Cabin and entertainment system

Abstract

The invention discloses a cabin and an entertainment system. The cabin comprises a plurality of splicing assemblies. Wherein the plurality of splicing assemblies are spliced and enclosed to form a riding cavity and a communication port communicated with the riding cavity, and each splicing assembly is in a triangular shape. According to the technical scheme, the manufacturing cost of the cockpit can be reduced, meanwhile, a structural foundation is provided, a user can splice the cockpits conveniently, the manipulative ability of the user is cultivated, interestingness is enhanced, and then the use experience of the user is improved.

Description

Technical Field

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

[0002] Currently, the volume of the cockpit in the related art is usually set to be relatively large, so that relatively large molds need to be correspondingly used during manufacturing. When the mold is relatively large in volume and complex in structure, its service life is low and the cost is high, which in turn leads to a relatively high manufacturing cost of the cockpit. Summary of the Invention

[0003] The main object of the present invention is to provide a cockpit, aiming to reduce the manufacturing cost of the cockpit.

[0004] To achieve the above object, the cockpit proposed by the present invention includes a plurality of splicing components, and the plurality of splicing components are spliced and enclosed to form a seating cavity and a communication port communicating with the seating cavity, and the shape of each splicing component is triangular.

[0005] Optionally, the shape of each splicing component is an isosceles triangle, and the sizes of the splicing components are equal.

[0006] Optionally, the shape of each splicing component is an equilateral triangle.

[0007] Optionally, some of the splicing components enclose to form a conical structure with one end open, and the conical structure is formed by enclosing 4 - 6 of the splicing components.

[0008] Optionally, some of the splicing components enclose 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;

[0009] The annular structure and the conical structure enclose to form the seating cavity, and the end of the annular structure away from the conical structure encloses to form the communication port.

[0010] Optionally, defining the number of splicing components in the conical structure as X and the number of splicing components in the annular structure as Y, the relationship is satisfied: Y = 2X.

[0011] Optionally, 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,

[0012] At least two of the conical structures are formed by splicing and enclosing different numbers of splicing components.

[0013] Optionally, the adjacent corners of the plurality of splicing components are connected.

[0014] Optionally, define the position where the corners of adjacent splicing components are close to each other as the connection point. The cockpit further includes a plurality of connecting members, and each connecting member is disposed at one connection point and connects the corners of the plurality of splicing components at this connection point.

[0015] Optionally, the connecting member includes:

[0016] a main body plate; and

[0017] a connecting plate. The connecting plate is a flat plate, and the number of the connecting plates is multiple. A plurality of the connecting plates are all connected to the edge of the main body. Each corner of the splicing components at the connection point is correspondingly connected to one connecting plate.

[0018] Optionally, the adjacent corners of the plurality of splicing components are spaced apart from each other so that the main body plate is exposed to the outside. The main body plate is a convex arc plate.

[0019] Optionally, the cockpit further includes a plurality of filling members, and each filling member is disposed inside the main body plate of one connecting member. The side of the filling member facing away from the main body plate is a plane.

[0020] Optionally, the connecting plate extends into the corner of the corresponding splicing component;

[0021] and / or, the connecting plate and the corner of the splicing component are connected by screws;

[0022] and / or, the connecting member further includes a plurality of first reinforcing plates. Each first reinforcing plate connects the main body plate and two adjacent connecting plates. The first reinforcing plate is a convex arc plate.

[0023] Optionally, the splicing component includes a mounting plate and a sound absorption block, and the sound absorption block is disposed inside the mounting plate;

[0024] At least one side of the mounting plate facing the sound absorption block is provided with a speaker, and the sound absorption block is provided with an avoidance hole corresponding to the position of the speaker.

[0025] Optionally, the splicing component further includes a protective net, and the protective net is disposed on the side of the sound absorption block facing away from the mounting plate.

[0026] Optionally, the splicing component further includes a second reinforcing plate, and the second reinforcing plate is disposed on the side of the mounting plate facing away from the sound absorption block.

[0027] Optionally, the splicing component further includes a decorative cover, and the decorative cover is disposed on the side of the second reinforcing plate facing away from the mounting plate.

[0028] Optionally, it is defined that the cockpit has an up-down direction and a horizontal direction, and the communication port is arranged to incline upwards;

[0029] The cockpit further includes a support structure, the support structure is arranged on the lower surface of the splicing component located at the bottommost, and the lower surface of the support structure is a plane.

[0030] Optionally, it is defined that the included angle formed by the plane where the communication port is located and the up-down direction is α, satisfying the relationship: 0° < α ≤ 30°;

[0031] And / or, it is defined 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, satisfying the relationship: 0.8 ≤ L2 / L1 ≤ 1;

[0032] And / or, it is defined 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, satisfying the relationship: 0.65 ≤ L4 / L3 ≤ 0.85.

[0033] Optionally, it is defined 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;

[0034] The support structure includes two groups of support frames, the two groups of support frames are arranged side by side in the left-right direction, the support frame includes a support rod and a connecting rod, the number of the 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.

[0035] Optionally, the distance between the two support rods located at the front side in the two groups of support frames is greater than the distance between the two support rods located at the rear side.

[0036] Optionally, it is defined that the distance between the two support rods located at the front side in the two groups of support frames is D1, and the distance between the two support rods located at the rear side is D2, satisfying the relationship: 0.5 ≤ D2 / D1 ≤ 0.7;

[0037] And / or, the connecting rod includes a first section body and a second section body which are connected and arranged at an angle, the ends of the first section body and the second section body away from each other are respectively connected to the two support rods, and the included angle formed by the first section body and the second section body of the connecting rod in one group of support frames and the included angle formed by the first section body and the second section body of the connecting rod in the other group of support frames are arranged back to back.

[0038] Optionally, the support structure further includes a fixing plate, which connects the two sets of support frames and is also connected to the splicing component at the lowermost position.

[0039] Optionally, the cockpit further includes a seat, which is arranged in the riding cavity.

[0040] Optionally, the seat includes:

[0041] A seat cushion part;

[0042] A backrest part, which protrudes from the edge of the seat cushion part; and

[0043] A headrest part, which is connected to one end of the backrest part away from the seat cushion part.

[0044] Optionally, one end of the seat cushion part away from the backrest part extends out from the communication port;

[0045] And / or, the seat cushion part has a riding surface, and the riding surface is a convex arc surface;

[0046] And / or, the backrest part has a backrest surface, which includes a connected first surface and a second surface. The first surface is arranged 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;

[0047] And / or, the headrest part has a headrest surface, and the headrest surface is a convex arc surface.

[0048] The present invention also provides an entertainment system, including the cockpit as described above.

[0049] The cockpit of the technical solution of the present invention is formed by splicing and enclosing multiple splicing components to form a riding cavity and a communication port connecting the riding cavity, so that each splicing component can be separately and independently manufactured during manufacturing. At this time, the split splicing components are simpler in structure and relatively smaller in volume compared to the whole cockpit, and thus relatively simpler and smaller molds can be used for production correspondingly. The molds with relatively simple structures and relatively small volumes have higher service lives and lower costs, and thus the manufacturing cost of the cockpit can be relatively lower accordingly. That is to say, the optimized design of the structure of the cockpit in this solution is beneficial to reducing the manufacturing cost of the cockpit. At the same time, it also provides a structural basis for users to splice the cockpit. In this way, it can cultivate users' hands-on ability and enhance the fun, and thus is beneficial to improving users' use experience. Further, the splicing components are set as triangles, and the triangle is the simplest polygon, which can facilitate splicing the splicing components into the cockpit of the required shape. That is to say, it improves the convenience and flexibility of splicing, and thus is beneficial to further improving users' use experience. Brief Description of the Drawings

[0050] In order to more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the following will briefly introduce the drawings required for the description of the embodiments or the prior art. Obviously, the drawings in the following description are only some embodiments of the present invention. For those of ordinary skill in the art, without creative efforts, other drawings can be obtained based on the structures shown in these drawings.

[0051] Figure 1 It is a schematic structural diagram of an embodiment of the cockpit of the present invention;

[0052] Figure 2 It is Figure 1 Another perspective schematic diagram of the cockpit in;

[0053] Figure 3 It is Figure 1 Another perspective schematic diagram of the cockpit in;

[0054] Figure 4 It is Figure 1 An assembled state schematic diagram of multiple splicing components of the cockpit in;

[0055] Figure 5 It is Figure 4 Another perspective schematic diagram of the assembled state of multiple splicing components in;

[0056] Figure 6 It is Figure 4 An exploded structural schematic diagram of multiple splicing components in;

[0057] Figure 7 It is Figure 6 Another perspective schematic diagram of the exploded structure of multiple splicing components in;

[0058] Figure 8 It is Figure 7 An assembled structural schematic diagram of a splicing component and a connecting member in;

[0059] Figure 9 It is Figure 8 Another perspective schematic diagram of the assembled structure of a splicing component and a connecting member in;

[0060] Figure 10 It is Figure 8 An exploded structural schematic diagram of a splicing component and a connecting member in;

[0061] Figure 11 It is Figure 10 A structural schematic diagram of a connecting member in;

[0062] Figure 12 It is Figure 11 Another perspective schematic diagram of a connecting member in;

[0063] Figure 13 is Figure 12 an exploded structural schematic diagram of the connecting piece and the filling piece in

[0064] Figure 14 is Figure 10 a structural schematic diagram of a splicing component in

[0065] Figure 15 is Figure 14 an exploded structural schematic diagram of the splicing component in

[0066] Figure 16 is Figure 1 a structural schematic diagram of the support structure in

[0067] Figure 17 is Figure 1 a structural schematic diagram of the seat in

[0068] Figure 18 is Figure 17 a sectional schematic diagram of the seat in

[0069] Explanation of the reference numerals in the drawings:

[0070]

[0071]

[0072] The realization of the object of the present invention, its functional characteristics and advantages will be further described in conjunction with the embodiments and with reference to the accompanying drawings. Specific embodiments

[0073] Next, the technical solutions in the embodiments of the present application will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present application. Obviously, the described embodiments are only a part of the embodiments of the present application, rather than all of the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present application without creative efforts shall fall within the scope of protection of the present application.

[0074] It should be noted that all the directional indications (such as up, down, left, right, front, back...) in the embodiments of the present application are only used to explain the relative positional relationship and movement conditions between components in a specific posture (as shown in the drawings). If the specific posture changes, the directional indications will also change accordingly.

[0075] In this application, unless otherwise clearly defined and limited, terms such as "connection" and "fixation" shall be understood in a broad sense. For example, "fixation" can be a fixed connection, a detachable connection, or integrated; it can be a mechanical connection or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium, and it can be the communication inside two components or the interaction relationship between two components, unless otherwise clearly limited. For those of ordinary skill in the art, the specific meanings of the above terms in this application can be understood according to specific circumstances.

[0076] In addition, in this application, the descriptions involving "first", "second", etc. are only for descriptive purposes and cannot be understood as indicating or implying their relative importance or implicitly indicating the quantity of the indicated technical features. Thus, the features defined with "first" and "second" may explicitly or implicitly include at least one such feature. In addition, the meaning of "and / or" appearing throughout the text is that it includes three parallel solutions. Taking "A and / or B" as an example, it includes solution A, solution B, or the solution where both A and B are satisfied simultaneously. In addition, the technical solutions between various embodiments can be combined with each other, but it must be based on the ability of those of ordinary skill in the art to implement. When the combination of technical solutions results in contradictions or cannot be implemented, it should be considered that such a combination of technical solutions does not exist and is not within the scope of protection required by this application.

[0077] A cockpit, as the name implies, is an object that can be used for users to sit in. Currently, the volume of cockpits in related technologies is usually set relatively large, so that relatively large molds need to be used correspondingly during manufacturing. When the mold is relatively large in volume and complex in structure, its service life is relatively low and the cost is relatively high, which in turn leads to a relatively high manufacturing cost of the cockpit. At the same time, the integrally arranged cockpit also cannot meet the needs of cultivating users' hands-on ability and enhancing the interest.

[0078] Therefore, based on the above considerations, in order to solve the problems that the current manufacturing cost of the cockpit is relatively high and it cannot better meet some personalized needs of users, this application proposes a new type of cockpit. This cockpit innovatively sets multiple splicing components in a triangular shape to form a seating cavity and a communication port communicating with the seating cavity by splicing and enclosing the multiple splicing components. As a result, when manufacturing the cockpit, relatively simple-structured and relatively small-sized molds can be used correspondingly to reduce the manufacturing cost of the cockpit. At the same time, it is convenient for users to perform splicing and assembly, thus meeting the needs of cultivating users' hands-on ability and enhancing the interest.

[0079] Next, the structure of the cockpit proposed in this application will be explained and described by way of examples. In an embodiment of this application, please refer to Figures 1 to 5, the cockpit 100 proposed in this application includes a plurality of splicing components 10. The plurality of splicing components 10 are spliced and enclosed to form a seating cavity 11 and a communication port 12 communicating with the seating cavity 11. The shape of each splicing component 10 is triangular.

[0080] The splicing component 10, that is, an object that can be used for splicing, and then encloses to form a seating cavity 11 and a communication port 12 communicating with the seating cavity 11. Among them, the splicing components 10 can be spliced and enclosed to form a triangular prism structure, a cube structure, a cuboid structure, a near-spherical structure or an ellipsoidal structure composed of multiple faces. Of course, it can also be a combination of a conical structure 13 and an annular structure 14 introduced below. This application does not limit the structural shape formed by the splicing components 10. The communication port 12 can be arranged in a plane, and of course, it can also be arranged in an arc surface. This application does not limit the shape of the communication port 12. And the shape of each splicing component 10 is triangular, that is to say, the splicing component 10 can be an isosceles triangle as introduced below, and of course, it can also be a right triangle. Even further, a fillet is made at the corners (that is, the connection 15 between two adjacent sides of the splicing component 10. Since the splicing component 10 is triangular, each splicing component 10 has three corners). This application does not limit the type of the triangle of the splicing component 10. Moreover, the sizes of the splicing components 10 can be the same, of course, only some of them can be the same, or they can all be different. In addition, the splicing component 10 can also be a multi-layer structure including a mounting plate 16 and a sound-absorbing block 17 as introduced below. Of course, it can also be a single-layer structure. This application does not limit the structure of the splicing component 10. In addition, when the splicing components 10 are spliced, they can be connected and assembled through the connector 30 introduced below. Of course, the splicing components 10 can also be directly connected and assembled with each other.

[0081] The cockpit 100 of the technical solution of the present application is formed by splicing and enclosing a plurality of splicing components 10 to form a seating cavity 11 and a communication port 12 communicating with the seating cavity 11, so that each splicing component 10 can be separately and independently manufactured during manufacturing. At this time, the split splicing component 10 has a simpler structure and a relatively smaller volume compared to the cockpit 100 as a whole, and thus a mold with a relatively simple structure and a relatively smaller volume can be correspondingly used for production. And a mold with a relatively simple structure and a relatively smaller volume has a higher service life and a lower cost, and thus the manufacturing cost of the cockpit 100 can be relatively lower accordingly. That is to say, the structural optimization design of the cockpit 100 in this solution is beneficial to reducing the manufacturing cost of the cockpit 100. At the same time, it also provides a structural basis for the user to splice the cockpit 100. In this way, the user's hands-on ability can be cultivated and the interest can be enhanced, which is beneficial to improving the user's experience. Further, the splicing component 10 is set to be triangular, and the triangle is the simplest polygon, so that the splicing component 10 can be conveniently spliced into the cockpit 100 of the required shape. That is to say, the convenience and flexibility of splicing are improved, which is beneficial to further improving the user's experience.

[0082] Please refer to Figure 5 , in an embodiment of the present application, the shape of each splicing component 10 is an isosceles triangle, and the sizes of all the splicing components 10 are equal.

[0083] In this embodiment, the splicing component 10 is set to be an isosceles triangle, and the sizes of all the splicing components 10 are equal, which can make each splicing component 10 more regular, so as to facilitate the adaptive splicing between the subsequent splicing components 10, which is beneficial to improving the convenience of splicing.

[0084] Please refer to Figure 5 , in an embodiment of the present application, the shape of each splicing component 10 is an equilateral triangle.

[0085] In this embodiment, the splicing component 10 is further set to be an equilateral triangle, so that the three side lengths of the splicing component 10 are the same. In this way, when splicing through the splicing component 10, the directionality of the splicing component 10 does not need to be considered, which is beneficial to further improving the convenience of splicing.

[0086] Please refer to in combination Figures 4 to 7 , in an embodiment of the present application, some splicing components 10 enclose to form a conical structure 13 with one end open, and the conical structure 13 is formed by splicing and enclosing 4-6 splicing components 10.

[0087] In this embodiment, a conical structure 13 is formed by enclosing some splicing components 10, so that the space enclosed by the some splicing components 10 can be set to increase in the direction towards the user. In this way, the riding cavity 11 can have a relatively large volume to facilitate the subsequent riding of the user. On the other hand, it can also make the shape of the cockpit 100 more novel, giving the user a more attractive visual sense, enhancing the sense of ritual of use and being beneficial to improving the user experience. Further, the conical structure 13 includes 4-6 splicing components 10, which can ensure that the number of the splicing components 10 is not too small, so as to splice a riding cavity 11 with a suitable volume. At the same time, it also ensures that the number of the splicing components 10 is not too large, resulting in a more complex splicing process. That is to say, by setting the number of the splicing components 10 in the conical structure 13 in this way, the size of the enclosed riding cavity 11 and the convenience of splicing are taken into account. Among them, the number of the conical structures 13 can be one, and of course it can also be two or more. The application does not limit the number of the conical structures 13. In addition, the number of the splicing components 10 in the conical structure 13 can be 4, or 5 or 6, etc.

[0088] Please refer to Figures 4 to 7 , in an embodiment of the present application, some splicing components 10 enclose to form an annular structure 14 with both ends open, 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 enclose to form a riding cavity 11, and the end of the annular structure 14 away from the conical structure 13 encloses to form a communication port 12.

[0089] In this embodiment, an annular structure 14 is further provided at one end of the conical structure 13, which can further increase the volume of the riding cavity 11. At the same time, through the annular structure 14, it is also convenient to directly or indirectly provide a riding position for the user (when indirectly providing a riding position, a seat 70 can be further provided in the riding cavity 11 as introduced below), which further facilitates the riding of the user. At this time, such a setting can also further improve the novelty of the shape of the cockpit 100, further enhance the sense of ritual of use and be beneficial to improving the user experience.

[0090] In addition, it should be noted that in some embodiments, the number of conical structures 13 can also be two or more, and the structure formed by splicing and enclosing the remaining splicing components 10 except those enclosing to form the conical structure 13 may not be the annular structure 14 introduced above, but enclose to form other shaped structures. At this time, some of the remaining splicing components 10 can be arranged between the conical structures 13 and some are spliced with each other, so that the remaining splicing components 10 and the at least two conical structures 13 enclose to form a seating cavity 11, and at the same time, a communication port 12 is formed by enclosing the remaining splicing components 10. Or, in some embodiments, when the cockpit 100 includes multiple conical structures 13, any one conical structure 13 can be formed by splicing and enclosing the same number of splicing components 10. That is, the number of splicing components 10 in each conical structure 13 is the same. In this way, each conical structure 13 can be made more consistent, which is beneficial to improving the convenience of splicing. Or, at least two conical structures 13 are formed by splicing and enclosing different numbers of splicing components 10. That is, the number of splicing components 10 in each conical structure 13 is different, or only the number of splicing components 10 in some conical structures 13 is the same. In this way, the conical structures 13 can be more diversified, so as to splice into a more novel cockpit 100.

[0091] In an embodiment of the present application, it is defined that the number of splicing components 10 in the conical structure 13 is X, and the number of splicing components 10 in the annular structure 14 is Y, satisfying the relationship: Y = 2X.

[0092] In this embodiment, setting the number of splicing components 10 in the annular structure 14 to be twice the number of splicing components 10 in the conical structure 13 can facilitate the adaptive splicing of the annular structure 14 and the conical structure 13, and at the same time, the number of splicing components 10 in the annular structure 14 is not too large, which is beneficial to improving the convenience of splicing. Among them, the number of splicing components 10 in the conical structure 13 can be 5 as introduced below, and the number of splicing components 10 in the annular structure 14 can be correspondingly 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 correspondingly 12. In addition, the communication port 12 can correspond to an X-sided polygon.

[0093] In an embodiment of the present application, X = 5, Y = 10.

[0094] In this embodiment, setting the number of splicing components 10 in the conical structure 13 to be 5 and the number of splicing components 10 in the annular structure 14 to be 10 makes the communication port 12 correspondingly form a pentagonal shape. In this way, while ensuring that the seating cavity 11 has a relatively large volume, the number of splicing components 10 can be greatly simplified to improve the convenience of splicing them.

[0095] Please refer to Figure 8 , in an embodiment of the present application, the adjacent corners of the plurality of splicing components 10 are connected.

[0096] In this embodiment, connecting the adjacent corners of the splicing components 10 enables a connection position to connect multiple splicing components 10, which is conducive to improving the convenience of connecting the splicing components 10. Especially when using the connecting member 30 for connection and assembly as introduced below, the number of connecting members 30 can be further simplified. Of course, it should be noted that the present application is not limited thereto. In other embodiments, adjacent splicing components 10 can also be connected through adjacent side edges.

[0097] Please refer to in combination Figures 8 to 10 , in an embodiment of the present application, a position where the adjacent corners of the plurality of splicing components 10 are close to each other is defined as a connection part 15. The cockpit 100 further includes a plurality of connecting members 30. Each connecting member 30 is disposed at a connection part 15 and connects the corners of the plurality of splicing components 10 at the connection part 15.

[0098] In this embodiment, the connecting member 30 facilitates contact with the adjacent corners of the plurality of splicing components 10, thereby facilitating the connection and assembly of the adjacent plurality of splicing components 10. At the same time, such a setting also enables the adjacent splicing components 10 not to be stacked, which is more convenient for the cooperative arrangement between the splicing components 10.

[0099] Please refer to in combination Figure 10 and Figure 11 , in an 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. The number of connecting plates 33 is multiple. The multiple connecting plates 33 are all connected to the edge of the main body. Each corner of the splicing component 10 at the connection part 15 is correspondingly connected to a connecting plate 33.

[0100] In this embodiment, the connecting member 30 is set to include a main body plate 31 and a connecting plate 33. The main body plate 31 can connect the multiple connecting plates 33 so that the multiple connecting plates 33 can form a whole, which is convenient for taking and placing the whole connecting member 30 to improve the convenience of installation. Through the connecting plate 33, it can better correspond to the corners of each splicing component 10 to realize the connection between the connecting member 30 and the splicing component 10. Further, the connecting plate 33 is set as a flat plate so that the connecting plate 33 can be in good contact with the splicing component 10, which is conducive to improving the convenience and stability of the connection between the two. Among them, the connecting plate 33 can extend into the splicing component 10 as introduced below, or can also be stacked on the outside or inside of the splicing component 10.

[0101] Please refer to Figures 9 to 11 , in an embodiment of the present application, the adjacent corners of the plurality of splicing components 10 are spaced apart so that the main body plate 31 is exposed to the outside, and the main body plate 31 is a convex arc plate.

[0102] In this embodiment, the adjacent corners of the plurality of splicing components 10 are spaced apart and the main body plate 31 is exposed, so that the adjacent corners in the plurality of splicing components 10 do not form sharp corners when spliced. Especially when the main body plate 31 is set as a convex arc plate, a smooth curved surface can be formed at this place, so as to reduce the possibility of injury when the user collides with this place, thereby being beneficial to improving the safety of using the cockpit 100. At the same time, the main body plate 31 exposed to the outside and in the shape of a convex arc plate, in cooperation with the triangular shape of the splicing component 10, can also make the shape of the cockpit 100 more unique and novel, so as to further enhance the attractive effect of the cockpit 100 on the user's visual sense and enhance the usage ritual sense of the splicing component 10. In addition, setting the main body plate 31 as a convex arc plate can also facilitate the contact connection between the edge of the main body plate 31 and each connecting plate 33 arranged at intervals along the circumference of the main body plate 31. Among them, in order to improve the exposure effect of the main body plate 31, the corners of the splicing component 10 can be rounded. At the same time, such a setting can also reduce the possibility of being easily damaged by collision at the corners and avoid the possibility of stabbing the user, thereby being beneficial to improving the service life and usage safety of the splicing component 10.

[0103] Please refer to Figure 12 and Figure 13 , in an embodiment of the present application, the cockpit 100 further includes a plurality of filling members 40, and each filling member 40 is arranged inside the main body plate 31 of a connecting member 30, and the side of the filling member 40 facing away from the main body plate 31 is a plane.

[0104] In this embodiment, the inside of the main body plate 31 can be filled through the filling member 40, and the side of the filling member 40 facing away from the main body plate 31 is a plane, so that the inside of the cockpit 100 can also be relatively flat, so as to give the user a better visual sense and improve the competitiveness of the subsequent cockpit 100 in the market.

[0105] In an embodiment of the present application, the connecting plate 33 extends into the corner of the corresponding splicing component 10.

[0106] Please refer to Figure 8 and Figure 10, in this embodiment, the connecting plate 33 is inserted into the corner of the splicing component 10 for connection, which can increase the contact area between the two, and thus is beneficial to improving the splicing connection stability between the splicing components 10. At the same time, such a setting can also improve the compactness of the distribution between the connecting plate 33 and the splicing component 10. And the connecting plate 33 is hidden, which is convenient for both the outside and the inside of the splicing component 10 to be presented better, improving the visual sense effect by enhancing the consistency of the visual sense of various parts of the cockpit 100.

[0107] In an embodiment of the present application, the connecting plate 33 and the corner of the splicing component 10 are connected by screws.

[0108] In this embodiment, the connecting plate 33 and the splicing component 10 are connected by screws. The screw connection has the advantages of simplicity and reliability. Thus, while ensuring the connection stability between the connecting plate 33 and the splicing component 10, the connection process of the two can be simplified to improve the connection efficiency. Of course, it should be noted that the present application is not limited to this. In other embodiments, the connecting member 30 and the splicing component 10 can also be connected by snap connection or magnetic attraction connection, etc.

[0109] Please refer to Figure 11 , in an embodiment of the present application, the connecting member 30 further includes a plurality of first reinforcing plates 35. Each first reinforcing plate 35 connects the main body plate 31 and two adjacent connecting plates 33. The first reinforcing plate 35 is a convex arc-shaped plate.

[0110] In this embodiment, by connecting the main body plate 31 and two adjacent connecting plates 33 through the first reinforcing plate 35, the overall strength of the connecting member 30 can be enhanced, so that the connecting member 30 can more stably carry and connect the adjacent splicing components 10. At this time, the first reinforcing plate 35 can also block the position between the two corners of the two adjacent splicing components 10, which is beneficial to improving the sealing performance of the riding cavity 11.

[0111] Please refer to in combination Figure 14 and Figure 15 , in an embodiment of the present application, the splicing component 10 includes a mounting plate 16 and a sound-absorbing block 17. The sound-absorbing block 17 is arranged inside the mounting plate 16; at least one side of the mounting plate 16 facing the sound-absorbing block 17 is provided with a speaker 161, and the sound-absorbing block 17 is provided with an avoidance hole 18 corresponding to the position of the speaker 161.

[0112] In this embodiment, a speaker 161 is provided on at least one mounting plate 16, so that the cockpit 100 can provide users with more scenarios and a better sound experience (such as game music or movie music) through the speaker 161, which is conducive to further improving the user experience. The setting of the sound absorption block 17 can absorb the sound propagated along the radial direction of the speaker 161 by the speaker 161, reduce sound reflection, and is conducive to improving the sound emission effect of the speaker 161 along the axial direction of the speaker 161. Among them, the speaker 161 can be provided on the mounting plate 16 of only one splicing component 10, or of course, on the mounting plates 16 of two or more splicing components 10. In addition, setting the splicing components 10 to include the mounting plate 16 and the sound absorption block 17 can make the structural shapes of the splicing components 10 consistent, which is convenient for subsequent splicing between the splicing components 10 and improves the consistency of the visual sense given by each splicing component 10, thereby improving the visual sense effect. In addition, the material of the mounting plate 16 can be wood to reduce the absorption of the sound generated by the speaker 161 and further facilitate the sound emission of the speaker 161 along the axial direction of the speaker 161. At the same time, using wood for preparation can also make the cost of the mounting plate 16 relatively low. Of course, the material of the mounting plate 16 can also be plastic, and this application does not limit this. The sound absorption block 17 can be sponge, so that it is easy to obtain and has a low cost.

[0113] In an embodiment of the present application, the splicing component 10 further includes a protective net 19, and the protective net 19 is provided on the side of the sound absorption block 17 away from the mounting plate 16.

[0114] In this embodiment, the protective net 19 can cover the avoidance hole 18, reducing the possibility of dust and other particles entering the speaker 161 and causing damage to it, which is conducive to improving the service life of the speaker 161. In addition, through the cover of the protective net 19, the inner sides of the splicing component 10 provided with the speaker 161 and the splicing component 10 not provided with the speaker 161 can have a consistent appearance, thereby improving the visual sense effect inside the cockpit 100. Among them, the material of the protective net 19 can be cloth, so that it is easy to obtain and has a low cost, while improving the lightweight effect of the splicing component 10.

[0115] Please refer to Figure 15 In an embodiment of the present application, the splicing component 10 further includes a second reinforcing plate 20, and the second reinforcing plate 20 is provided on the side of the mounting plate 16 away from the sound absorption block 17.

