic compound simulated sports appts. |
| US6354954B1 (en) * | 2000-12-28 | 2002-03-12 | Disney Enterprises, Inc. | Amusement apparatus and method |
| CN102151411A (en) * | 2011-03-17 | 2011-08-17 | 深圳市一品红文化传播有限公司 | Autokinetic seat for 4D cinema |
| CN102728075B (en) * | 2012-05-23 | 2014-08-27 | 宁波新文三维股份有限公司 | Flying cinema device |
| CN203160750U (en) * | 2013-04-24 | 2013-08-28 | 山东华夏集团有限公司 | Aerial three-dimensional dynamic movie theatre |
| CN203914087U (en) * | 2014-06-26 | 2014-11-05 | 湛江创宇影视设备有限公司 | A kind of dynamic cinema seat system |
| CN204093054U (en) * | 2014-09-18 | 2015-01-14 | 江苏卡罗卡国际动漫城有限公司 | The multidimensional seat of ball screen cinema |
-
2015
- 2015-06-25 CN CN201510362931.0A patent/CN104912352B/en active Active
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204754340U (en) * | 2015-06-25 | 2015-11-11 | 新字多媒体技术开发（上海）有限公司 | See shadow aircraft, see shadow system and ball curtain sight film and drama field |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104912352A (en) | 2015-09-16 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104912352B (en) | Viewing aircraft, viewing system and ball curtain viewing arenas | |
| CN103711335B (en) | A kind of comprehensive dynamic tracking viewing system | |
| EP2821116A1 (en) | Attraction for amusement rides based on motion simulation | |
| CN101252974A (en) | Free fall simulator which can display a simulated visual environment | |
| KR20120114289A (en) | A motion-based attraction with image display assembly | |
| CN204352564U (en) | Circle in the air cinema system platform | |
| CN101121075B (en) | Action simulating equipment, system and method for entertainment | |
| WO2016123833A1 (en) | Circulating dynamic vehicle viewing system | |
| CN102296840B (en) | Watching platform in dome cinema | |
| CN204754340U (en) | See shadow aircraft, see shadow system and ball curtain sight film and drama field | |
| CN106003149B (en) | A kind of bad weather electric power Detecting Robot hides device | |
| CN204691322U (en) | Rotating viewing aircraft | |
| CN109350975B (en) | Multi-degree-of-freedom air diving type flight cinema | |
| CN209848334U (en) | Dynamic seat capable of measuring heart rate | |
| CN204691324U (en) | The viewing aircraft of ball curtain viewing arenas | |
| CN204798865U (en) | Dispose sight shadow rotary platform who sees shadow aircraft | |
| CN211462079U (en) | Dynamic system of panoramic cinema and panoramic cinema | |
| CN209855308U (en) | Flight cinema system | |
| CN207871511U (en) | Rotate machine and the machine cinema experience system of jumping out of the building of jumping out of the building | |
| CN209286681U (en) | A kind of flight movie theatre for overlooking flight instruments in the air equipped with multiple degrees of freedom | |
| CN105041006B (en) | Viewing turntable, viewing system and ball curtain viewing arenas | |
| CN209237353U (en) | The guarantee door machine structure of 4D movie theatre viewing platform | |
| CN108126349A (en) | Rotate machine and the machine cinema experience system of jumping out of the building of jumping out of the building | |
| US20190111351A1 (en) | Kinesthetic device with different seating orientations | |
| CN106466531B (en) | A kind of crossings on different level dynamic viewing system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |