CN219539436U - Matrix type flight cinema - Google Patents
Matrix type flight cinema Download PDFInfo
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- CN219539436U CN219539436U CN202320503949.8U CN202320503949U CN219539436U CN 219539436 U CN219539436 U CN 219539436U CN 202320503949 U CN202320503949 U CN 202320503949U CN 219539436 U CN219539436 U CN 219539436U
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- matrix
- revolving body
- flight cinema
- seat
- rotating mechanism
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
The utility model relates to the field of amusement equipment and discloses a matrix type flight cinema which comprises a supporting platform, wherein the supporting platform is of a stepped structure and at least comprises one layer of steps; the mechanical arm type dynamic unit is arranged on each layer of stairs of the supporting platform and distributed in a matrix, and specifically comprises a base frame assembly, a revolving body and a multi-axis rotating mechanism, wherein the revolving body is arranged on the base frame assembly, the multi-axis rotating mechanism is connected with the revolving body, the tail end of the multi-axis rotating mechanism is connected with a seat assembly, and the revolving body is matched with the multi-axis rotating mechanism to drive the seat assembly to move in six degrees of freedom; the ball curtain is arranged on the step at the lowest layer of the supporting platform and is positioned in front of the mechanical arm type dynamic unit. According to the utility model, each mechanical arm dynamic unit can realize six-degree-of-freedom motion, realize large-amplitude flying motion in the air, bring stimulated immersive flying experience to the audience, and is suitable for various fields, large in motion amplitude, high in precision, small in fault influence, low in cost and convenient to install and maintain.
Description
Technical Field
The utility model relates to the field of amusement equipment, in particular to a matrix type flight cinema.
Background
The flight cinema is a large suspended spherical cinema, and is combined with a dynamic seat without boundary film and television pictures, so that a spectator can feel the feeling of being in the scene. However, the main stream equipment of the existing flight cinema mainly comprises 8-person or 10-person seats with 3 degrees of freedom and 6 degrees of freedom, the combination form is single, the action amplitude is small, and the effect of watching the film is relatively poor.
In order to solve the problems, the matrix type flight cinema with the parallel multi-mechanical arms is provided, the actions of the matrix type flight cinema are uniform, the combination forms are various, the action range is large, and the immersive flight experience of stimulation can be brought to audiences.
Disclosure of Invention
Aiming at the existing problems, the utility model provides a matrix type flight cinema which can effectively solve the problems in the background technology.
In order to solve the problems, the utility model adopts the following technical scheme:
a matrix flight cinema comprising
The support platform is of a stepped structure and is provided with at least one layer of steps;
the mechanical arm type dynamic unit is arranged on each layer of stairs of the supporting platform and distributed in a matrix, and comprises a base frame assembly, a revolving body and a multi-axis rotating mechanism, wherein the revolving body is arranged on the base frame assembly, the head end of the multi-axis rotating mechanism is connected with the revolving body, the tail end of the multi-axis rotating mechanism is connected with a seat assembly, and the revolving body is matched with the multi-axis rotating mechanism to drive the seat assembly to move in six degrees of freedom;
and the ball curtain is arranged on the step at the lowest layer of the supporting platform and is positioned in front of the mechanical arm type dynamic unit.
As still further aspects of the utility model: the revolving body comprises a fixed part fixedly connected with the base frame assembly and a rotating part horizontally rotating relative to the fixed part, a first servo motor is installed on the rotating part, and the servo motor drives the rotating part to horizontally rotate relative to the fixed part.
As still further aspects of the utility model: the multi-axis rotating mechanism comprises a large arm, a small arm, a straight wrist, a wrist shaft and a tail end revolving body, one end of the large arm is rotatably mounted on the rotating part through a second servo motor, one end of the small arm is rotatably mounted on the other end of the large arm through a third servo motor, the straight wrist is mounted on the other end of the small arm, the straight wrist is connected with the tail end revolving body through the wrist shaft, and the tail end revolving body is fixedly connected with the seat assembly.
As still further aspects of the utility model: and the forearm is provided with three groups of servo motors IV, and the servo motors IV drive the straight wrist, the wrist shaft and the tail end revolving body to realize triaxial rotation.
As still further aspects of the utility model: the big arm is connected with the rotating part in a rotating way through a balancing device.
As still further aspects of the utility model: the balancing device is a telescopic cylinder.
As still further aspects of the utility model: the seat assembly comprises a seat frame, a protection frame is rotatably arranged at the top of a backrest of the seat frame, and safety belts corresponding to the protection frames one by one are arranged on the seat frame.
As still further aspects of the utility model: sensors are arranged on two sides of the seat frame.
As still further aspects of the utility model: the sensor is a proximity sensor.
As still further aspects of the utility model: the ball curtain is of a hemispherical structure, the screen of the ball curtain faces the seat assembly, and the bottom of the ball curtain is arranged on the supporting platform through the stand.
