Cabin and entertainment system

Abstract

Disclosed in the present invention are a cabin and an entertainment system. The cabin comprises a plurality of assembling components, the plurality of assembling components being assembled to form a enclosed seating cavity and a communication port communicated with the seating cavity, and the shapes of the assembling components being triangular. The technical solution of the present invention can reduce the manufacturing cost of cabins, and provides a structural foundation for users to assemble cabins, thus cultivating hands-on skills of users and enhancing interestingness, and further improving the use experience of users.

Description

Cockpit and entertainment systems Technical Field

[0001] The present invention relates to the technical field of cockpits, and in particular to a cockpit and an entertainment system using the cockpit. Background Art

[0002] Currently, cabins in related technologies are typically designed to be relatively large, requiring the use of correspondingly large molds during manufacturing. Large molds with complex structures can shorten their lifespans and increase costs, leading to relatively high cabin manufacturing costs.

[0003] Summary of the Invention

[0004] The main purpose of the present invention is to provide a cockpit, aiming to reduce the manufacturing cost of the cockpit.

[0005] To achieve the above objectives, the cabin proposed in the present invention includes a plurality of splicing components, which are spliced ​​together to form a seating cavity and a connecting port connecting the seating cavity, and each of the splicing components is triangular in shape.

[0006] Optionally, each of the splicing components is in the shape of an isosceles triangle, and each of the splicing components is equal in size.

[0007] Optionally, each of the splicing components is in the shape of an equilateral triangle.

[0008] Optionally, some of the splicing components are enclosed to form a conical structure with an open end, and the conical structure is formed by enclosing 4-6 of the splicing components.

[0009] Optionally, part of the splicing components encloses to form an annular structure with openings at both ends, and one end of the annular structure is connected to the end of the cone structure with the opening;

[0010] The annular structure and the conical structure enclose the seating chamber, and one end of the annular structure away from the conical structure encloses the communicating port.

[0011] Optionally, the number of splicing components in the conical structure is defined as X, and the number of splicing components in the annular structure is defined as Y, satisfying the relationship: Y=2X.

[0012] Optionally, the cabin includes a plurality of the conical structures, and any of the conical structures is formed by splicing and enclosing the same number of splicing components; or,

[0013] At least two of the conical structures are formed by splicing and enclosing different numbers of splicing components.

[0014] Optionally, adjacent corners of a plurality of the splicing components are connected.

[0015] Optionally, the position where the corners of the adjacent multiple splicing components are close to each other is defined as a connection point, and the cabin further includes multiple connecting parts, each of which is provided at one of the connections and connects the corners of the multiple splicing components in the connection point.

[0016] Optionally, the connecting member includes:

[0017] body panels; and

[0018] The connecting plate is a flat plate. There are multiple connecting plates, all of which are connected to the edge of the main body. Each corner of the splicing assembly at the connection is connected to a corresponding connecting plate.

[0019] Optionally, the adjacent corners of the plurality of splicing components are spaced apart so that the main body plate is exposed to the outside, and the main body plate is an outwardly convex arc-shaped plate.

[0020] Optionally, the cabin further comprises a plurality of filling pieces, each of the filling pieces being arranged on the inner side of a main body plate of the connecting piece, and a side of the filling piece facing away from the main body plate is a plane.

[0021] Optionally, the connecting plate extends into the corner of the corresponding splicing component;

[0022] And / or, the connecting plate and the corners of the splicing assembly are connected by screws;

[0023] And / or, the connecting member further includes a plurality of first reinforcing plates, each of the first reinforcing plates connects the main body plate and two adjacent connecting plates, and the first reinforcing plates are outwardly convex arc-shaped plates.

[0024] Optionally, the splicing assembly includes a mounting plate and a sound absorbing block, and the sound absorbing block is arranged on the inner side of the mounting plate;

[0025] A loudspeaker is provided on a side of at least one of the mounting plates facing the sound absorbing block, and an avoidance hole is provided on the sound absorbing block at a position corresponding to the loudspeaker.

[0026] Optionally, the splicing assembly further includes a protective net, which is arranged on a side of the sound absorbing block facing away from the mounting plate.

[0027] Optionally, the splicing assembly further includes a second reinforcing plate, which is arranged on a side of the mounting plate away from the sound absorbing block.

[0028] Optionally, the splicing assembly further includes a decorative cover, which is provided on a side of the second reinforcing plate facing away from the mounting plate.

[0029] Optionally, the cabin is defined to have an up-down direction and a horizontal direction, and the communication port is arranged to be inclined upward;

[0030] The cockpit further includes a supporting structure, which is arranged on the lower surface of the splicing assembly located at the bottom, and the lower surface of the supporting structure is a plane.

[0031] Optionally, the angle formed by the plane where the communication port is located and the up-down direction is defined as α, which satisfies the relationship: 0°<α≤30°;

[0032] And / or, the cabin is defined to include a front-to-back direction and a left-to-right direction in a horizontal direction, the communication port is provided on the front side of the cabin, and on a projection plane perpendicular to the left-to-right direction, the maximum projection distance of the passenger chamber wall in the front-to-back direction is L1, and the maximum projection distance of the support structure in the front-to-back direction is L2, satisfying the relationship: 0.8≤L2 / L1≤1;

[0033] And / or, defined on a projection plane perpendicular to the front-to-back direction, the maximum projection distance of the cavity wall of the seating cavity in the left-right direction is L3, and the maximum projection distance of the supporting structure in the left-right direction is L4, satisfying the relationship: 0.65≤L4 / L3≤0.85.

[0034] Optionally, the cabin is defined to include a front-to-rear direction and a left-to-right direction in a horizontal direction, and the communication port is provided at the front side of the cabin;

[0035] The support structure includes two groups of support frames, which are arranged side by side in the left and right directions. The support frames include support rods and connecting rods. There are two support rods, which are arranged in sequence in the front and back directions. The opposite ends of the connecting rods are respectively connected to the two support rods.

[0036] Optionally, the distance between the two support rods located at the front side of the two groups of support frames is greater than the distance between the two support rods located at the rear side.

[0037] Optionally, the distance between the two support rods located at the front side of the two groups of support frames is defined as D1, and the distance between the two support rods located at the rear side is defined as D2, satisfying the relationship: 0.5≤D2 / D1≤0.7;

[0038] And / or, the connecting rod includes a first section and a second section that are connected and arranged at an angle, the ends of the first section and the second section that are away from each other are respectively connected to the two support rods, and the angle formed by the first section and the second section of the connecting rod in one group of support frames and the angle formed by the first section and the second section of the connecting rod in another group of support frames are arranged back to back.

[0039] Optionally, the support structure further includes a fixing plate, which connects the two groups of support frames, and the fixing plate is also connected to the splicing assembly located at the bottom.

[0040] Optionally, the cabin further includes a seat, which is arranged in the seating cavity.

[0041] Optionally, the seat includes:

[0042] Cushion part;

[0043] a backrest portion, the backrest portion being protruded from an edge of the seat cushion portion; and

[0044] A headrest portion is connected to an end of the backrest portion away from the seat cushion portion.

[0045] Optionally, one end of the cushion portion away from the backrest portion extends out from the communication port;

[0046] And / or, the seat cushion portion has a seating surface, and the seating surface is an outwardly convex curved surface;

[0047] And / or, the backrest portion has a backrest surface, the backrest surface includes a first surface and a second surface connected to each other, the first surface is arranged closer to the seat cushion portion than the second surface, the first surface is an inner concave arc surface, and the second surface is an outer convex arc surface;

[0048] And / or, the headrest portion has a headrest surface, and the headrest surface is an outwardly convex arc surface.

[0049] The present invention also provides an entertainment system comprising the cockpit as described above.

[0050] The cabin of the present invention utilizes multiple splicing components to form a passenger compartment and a connecting port connecting the compartments. This allows for separate, independent manufacturing of each component during manufacturing. Compared to the entire cabin, the resulting components are simpler in structure and smaller in size, enabling production using simpler and smaller molds. Simpler and smaller molds have a longer lifespan and lower costs, resulting in a relatively low cabin manufacturing cost. The optimized cabin structure of this solution helps reduce manufacturing costs. It also provides a structural foundation for user assembly, fostering hands-on skills and enhancing user experience. Furthermore, the splicing components are designed in a triangular shape, the simplest polygon, making it easy to assemble the components into the desired cabin shape. This improves assembly convenience and flexibility, further enhancing the user experience. BRIEF DESCRIPTION OF THE DRAWINGS

[0051] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on the structures shown in these drawings without paying any creative work.

[0052] FIG1 is a schematic structural diagram of an embodiment of a cockpit of the present invention;

[0053] FIG2 is a schematic diagram of the cockpit in FIG1 from another perspective;

[0054] FIG3 is a schematic diagram of the cockpit in FIG1 from another perspective;

[0055] FIG4 is a schematic diagram of the assembled state of multiple splicing components of the cockpit in FIG1 ;

[0056] FIG5 is a schematic diagram of the assembled multiple components in FIG4 from another perspective;

[0057] FIG6 is a schematic diagram of an exploded structure of multiple splicing components in FIG4;

[0058] FIG7 is a schematic diagram of the exploded structure of the multiple splicing components in FIG6 from another perspective;

[0059] FIG8 is a schematic diagram of the assembly structure of the splicing component and the connector in FIG7 ;

[0060] FIG9 is a schematic diagram of the assembly structure of the splicing component and the connector in FIG8 from another perspective;

[0061] FIG10 is a schematic diagram of an exploded structure of the splicing assembly and the connector in FIG8 ;

[0062] FIG11 is a schematic structural diagram of the connecting member in FIG10 ;

[0063] FIG12 is a schematic diagram of the connecting member in FIG11 from another perspective;

[0064] FIG13 is a schematic diagram of an exploded structure of the connecting member and the filling member in FIG12;

[0065] FIG14 is a schematic structural diagram of a splicing assembly in FIG10;

[0066] FIG15 is a schematic diagram of an exploded structure of the splicing assembly in FIG14;

[0067] FIG16 is a schematic structural diagram of the support structure in FIG1 ;

[0068] Figure 17 is a schematic structural diagram of the seat in Figure 1;

[0069] FIG18 is a schematic cross-sectional view of the seat in FIG17 .

[0070] Description of Figure Numbers:

[0071] The purpose, features and advantages of the present invention will be further described with reference to the accompanying drawings and in conjunction with the embodiments. DETAILED DESCRIPTION

[0072] The following will be combined with the drawings in the embodiments of this application to clearly and completely describe the technical solutions in the embodiments of this application. Obviously, the embodiments described are only part of the embodiments of this application, not all of the embodiments. Based on the embodiments of this application, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of this application.

[0073] It should be noted that all directional indications in the embodiments of the present application (such as up, down, left, right, front, back, etc.) are only used to explain the relative position relationship, movement status, etc. between the various components under a certain specific posture (as shown in the accompanying drawings). If the specific posture changes, the directional indication will also change accordingly.

[0074] In this application, unless otherwise specified or limited, the terms "connection" and "fixation" should be understood in a broad sense. For example, "fixation" can mean fixed connection, detachable connection, or integration; mechanical connection or electrical connection; direct connection or indirect connection through an intermediate medium; internal communication between two elements or interaction between two elements, unless otherwise specified. For those skilled in the art, the specific meanings of the above terms in this application can be understood according to specific circumstances.

[0075] In addition, the descriptions of "first", "second", etc. in this application are for descriptive purposes only and cannot be understood as indicating or implying their relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features defined as "first" and "second" may explicitly or implicitly include at least one of such features. In addition, the meaning of "and / or" appearing throughout the text is to include three parallel solutions. Taking "A and / or B" as an example, it includes solution A, or solution B, or a solution in which both A and B are satisfied. In addition, the technical solutions between the various embodiments can be combined with each other, but this must be based on the ability of ordinary technicians in this field to implement. When the combination of technical solutions is mutually contradictory or cannot be implemented, it should be deemed that such a combination of technical solutions does not exist and is not within the scope of protection required by this application.

[0076] A cockpit, as the name suggests, is an object designed to accommodate passengers. Currently, cockpits in related technologies are typically relatively large, requiring the use of correspondingly large molds. Large molds with complex structures shorten their lifespans and increase costs, leading to relatively high cockpit manufacturing costs. Furthermore, integrated cockpits fail to cultivate user skills and enhance user enjoyment.

[0077] Therefore, based on the above considerations, and to address the relatively high manufacturing costs of current cockpits and their inability to adequately meet some of the personalized needs of users, this application proposes a novel cockpit. This cockpit innovatively incorporates multiple triangular-shaped assembly components, which are joined together to form a passenger compartment and a connecting port connecting the compartments. This allows the cockpit to be manufactured using a relatively simple and compact mold, reducing manufacturing costs. Furthermore, this facilitates user assembly, fostering hands-on skills and enhancing user enjoyment.

[0078] Next, the structure of the cabin proposed in the present application will be explained and illustrated by an embodiment. In one embodiment of the present application, please refer to Figures 1 to 5. The cabin 100 proposed in the present application includes a plurality of splicing components 10, and the plurality of splicing components 10 are spliced ​​together to form a riding cavity 11 and a connecting port 12 connected to the riding cavity 11. The shape of each splicing component 10 is triangular.

[0079] The splicing assembly 10 is an object that can be used for splicing, and then encloses a seating cavity 11 and a communication port 12 that connects the seating cavity 11. Among them, the splicing assembly 10 can be spliced ​​to form a triangular prism structure, a cube structure, a rectangular parallelepiped structure, a near-spherical structure composed of multiple faces, or an ellipsoidal structure. Of course, it can also be a combination of a cone structure 13 and an annular structure 14 as described below. The present application does not limit the shape of the structure enclosed by the splicing assembly 10. The communication port 12 can be set in a plane, or in an arc surface. The present application does not limit the shape of the communication port 12. The shape of each splicing assembly 10 is a triangle, that is, the splicing assembly 10 can be an isosceles triangle as described below, or a right triangle, or even further rounded at the corners (that is, the connection 15 between two adjacent sides of the splicing assembly 10. Since the splicing assembly 10 is a triangle, each splicing assembly 10 has three corners). The present application does not limit the type of triangle of the splicing assembly 10. Furthermore, the sizes of the individual splicing assemblies 10 can be identical, or they can be partially identical, or they can be completely different in size. Furthermore, the splicing assemblies 10 can also be a multi-layer structure, including the mounting plate 16 and the sound-absorbing block 17, as described below, or a single-layer structure. This application does not limit the structure of the splicing assemblies 10. Furthermore, when splicing, the individual splicing assemblies 10 can be connected and assembled using connectors 30, as described below, or they can be directly connected and assembled.

[0080] The cabin 100 of the present invention utilizes multiple splicing components 10 to form a passenger compartment 11 and a connecting port 12 connecting the passenger compartment 11. This allows for separate and independent manufacturing of each component 10 during manufacturing. Compared to the entire cabin 100, the resulting components 10 are simpler and smaller in size, enabling the use of simpler and smaller molds for production. Simpler and smaller molds have a longer lifespan and lower costs, resulting in a relatively low manufacturing cost for the cabin 100. In other words, the optimized structural design of the cabin 100 in this embodiment helps reduce manufacturing costs. It also provides a structural foundation for users to assemble the cabin 100. This fosters user skills and enhances user enjoyment, thereby improving the user experience. Furthermore, the splicing components 10 are designed in a triangular shape, the simplest polygon, making it easier to assemble the components 10 into the desired cabin 100 shape. That is to improve the convenience and flexibility of splicing, which in turn helps to further enhance the user experience.

[0081] Please refer to FIG. 5 . In one embodiment of the present application, the shape of each splicing component 10 is an isosceles triangle, and the sizes of each splicing component 10 are equal.

[0082] In this embodiment, the splicing components 10 are set to be isosceles triangles, and the sizes of the splicing components 10 are equal, so that the splicing components 10 are more regular, which facilitates the subsequent adaptation and splicing between the splicing components 10, thereby improving the convenience of splicing.

[0083] Please refer to FIG. 5 . In one embodiment of the present application, each splicing assembly 10 is in the shape of an equilateral triangle.

[0084] In this embodiment, the splicing assembly 10 is further configured as an equilateral triangle so that the three sides of the splicing assembly 10 are of the same length. In this way, when splicing with the splicing assembly 10, there is no need to consider the directionality of the splicing assembly 10, which is conducive to further improving the convenience of splicing.

[0085] Please refer to Figures 4 to 7. In one embodiment of the present application, some splicing components 10 are enclosed to form a conical structure 13 with an open end. The conical structure 13 is formed by splicing and enclosing 4-6 splicing components 10.

[0086] In this embodiment, the conical structure 13 is formed by enclosing some of the splicing components 10, so that the space enclosed by these components 10 can be arranged to increase in the direction toward the user. This allows the passenger compartment 11 to have a relatively large volume, making it easier for subsequent passengers to board. Furthermore, it also allows the cabin 100 to have a more novel shape, giving the user a more attractive visual experience and enhancing the sense of ritual, which in turn helps improve the user experience. Furthermore, the conical structure 13 includes 4-6 splicing components 10, ensuring that the number of splicing components 10 is not too small, allowing for the splicing of a passenger compartment 11 of appropriate volume. At the same time, it also prevents the number of splicing components 10 from being too large, which would complicate the splicing process. In other words, the number of splicing components 10 in the conical structure 13 is configured in this way, balancing the size of the enclosed passenger compartment 11 and the ease of splicing. The number of conical structures 13 can be one, or two or more; this application does not impose any restrictions on the number of conical structures 13. In addition, the number of the splicing components 10 in the conical structure 13 can be 4, 5, or 6.

[0087] Please refer to Figures 4 to 7. In one embodiment of the present application, part of the splicing components 10 are enclosed to form an annular structure 14 with openings at both ends, and one end of the annular structure 14 is connected to the open end of the conical structure 13; the annular structure 14 and the conical structure 13 are enclosed to form a seating chamber 11, and the end of the annular structure 14 away from the conical structure 13 is enclosed to form a connecting port 12.

[0088] In this embodiment, an annular structure 14 is further provided at one end of the tapered structure 13, further increasing the volume of the seating chamber 11. This annular structure 14 also facilitates direct or indirect seating for users (if a seating position is provided indirectly, a seat 70 may be further provided within the seating chamber 11, as described below), further facilitating passenger comfort. This arrangement further enhances the novelty of the cabin 100's shape, further improving the sense of ritual and user experience.

[0089] It should also be noted that in some embodiments, the number of conical structures 13 can be two or more, and the structure formed by the splicing components 10 other than those that enclose the conical structure 13 can be other than the ring structure 14 described above, but can instead be formed into other shapes. In this case, the remaining splicing components 10 can be partially positioned between the conical structures 13 and partially spliced ​​together, so that the remaining splicing components 10 and the at least two conical structures 13 enclose the seating chamber 11, while the remaining splicing components 10 enclose the connecting opening 12. Alternatively, in some embodiments, when the cabin 100 includes multiple conical structures 13, each conical structure 13 can be formed by the same number of splicing components 10. That is, the number of splicing components 10 in each conical structure 13 is the same. This allows for greater consistency between the conical structures 13, thereby facilitating easier splicing. Alternatively, at least two conical structures 13 can be formed by splicing different numbers of splicing components 10. That is, the number of splicing components 10 in each conical structure 13 is different, or the number of splicing components 10 in only some conical structures 13 is the same. In this way, the conical structures 13 can be more diversified, so as to be spliced ​​into a more novel cabin 100.

[0090] In one embodiment of the present application, the number of splicing components 10 in the conical structure 13 is defined as X, and the number of splicing components 10 in the annular structure 14 is defined as Y, satisfying the relationship: Y=2X.

[0091] In this embodiment, the number of splicing components 10 in the annular structure 14 is set to twice the number of splicing components 10 in the conical structure 13, which can facilitate the adaptive splicing of the annular structure 14 and the conical structure 13. At the same time, the number of splicing components 10 in the annular structure 14 will not be too many, which is conducive to improving the convenience of splicing. Among them, the number of splicing components 10 in the conical structure 13 can be 5 as described below, and the number of splicing components 10 in the annular structure 14 can be 10. Of course, the number of splicing components 10 in the conical structure 13 can also be 6, and the number of splicing components 10 in the annular structure 14 can be 12. In addition, the connecting port 12 can correspond to an X-shaped polygon.

[0092] In one embodiment of the present application, X=5, Y=10.

[0093] In this embodiment, the number of splicing components 10 in the conical structure 13 is set to 5, and the number of splicing components 10 in the annular structure 14 is set to 10, so that the communication port 12 is correspondingly formed into a pentagonal shape. This can greatly simplify the number of splicing components 10 while ensuring a relatively large volume of the seating chamber 11, thereby improving its splicing convenience.

[0094] Please refer to FIG. 8 . In one embodiment of the present application, the adjacent corners of a plurality of splicing components 10 are connected.

[0095] In this embodiment, the adjacent corners of the splicing assemblies 10 are connected, so that a single connection location can connect multiple splicing assemblies 10, thereby facilitating the connection of the splicing assemblies 10. In particular, when connectors 30 are used for connection and assembly as described below, the number of connectors 30 can be further reduced. Of course, it should be noted that the present application is not limited to this, and in other embodiments, adjacent splicing assemblies 10 can also be connected via adjacent side edges.

[0096] Please refer to Figures 8 to 10. In one embodiment of the present application, the position where the corners of multiple adjacent splicing components 10 are close to each other is defined as a connection 15. The cabin 100 also includes multiple connecting parts 30, each connecting part 30 is arranged at a connection 15 and connects the corners of multiple splicing components 10 in the connection 15.

[0097] In this embodiment, the connector 30 facilitates contact with adjacent corners of the plurality of splicing assemblies 10, thereby facilitating the connection and assembly of the adjacent plurality of splicing assemblies 10. Furthermore, such an arrangement eliminates the need for stacking adjacent splicing assemblies 10, further facilitating the arrangement of the splicing assemblies 10.

[0098] Please refer to Figures 10 and 11. In one embodiment of the present application, the connecting member 30 includes a main body plate 31 and a connecting plate 33. The connecting plate 33 is a flat plate. There are multiple connecting plates 33. The multiple connecting plates 33 are all connected to the edge of the main body. The corners of each splicing component 10 in the connection 15 are correspondingly connected to a connecting plate 33.

[0099] In this embodiment, the connector 30 is configured to include a main body plate 31 and a connecting plate 33. Multiple connecting plates 33 can be connected through the main body plate 31, so that the multiple connecting plates 33 can form a whole, thereby facilitating the removal and placement of the connector 30 as a whole and improving the convenience of installation. The connecting plates 33 can better correspond to the corners in each splicing assembly 10, so as to achieve the connection between the connector 30 and the splicing assembly 10. Furthermore, the connecting plate 33 is configured as a flat plate, so that the connecting plate 33 can better abut against the splicing assembly 10, thereby facilitating the improvement of the convenience and stability of the connection between the two. Among them, the connecting plate 33 can extend into the splicing assembly 10 as described below, and of course it can also be stacked on the outside or inside of the splicing assembly 10.

[0100] Please refer to Figures 9 to 11. In one embodiment of the present application, the adjacent corners of the plurality of splicing components 10 are spaced apart so that the main plate 31 is exposed to the outside. The main plate 31 is a convex arc plate.

[0101] In this embodiment, the adjacent corners of the multiple splicing assemblies 10 are spaced apart, exposing the main body panel 31. This prevents adjacent corners of the multiple splicing assemblies 10 from forming sharp corners. Specifically, when the main body panel 31 is configured as a convex curved plate, this area can be smoothly curved, reducing the risk of injury from collisions with the user, thereby improving the safety of the cabin 100. Furthermore, the exposed convex curved shape of the main body panel 31, combined with the triangular shape of the splicing assemblies 10, also makes the cabin 100 more unique and novel, further enhancing the visual appeal of the cabin 100 and the sense of ritual when using the splicing assemblies 10. Furthermore, the convex curved shape of the main body panel 31 facilitates contact and connection between the edges of the main body panel 31 and the various connecting panels 33 spaced along the circumference of the main body panel 31. To enhance the visibility of the main body panel 31, the corners of the splicing assemblies 10 can be rounded. At the same time, such a configuration can also reduce the possibility of corners being easily damaged by collisions and avoid the possibility of punctures to users, thereby helping to improve the service life and safety of the splicing assembly 10.

[0102] Please refer to Figures 12 and 13. In one embodiment of the present application, the cabin 100 also includes a plurality of filling pieces 40. Each filling piece 40 is arranged on the inner side of the main plate 31 of a connecting piece 30, and the side of the filling piece 40 facing away from the main plate 31 is a plane.

[0103] In this embodiment, the inner side of the main panel 31 can be filled by the filling piece 40, and the side of the filling piece 40 facing away from the main panel 31 is flat, so that the inner side of the cabin 100 can also be relatively flat, so as to give the user a better visual experience and improve the competitiveness of the subsequent cabin 100 in the market.

[0104] In one embodiment of the present application, the connecting plates 33 extend into corners of corresponding splicing components 10 .

[0105] Referring to Figures 8 and 10 , in this embodiment, extending the connecting plate 33 into the corners of the splicing assembly 10 for connection increases the contact area between the two, thereby improving the stability of the splicing connection between the splicing assemblies 10. This arrangement also improves the compactness of the connection between the connecting plate 33 and the splicing assembly 10. Furthermore, the connecting plate 33 is concealed, thereby facilitating a better display of both the exterior and interior of the splicing assembly 10, enhancing the visual consistency and overall visual quality of the cabin 100.

[0106] In one embodiment of the present application, the connecting plate 33 and the corners of the splicing assembly 10 are connected by screws.

[0107] In this embodiment, the connecting plate 33 and the splicing assembly 10 are connected by screws, which have the advantages of being simple and reliable. This can simplify the connection process between the connecting plate 33 and the splicing assembly 10 while ensuring the stability of the connection between the connecting plate 33 and the splicing assembly 10, thereby improving the connection efficiency. Of course, it should be noted that the present application is not limited to this. In other embodiments, the connector 30 and the splicing assembly 10 can also be connected by snap-fit ​​connection or magnetic connection.

[0108] Please refer to Figure 11. In one embodiment of the present application, the connecting member 30 further includes multiple first reinforcing plates 35. Each first reinforcing plate 35 connects the main plate 31 and two adjacent connecting plates 33. The first reinforcing plates 35 are outwardly convex arc-shaped plates.

[0109] In this embodiment, the first reinforcing plate 35 connects the main plate 31 and the two adjacent connecting plates 33, thereby enhancing the overall strength of the connector 30 and providing a more stable load-bearing connection between the connector 30 and the adjacent splicing assemblies 10. The first reinforcing plate 35 can also shield the area between the two corners of the two adjacent splicing assemblies 10, thereby improving the sealing of the seating chamber 11.

[0110] Please refer to Figures 14 and 15. In one embodiment of the present application, the splicing assembly 10 includes a mounting plate 16 and a sound-absorbing block 17. The sound-absorbing block 17 is arranged on the inner side of the mounting plate 16; a speaker 161 is provided on the side of at least one mounting plate 16 facing the sound-absorbing block 17, and an avoidance hole 18 is provided on the sound-absorbing block 17 at a position corresponding to the speaker 161.

[0111] In this embodiment, at least one mounting plate 16 is provided with a speaker 161. This allows the cockpit 100 to provide users with a wider range of scenarios and a more comprehensive experience of high-quality sound (e.g., game or movie music) through the speaker 161, thereby further enhancing the user experience. The sound-absorbing block 17 absorbs sound generated by the speaker 161 that propagates radially from the speaker 161, reducing sound reflections and improving the sound quality of the speaker 161 along the axial direction of the speaker 161. The speaker 161 may be provided on the mounting plate 16 of only one assembly 10, or it may be provided on the mounting plates 16 of two or more assemblies 10. Furthermore, configuring each assembly 10 to include a mounting plate 16 and a sound-absorbing block 17 ensures a consistent structure and appearance across the assembly 10, facilitating subsequent assembly and connection between the assemblies 10 and enhancing the visual consistency of the assemblies 10, thereby improving the visual experience. Furthermore, mounting plate 16 can be made of wood to reduce absorption of sound generated by speaker 161, further facilitating sound emission from speaker 161 along its axial direction. Furthermore, using wood also reduces the cost of mounting plate 16. Of course, mounting plate 16 can also be made of plastic, a material not limited in this application. Sound-absorbing block 17 can be made of sponge, making it easily available and cost-effective.

[0112] In one embodiment of the present application, the splicing assembly 10 further includes a protective net 19 , which is disposed on a side of the sound absorbing block 17 facing away from the mounting plate 16 .

[0113] In this embodiment, the protective net 19 covers the avoidance hole 18, reducing the possibility of dust and other particles entering the speaker 161 and damaging it, thereby improving the service life of the speaker 161. Furthermore, the protective net 19 provides a consistent appearance between the interior of the assembly 10 equipped with the speaker 161 and the interior of the assembly 10 without the speaker 161, thereby enhancing the visual experience of the interior of the cabin 100. The protective net 19 can be made of fabric, making it readily available and cost-effective, while also increasing the lightweightness of the assembly 10.

[0114] Please refer to FIG. 15 . In one embodiment of the present application, the splicing assembly 10 further includes a second reinforcing plate 20 . The second reinforcing plate 20 is disposed on a side of the mounting plate 16 that faces away from the sound absorbing block 17 .

[0115] In this embodiment, the second reinforcing plate 20 can be used to strengthen the overall strength of the splicing assembly 10, reduce the possibility of the splicing assembly 10 being damaged by collision, and thus help to improve the service life of the cabin 100. The material of the second reinforcing plate 20 can be metal, so as to improve the reinforcing effect on the strength of the splicing assembly 10. Of course, the second reinforcing plate 20 can also be plastic. In addition, the connecting plate 33 in the connector 30 introduced above can extend between the second reinforcing plate 20 and the mounting plate 16, and be connected to the second reinforcing plate 20 with relatively strong strength, so as to enhance the stability of the connection between the connecting plate 33 and the splicing assembly 10. Of course, the connecting plate 33 can also be connected to the mounting plate 16, and this application does not limit this.

[0116] Please refer to FIG. 15 . In one embodiment of the present application, the splicing assembly 10 further includes a decorative cover 21 . The decorative cover 21 is disposed on a side of the second reinforcing plate 20 facing away from the mounting plate 16 .

[0117] In this embodiment, a decorative cover 21 is further provided on the outer side of the second reinforcing plate 20. The decorative cover 21 can decorate the outer side of the splicing assembly 10, thereby further improving the consistency of the outer appearance of each splicing assembly 10 and enhancing the visual effect of the cabin 100. At the same time, the decorative cover 21 can also play a protective role.

[0118] In one embodiment of the present application, when the splicing assembly 10 includes the aforementioned mounting plate 16, sound-absorbing block 17, protective mesh 19, second reinforcing plate 20, and decorative cover 21, each of these components may be triangular in shape. Alternatively, only the decorative cover 21 and the sound-absorbing block 17 may be triangular in shape. In this case, the decorative cover 21 may be positioned outside the second reinforcing plate 20, while the sound-absorbing block 17 may also be positioned outside the mounting plate 16.

[0119] Please refer to Figures 1 and 2. In one embodiment of the present application, the cabin 100 is defined as having an up-down direction and a horizontal direction (the up-down direction and the horizontal direction are defined when the cabin 100 is in a normal use and placement state), and the connecting port 12 is arranged to be inclined upward; the cabin 100 also includes a support structure 50, which is arranged on the lower surface of the splicing component 10 located at the bottom, and the lower surface of the support structure 50 is a plane.

[0120] In this embodiment, the connecting port 12 is arranged to be tilted upward, which can reduce the obstruction of the user's head, thereby making it easier for the user to get on and off the riding chamber 11, and further improving the user's experience. At the same time, such an arrangement also makes it easier for the user's body to sit in the riding chamber 11 at an angle, so that the user's perspective can be more consistent with the direction of the connecting port 12, thereby making it easier for the user in the riding chamber 11 to have a wider perspective of the outside world. Further, a support structure 50 is arranged below the combined structure formed by the splicing components 10, and the lower surface of the support structure 50 is also arranged to be flat, so that the cabin 100 can be stably placed on a supporting surface such as the ground through the support structure 50. Among them, the support structure 50 can be in the form of a support frame 51 as described below, or of course, it can be in the form of a support seat. This application does not limit the structural type of the support structure 50.

[0121] Please refer to FIG. 2 . In one embodiment of the present application, the angle formed by the plane where the communication port 12 is located and the up-down direction is defined as α, which satisfies the relationship: 0°<α≤30°.

[0122] In this embodiment, the angle α formed between the plane where the communication opening 12 is located and the vertical direction is set to 0° to 30°, so that the inclination angle of the communication opening 12 is not too large, so that the user can enter smoothly and have a good view of the outside through the communication opening 12 after riding. Among them, the angle α formed between the plane where the communication opening 12 is located and the vertical direction can be 1°, 2°, 3°, 4°, 5°, 6°, 7°, 8°, 9°, 10°, 11°, 12°, 13°, 14°, 15°, 16°, 17°, 18°, 19°, 20°, 21°, 22°, 23°, 24°, 25°, 26°, 27°, 28°, 29° or 30°, and of course it can also be any value within the above range.

[0123] Please refer to Figure 2. In one embodiment of the present application, the cabin 100 is defined to include the front-to-back direction and the left-to-right direction in the horizontal direction. The connecting port 12 is provided on the front side of the cabin 100. On a projection plane perpendicular to the left-to-right direction, the cavity wall of the riding cavity 11 (in other words, the combined structure formed by splicing multiple splicing components 10) has a maximum projection distance L1 in the front-to-back direction, and the maximum projection distance of the support structure 50 in the front-to-back direction is L2, satisfying the relationship: 0.8≤L2 / L1≤1.

[0124] In this embodiment, the ratio of the maximum front-to-back projection distance L2 of the support structure 50 to the maximum front-to-back projection distance L1 of the passenger compartment 11 is set to 0.8 to 1. This ensures that the maximum front-to-back projection distance L2 of the support structure 50 is not too small, thereby affecting the stability of the support structure formed by the multiple assembly components 10. Furthermore, it also ensures that the maximum front-to-back projection distance L2 of the support structure 50 is not too large, thereby increasing the overall volume of the cabin 100 and the required space. Therefore, setting L2 / L1 to 0.8 to 1 balances the stability of the support structure formed by the multiple assembly components 10 and the compactness of the cabin 100, ensuring a stable ride for users and facilitating the placement of the cabin 100 within a limited space. L2 / L1 can be 0.8, 0.85, 0.9, 0.95, or 1, or any other value within this range. To achieve the same effect, in one embodiment of the present application, referring to FIG. 3 , a maximum left-right projection distance of the wall of the seating chamber 11 is defined as L3 on a projection plane perpendicular to the front-to-back direction, and a maximum left-right projection distance of the support structure 50 is defined as L4, satisfying the relationship: 0.65 ≤ L4 / L3 ≤ 0.85. The ratio of the maximum left-right projection distance L4 of the support structure 50 to the maximum left-right projection distance L3 of the wall of the seating chamber 11 can be 0.65, 0.7, 0.75, 0.8, or 0.85, or any other value within the above ranges.

[0125] Please refer to Figures 1 to 3, as well as Figure 16. In one embodiment of the present application, the cabin 100 is defined to include a front-to-back direction and a left-to-right direction in the horizontal direction, and the connecting port 12 is provided on the front side of the cabin 100; the support structure 50 includes two groups of support frames 51, and the two groups of support frames 51 are arranged side by side in the left-to-right direction. The support frames 51 include support rods 511 and connecting rods 513. There are two support rods 511, which are arranged sequentially in the front-to-back direction, and the opposite ends of the connecting rod 513 are respectively connected to the two support rods 511.

[0126] In this embodiment, the support structure 50 is set as two groups of support frames 51, and each group of support frames 51 includes two support rods 511 and a connecting rod 513. On the basis of ensuring that the support structure 50 is stably supported by the four support rods 511, the structure of the support structure 50 can be made simpler, thereby improving the lightweight effect of the support structure 50, and at the same time reducing the raw materials required for manufacturing and reducing manufacturing costs.

[0127] Please refer to FIG. 16 . In one embodiment of the present application, the distance between the two support rods 511 located at the front side of the two sets of support frames 51 is greater than the distance between the two support rods 511 located at the rear side.

[0128] In this embodiment, the distance between the two support rods 511 located on the front sides of the two sets of support frames 51 is set relatively large, and the center of gravity of the cabin 100 is also located close to the front support rods 511. Therefore, the stability of the support of the cabin 100 can be improved by the two support rods 511 with a large distance between them.

[0129] Please refer to Figure 16. In one embodiment of the present application, the distance between the two support rods 511 located on the front side of the two groups of support frames 51 is defined as D1, and the distance between the two support rods 511 located on the rear side is defined as D2, satisfying the relationship: 0.5≤D2 / D1≤0.7.

[0130] In this embodiment, the ratio of the spacing D2 between the two support rods 511 on the rear side to the spacing D1 between the two support rods 511 on the front side is set to 0.5 to 0.7. This ensures that the spacing D2 between the two support rods 511 on the rear side does not affect the stability of the support structure 50 due to being too small. At the same time, it also ensures that the spacing D2 between the two support rods 511 on the rear side does not occupy too much space due to being too large. Therefore, setting the ratio range of the spacing D2 between the two support rods 511 on the rear side to the spacing D1 between the two support rods 511 on the front side in this way takes into account both the stability of the support structure 50 and the compactness of the structure. Among them, the ratio of the spacing D2 between the two support rods 511 on the rear side to the spacing D1 between the two support rods 511 on the front side can be 0.5, 0.55, 0.6, 0.65 or 0.7, and of course it can also be any value within the above range.