Compared with the prior art, the utility model has the beneficial effects that: according to the utility model, the independently controlled mechanical arm type dynamic units are arranged on the steps of the supporting platform, so that the mechanical arm type dynamic units can be distributed randomly according to design requirements, and are matched with the ball curtains, and the seat components on the mechanical arm type dynamic units are arranged in parallel in an electric control mode to realize synchronous motion; the mechanical arm type dynamic unit is applicable to various fields, has smaller overall dimension, can be arranged randomly according to requirements, and can be more or less so as to adapt to different fields; the mechanical arm is mainly controlled by the rotary driver, and can complete the action with large amplitude and high precision; the influence of the faults is small, and when the mechanical arm type dynamic unit breaks down, the operation of the whole equipment is not influenced; the cost is low, the production, assembly, transportation, installation and other costs of the mechanical arm type dynamic seat unit are low, and the installation and debugging cost of the whole device is also low; the mechanical arm type dynamic seat unit is convenient to install and maintain, and is easy to maintain due to small body weight.
Drawings
FIG. 1 is a perspective view of an overall structure of a matrix type flight cinema;
fig. 2 is a schematic diagram of a mechanical arm type dynamic unit structure in a matrix type flight cinema;
FIG. 3 is a schematic illustration of a seat assembly configuration in a matrix flight cinema;
FIG. 4 is a top view of the overall structure of a matrix-type flight cinema;
fig. 5 is a side view of the overall structure of a matrix-type flight cinema.
In the figure: 1. a support platform; 2. a base frame assembly; 3. a revolving body; 31. a fixing part; 32. a rotating part; 4. a balancing device; 5. a servo motor I; 6. a servo motor II; 7. a large arm; 8. a servo motor IV; 9. a servo motor III; 10. a forearm; 11. a straight wrist; 12. a wrist axis; 13. a terminal rotator; 14. a seat assembly; 141. a seat frame; 142. a protective frame; 143. a safety belt; 144. a sensor; 15. a ball curtain; 16. and (5) a vertical frame.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
In this embodiment, the present embodiment is described with reference to fig. 1 to 5, and this embodiment provides a matrix type flight cinema, including supporting platform 1, one end of supporting platform 1 is equipped with two-layer ladder, be equipped with three mechanical arm formula dynamic units on each ladder of supporting platform 1, and six mechanical arm formula dynamic units are matrix distribution, mechanical arm dynamic units includes base frame assembly 2, solid of revolution 3 and multiaxis slewing mechanism, solid of revolution 3 is installed on base frame assembly 2, multiaxis slewing mechanism's head end is connected with solid of revolution 3, multiaxis slewing mechanism's end is connected with seat assembly 14, solid of revolution cooperation multiaxis slewing mechanism drives seat assembly 14 six degrees of freedom motion, install grudging post 16 at supporting platform 1's other end, install ball curtain 15 on grudging post 16, ball curtain 15 is hemisphere structure and screen orientation seat assembly 14, every mechanical arm dynamic unit all can realize six degrees of freedom motion, and a plurality of mechanical arm dynamic units parallel synchronous operation, cooperate ball curtain 15 and, realize aerial movement by a wide margin, the action is unified, the combination form is various, the action range is big, can bring the stimulated various modes of flight, the effect is applicable to various places, the high-level, the maintenance is easy to install, the film has low cost, the maintenance is convenient.
As shown in fig. 2, the revolving body 3 includes a fixed portion 31 fixedly connected with the base frame assembly 2 and a rotating portion 32 horizontally rotating relative to the fixed portion 31, a first servo motor 5 is installed on the rotating portion 32, the first servo motor 5 drives the rotating portion 32 to horizontally rotate relative to the fixed portion 31, the first servo motor 5 realizes 1-axis rotation, the multi-axis rotation mechanism includes a large arm 7, a small arm 10, a straight wrist 11, a wrist shaft 12 and a terminal revolving body 13, one end of the large arm 7 is rotatably installed on the rotating portion 32 through a second servo motor 6, one end of the small arm 10 is rotatably installed on the other end of the large arm 7 through a third servo motor 9, the straight wrist 11 is installed on the other end of the small arm 10, the straight wrist 11 is connected with the terminal revolving body 13 through a wrist shaft 12, the terminal revolving body 13 is fixedly connected with the seat assembly 14, the second servo motor 6 and the third servo motor 9 realize 2-axis and 3-axis rotation, and three groups of servo motors four 8 are installed on the small arm 10, the fourth servo motor 8 drives the straight 11, the wrist shaft 12 and the terminal revolving body 13 realize three-axis rotation, the fourth servo motor 8 realizes 4-axis rotation, 5-axis rotation and 6-axis rotation, and the detailed structure of the conventional structure is not described. The big arm 7 is rotationally connected with the rotating part 32 through the balancing device 4, and the balancing device 4 is a telescopic cylinder, and the stability of the big arm 7 during rotation is guaranteed through the balancing device 4.