[0131] Please refer to Figure 16. In one embodiment of the present application, the connecting rod 513 includes a first segment 515 and a second segment 517 that are connected and arranged at an angle. The ends of the first segment 515 and the second segment 517 that are away from each other are respectively connected to the two support rods 511. The angle formed by the first segment 515 and the second segment 517 of the connecting rod 513 in one group of support frames 51 and the angle formed by the first segment 515 and the second segment 517 of the connecting rod 513 in another group of support frames 51 are arranged back to back.

[0132] In this embodiment, the connecting rod 513 is configured to include a first segment 515 and a second segment 517 at an angle, and the angle formed by the two connecting rods 513 is arranged to face each other, which can make the two connecting rods 513 more compact. At the same time, this arrangement can also provide more suitable abutment support for the triangular-shaped splicing assembly 10. For example, the first segments 515 of the two connecting rods 513 can abut and support the two sides of the triangular-shaped splicing assembly 10.

[0133] Please refer to FIG. 16 . In one embodiment of the present application, the support structure 50 further includes a fixing plate 53 . The fixing plate 53 connects the two sets of support frames 51 . The fixing plate 53 is also connected to the splicing assembly 10 located at the bottom.

[0134] In this embodiment, the fixing plate 53 can be used to adapt and abut against the splicing assembly 10, thereby improving the convenience and stability of the connection between the two. On the other hand, it can also be used to connect the two sets of support frames 51 to form a whole, thereby allowing the two sets of support frames 51 to be installed at one time, thereby improving the convenience of installation.

[0135] Please refer to FIG. 1 and FIG. 3 . In one embodiment of the present application, the cabin 100 further includes a seat 70 . The seat 70 is disposed in the seating cavity 11 .

[0136] In this embodiment, the provision of seat 70 provides a more comfortable seating position for the user, thereby improving the user's comfort within cabin 100 and further enhancing the user's experience. The seat 70 can be connected to the upper surface of the lowest splicing assembly 10. In this case, this splicing assembly 10 can be configured similarly to other splicing assemblies 10, including a mounting plate 16, sound-absorbing blocks 17, a protective net 19, a second reinforcing plate 20, and a decorative cover 21. Alternatively, it can be configured differently from other splicing assemblies 10, including only the second reinforcing plate 20 and the decorative cover 21, so that the connection to the seat 70 does not result in excessive thickness in this area.

[0137] Please refer to Figure 17. In one embodiment of the present application, the seat 70 includes a cushion portion 71, a backrest portion 73 and a headrest portion 75; the backrest portion 73 is protruded from the edge of the cushion portion 71; and the headrest portion 75 is connected to one end of the backrest portion 73 away from the cushion portion 71.

[0138] In this embodiment, the seat 70 is configured to include a seat cushion portion 71, a backrest portion 73, and a headrest portion 75. The seat cushion portion 71 can be used for seating, the backrest portion 73 can be used for backrest, and the headrest portion 75 can be used to support the user's head. This allows the seat 70 to provide good support for all parts of the user's body, thereby improving the user's riding comfort. Further, please refer to Figure 18. In order to facilitate the user to sit more comfortably on the seat 70 with the body in a tilted posture, the seat cushion portion 71 is defined as having a seating surface 711, and the seating surface 711 can be an outward convex curved surface; the backrest portion 73 is defined as having a backrest surface 731, and the backrest surface 731 can include a first surface 733 and a second surface 735 connected to each other, and the first surface 733 is arranged closer to the seat cushion portion 71 than the second surface 735, the first surface 733 is an inward concave curved surface, and the second surface 735 is an outward convex curved surface; the headrest portion 75 is defined as having a headrest surface 751, and the headrest surface 751 can be an outward convex curved surface.

[0139] Please refer to FIG. 1 and FIG. 2 . In one embodiment of the present application, one end of the cushion portion 71 away from the backrest portion 73 extends out from the communication opening 12 .

[0140] In this embodiment, the connecting opening 12 is protruded from one end of the cushion portion 71 away from the backrest portion 73, so that when the user sits in the cabin 100, the connection 15 between the user's thigh and calf can be overlapped on the cushion portion 71, avoiding being squeezed by the edge of the connecting opening 12 and causing a sense of oppression, thereby helping to further improve the riding comfort and further enhance the user experience.

[0141] The present application also proposes an entertainment system, which includes a cockpit 100. The specific structure of the cockpit 100 refers to the above-mentioned embodiment. Since the present entertainment system adopts all the technical solutions of all the above-mentioned embodiments, it has at least all the beneficial effects brought about by the technical solutions of the above-mentioned embodiments, which will not be repeated here. Among them, the entertainment system may also include a head-mounted display device (VR device or AR device). At this time, the user can use the head-mounted display device more conveniently while sitting in the cockpit 100. Of course, the entertainment system may also include a projector, in which case the user can sit in the cockpit 100 and watch the movie projected by the projector.

[0142] The above description is only a preferred embodiment of the present application and does not limit the patent scope of the present application. All equivalent structural transformations made by using the contents of the present application description and drawings under the inventive concept of the present application, or direct / indirect application in other related technical fields are included in the patent protection scope of the present application.

Claims

1. A cockpit, characterized in that, It includes a plurality of splicing components, and the plurality of splicing components are spliced and enclosed to form a riding cavity and a communication port communicating with the riding cavity, and the shape of each of the splicing components is triangular.

2. The cockpit according to claim 1, characterized in that, The shape of each of the splicing components is an isosceles triangle, and the sizes of the splicing components are equal.

3. The cockpit according to claim 2, characterized in that, The shape of each of the splicing components is an equilateral triangle.

4. The cockpit according to claim 1, characterized in that, Some of the splicing components are enclosed to form a conical structure with one end open, and the conical structure is formed by splicing and enclosing 4-6 of the splicing components.

5. The cockpit according to claim 4, characterized in that, Some of the splicing components are enclosed to form an annular structure with both ends open, and one end of the annular structure is connected to the open end of the conical structure; The annular structure and the conical structure enclose to form the riding cavity, and the end of the annular structure away from the conical structure encloses to form the communication port.