As shown in fig. 3, the seat assembly 14 includes a seat frame 141, a protection frame 142 is rotatably installed at the top of the backrest of the seat frame 141, and safety belts 143 corresponding to the protection frames 142 one by one are installed on the seat frame 141, so that the protection frames 142 and the safety belts 143 play a double-layer protection role on tourists, the potential safety hazards that the tourists break away from in the experience process are avoided, and the safety in the experience process is ensured. And the sensors 144 are arranged on two sides of the seat frame 141, the sensors 144 are proximity sensors, and when the actions are asynchronous and have collision danger, signals can be transmitted to the central control to immediately stop the actions, so that the safety performance is further improved.
The working principle of the utility model is as follows: the independent control mechanical arm type dynamic units are arranged on the steps of the supporting platform 1, the independent control mechanical arm type dynamic units can be distributed randomly according to design requirements, the seat assemblies 14 on the mechanical arm type dynamic units are arranged in parallel in an electric control mode to realize synchronous motion, when a film is played on the ball curtain 15, the mechanical arm type dynamic units simultaneously receive film action code signals and synchronously move together in cooperation with the film, and when 360-degree rotation is experienced, vision moves together along with kinesthesia, so that the experience of being personally on the scene is achieved; the mechanical arm type dynamic unit is applicable to various fields, has smaller overall dimension, can be arranged randomly according to requirements, and can be more or less so as to adapt to different fields; the mechanical arm is mainly controlled by the rotary driver, and can complete the action with large amplitude and high precision; the influence of the faults is small, and when the mechanical arm type dynamic unit breaks down, the operation of the whole equipment is not influenced; the cost is low, the production, assembly, transportation, installation and other costs of the mechanical arm type dynamic seat unit are low, and the installation and debugging cost of the whole device is also low; the mechanical arm type dynamic seat unit is convenient to install and maintain, and is easy to maintain due to small body weight.
It is noted that relational terms such as first and second, and the like, are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions, and further, that the terms "comprise," "include," or any other variation thereof, are intended to cover a non-exclusive inclusion such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements, but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (10)
1. A matrix flight cinema, comprising:
the support platform is of a stepped structure and is provided with at least one layer of steps;
the mechanical arm type dynamic unit is arranged on each layer of stairs of the supporting platform and distributed in a matrix, and comprises a base frame assembly, a revolving body and a multi-axis rotating mechanism, wherein the revolving body is arranged on the base frame assembly, the head end of the multi-axis rotating mechanism is connected with the revolving body, the tail end of the multi-axis rotating mechanism is connected with a seat assembly, and the revolving body is matched with the multi-axis rotating mechanism to drive the seat assembly to move in six degrees of freedom;
and the ball curtain is arranged on the step at the lowest layer of the supporting platform and is positioned in front of the mechanical arm type dynamic unit.
2. The matrix flight cinema of claim 1, wherein the revolving body comprises a fixed part fixedly connected with the base frame assembly and a rotating part horizontally rotating relative to the fixed part, the rotating part is provided with a first servo motor, and the servo motor drives the rotating part to horizontally rotate relative to the fixed part.
3. The matrix flight cinema of claim 2 wherein the multi-axis rotation mechanism comprises a large arm, a small arm, a straight wrist, a wrist shaft and a terminal rotator, wherein one end of the large arm is rotatably mounted on the rotation part through a second servo motor, one end of the small arm is rotatably mounted on the other end of the large arm through a third servo motor, the straight wrist is mounted on the other end of the small arm, the straight wrist is connected with the terminal rotator through the wrist shaft, and the terminal rotator is fixedly connected with the seat assembly.
4. A matrix flight cinema according to claim 3 in which three groups of servo motors four are mounted on the small arm, and the servo motors four drive the straight wrist, wrist shaft and end rotator to realize three-axis rotation.
5. A matrix flight cinema according to claim 3 in which the boom is rotatably connected to the swivel by a balancing device.
6. The matrix flight cinema of claim 5 wherein the balancing means is a telescopic cylinder.
7. The matrix flight cinema of claim 1 wherein the seat assembly comprises a seat frame having a guard frame rotatably mounted on a top of a backrest of the seat frame and a seat belt mounted on the seat frame in one-to-one correspondence with the guard frame.
8. The matrix flight cinema of claim 7 wherein the seat frame is provided with sensors on both sides.
9. The matrix flight cinema of claim 8 wherein the sensor is a proximity sensor.
10. The matrix flight cinema of claim 1 wherein the spherical screen is of hemispherical construction and the screen of the spherical screen faces the seat assembly, the bottom of the spherical screen being mounted on the support platform by a stand.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202320503949.8U CN219539436U (en) | 2023-03-15 | 2023-03-15 | Matrix type flight cinema |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN202320503949.8U CN219539436U (en) | 2023-03-15 | 2023-03-15 | Matrix type flight cinema |
Publications (1)
Publication Number | Publication Date |
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CN219539436U true CN219539436U (en) | 2023-08-18 |
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CN202320503949.8U Active CN219539436U (en) | 2023-03-15 | 2023-03-15 | Matrix type flight cinema |
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- 2023-03-15 CN CN202320503949.8U patent/CN219539436U/en active Active
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