6. The cockpit according to claim 5, characterized in that, Define the number of splicing components in the conical structure as X, and the number of splicing components in the annular structure as Y, satisfying the relationship: Y = 2X.

7. The cockpit according to claim 4, characterized in that, The cockpit includes a plurality of the conical structures, and any one of the conical structures is formed by splicing and enclosing the same number of the splicing components; or, At least two of the conical structures are formed by splicing and enclosing different numbers of splicing components.

8. The cockpit according to any one of claims 1 to 7, characterized in that, The adjacent corners of the plurality of splicing components are connected.

9. The cockpit according to claim 8, characterized in that, Define the position where the adjacent corners of the plurality of splicing components are close to each other as the connection part. The cockpit further includes a plurality of connecting pieces, and each connecting piece is arranged at one connection part and connects the corners of the plurality of splicing components in this connection part.

10. The cockpit according to claim 9, characterized in that, The connecting piece includes: A main body plate; and Connecting plates. The connecting plates are flat plates, and the number of the connecting plates is multiple. The multiple connecting plates are all connected to the edge of the main body. Each corner of the splicing components in the connection part is correspondingly connected to one connecting plate.

11. The cockpit according to claim 10, characterized in that, The adjacent corners of the plurality of splicing components are spaced apart so that the main body plate is exposed to the outside, and the main body plate is a convex arc-shaped plate.

12. The cockpit according to claim 11, characterized in that, The cockpit further includes a plurality of filling pieces, and each filling piece is arranged inside the main body plate of one connecting piece, and the side of the filling piece facing away from the main body plate is a plane.

13. The cockpit according to claim 10, characterized in that, The connecting plate extends into the corner of the corresponding splicing component; And / or, the connecting plate and the corner of the splicing component are connected by screws; And / or, the connecting piece further includes a plurality of first reinforcing plates, and each first reinforcing plate connects the main body plate and two adjacent connecting plates, and the first reinforcing plate is a convex arc-shaped plate.

14. The cockpit according to any one of claims 1 to 7, characterized in that, The splicing component includes a mounting plate and a sound-absorbing block, and the sound-absorbing block is arranged inside the mounting plate; At least one side of the mounting plate facing the sound-absorbing block is provided with a speaker, and the sound-absorbing block is provided with an avoidance hole corresponding to the position of the speaker.

15. The cockpit according to claim 14, characterized in that, The splicing component further includes a protective net, and the protective net is arranged on the side of the sound-absorbing block facing away from the mounting plate.

16. The cockpit according to claim 14, wherein The splicing component further includes a second reinforcing plate, and the second reinforcing plate is arranged on the side of the mounting plate facing away from the sound-absorbing block.

17. The cockpit according to claim 16, characterized in that, The splicing component further includes a decorative cover, and the decorative cover is arranged on the side of the second reinforcing plate facing away from the mounting plate.

18. The cockpit according to any one of claims 1 to 7, characterized in that, Define that the cockpit has an up-down direction and a horizontal direction, and the communication port is arranged to incline upwards; The cockpit further includes a support structure, the support structure is arranged on the lower surface of the splicing component located at the lowermost part, and the lower surface of the support structure is a plane.

19. The cockpit according to claim 18, characterized in that, Define the included angle formed by the plane where the communication port is located and the up-down direction as α, and satisfy the relationship: 0° < α ≤ 30°; And / or, define that the cockpit includes a front-back direction and a left-right direction in the horizontal direction, the communication port is arranged on the front side of the cockpit, on a projection plane perpendicular to the left-right direction, the maximum projection distance of the cavity wall of the riding cavity in the front-back direction is L1, and the maximum projection distance of the support structure in the front-back direction is L2, and satisfy the relationship: 0.8 ≤ L2 / L1 ≤ 1; And / or, define that on a projection plane perpendicular to the front-back direction, the maximum projection distance of the cavity wall of the riding cavity in the left-right direction is L3, and the maximum projection distance of the support structure in the left-right direction is L4, and satisfy the relationship: 0.65 ≤ L4 / L3 ≤ 0.

85.

20. The cockpit according to claim 18, characterized in that, Define that the cockpit includes a front-back direction and a left-right direction in the horizontal direction, and the communication port is arranged on the front side of the cockpit; The support structure includes two sets of support frames, the two sets of support frames are arranged side by side in the left-right direction, each support frame includes a support rod and a connecting rod, the number of support rods is two, and they are arranged in sequence in the front-back direction, and the opposite ends of the connecting rod are respectively connected to the two support rods.

21. The cockpit according to claim 20, wherein The distance between the two support rods located at the front side in the two sets of support frames is greater than the distance between the two support rods located at the rear side.

22. The cockpit according to claim 21, wherein, Define the distance between the two support rods located at the front side in the two sets of support frames as D1, and the distance between the two support rods located at the rear side as D2, and satisfy the relationship: 0.5 ≤ D2 / D1 ≤ 0.7; And / or, the connecting rod includes a first body and a second body that are connected and arranged at an angle, the ends of the first body and the second body that are away from each other are respectively connected to the two support rods, and the included angle formed by the first body and the second body of the connecting rod in one set of support frames and the included angle formed by the first body and the second body of the connecting rod in the other set of support frames are arranged back to back.

23. The cockpit according to claim 20, characterized in that, The support structure further includes a fixing plate, the fixing plate connects the two sets of support frames, and the fixing plate is also connected to the splicing component located at the lowermost part.

24. The cockpit according to any one of claims 1 to 7, characterized in that, The cockpit further includes a seat, and the seat is arranged in the riding cavity.

25. The cockpit according to claim 24, characterized in that, The seat includes: A seat cushion part; A backrest part, the backrest part protrudes from the edge of the seat cushion part; and A headrest part, the headrest part is connected to the end of the backrest part away from the seat cushion part.

26. The cockpit according to claim 25, characterized in that, The end of the seat cushion part away from the backrest part extends out from the communication port; And / or, the seat cushion part has a riding surface, and the riding surface is a convex arc surface; And / or, the backrest part has a backrest surface, the backrest surface includes a first surface and a second surface that are connected, the first surface is closer to the seat cushion part than the second surface, the first surface is a concave arc surface, and the second surface is a convex arc surface; And / or, the headrest part has a headrest surface which is a convex arc surface.

27. An entertainment system, characterized in that, Comprising a cockpit as described in any one of claims 1 to 26.

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