[0116] In this embodiment, the second reinforcing plate 20 can enhance the overall strength of the splicing component 10, reduce the possibility of the splicing component 10 being damaged by collision, and thus contribute to improving the service life of the cockpit 100. Among them, the material of the second reinforcing plate 20 can be metal to enhance the strengthening effect on the strength of the splicing component 10. Of course, the second reinforcing plate 20 can also be plastic. In addition, the connecting plate 33 in the connecting member 30 introduced above can extend between the second reinforcing plate 20 and the mounting plate 16 and be connected to the relatively stronger second reinforcing plate 20 to enhance the connection stability between the connecting plate 33 and the splicing component 10. Of course, the connecting plate 33 can also be connected to the mounting plate 16, and this application does not limit this.

[0117] Please refer to Figure 15 , in an embodiment of the present application, the splicing component 10 further includes a decorative cover 21, and the decorative cover 21 is arranged on the side of the second reinforcing plate 20 facing away from the mounting plate 16.

[0118] In this embodiment, further, a decorative cover 21 is arranged on the outside of the second reinforcing plate 20, so that the decorative cover 21 can play a decorative role on the outside of the splicing component 10 to further improve the consistency of the appearance of the outside of each splicing component 10 and improve the visual sense effect of the cockpit 100. At the same time, the decorative cover 21 can also play a protective role.

[0119] In an embodiment of the present application, when the splicing component 10 includes the mounting plate 16, the sound-absorbing block 17, the protective net 19, the second reinforcing plate 20, and the decorative cover 21 introduced above, each of them can be triangular in shape. Of course, only the decorative cover 21 and the sound-absorbing block 17 can be triangular in shape. At this time, the decorative cover 21 can cover the outside of the second reinforcing plate 20, and the sound-absorbing block 17 can also cover the outside of the mounting plate 16.

[0120] Please refer to in combination Figure 1 and Figure 2 , in an embodiment of the present application, it is defined that the cockpit 100 has an up-down direction and a horizontal direction (the up-down direction and the horizontal direction defined when the cockpit 100 is in a normal use and placement state), and the communication port 12 is arranged to incline upwards; the cockpit 100 further includes a support structure 50, the support structure 50 is arranged on the lower surface of the lowermost splicing component 10, and the lower surface of the support structure 50 is a plane.

[0121] In this embodiment, the communication port 12 is arranged to tilt upward, which can reduce the obstruction to the user's head, thereby facilitating the user to get on and off the riding cavity 11, and further improving the user experience. At the same time, such an arrangement also facilitates the user's body to have a relatively corresponding viewing angle with the orientation of the communication port 12 when the user is sitting in the tilted riding cavity 11, so as to facilitate the user in the riding cavity 11 to have a wider viewing angle to the outside world. Further, a support structure 50 is arranged below the combined structure formed by splicing the splicing components 10, and the lower surface of the support structure 50 is also set as a plane, so that the cockpit 100 can be stably placed on a support surface such as the ground through the support structure 50. Among them, the support structure 50 can be in the structural form of the support frame 51 introduced below, and of course it can also be in the structural form of a support base. The present application does not limit the structural type of the support structure 50.

[0122] Please refer to Figure 2 , in an embodiment of the present application, the angle α formed by the plane where the communication port 12 is located and the up-down direction is defined, and the relationship is satisfied: 0° < α ≤ 30°.

[0123] In this embodiment, setting the angle α formed by the plane where the communication port 12 is located and the up-down direction to be between 0° and 30° can ensure that the tilt angle of the communication port 12 is not too large, so as to facilitate the user to enter smoothly and have a good viewing angle to the outside through the communication port 12 after riding. Among them, the angle α formed by the plane where the communication port 12 is located and the up-down 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 in the above range.

[0124] Please refer to Figure 2 , in an embodiment of the present application, it is defined that the cockpit 100 includes a front-back direction and a left-right direction in the horizontal direction. The communication port 12 is arranged on the front side of the cockpit 100. On a projection plane perpendicular to the left-right direction, the maximum projection distance of the cavity wall of the riding cavity 11 (in other words, the combined structure formed by splicing a plurality of splicing components 10) in the front-back direction is L1, and the maximum projection distance of the support structure 50 in the front-back direction is L2, and the relationship is satisfied: 0.8 ≤ L2 / L1 ≤ 1.

[0125] In this embodiment, the ratio of the maximum projection distance L2 of the support structure 50 in the front-back direction to the maximum projection distance L1 of the cavity wall of the riding cavity 11 in the front-back direction is set to be 0.8 to 1. On the one hand, it ensures that the maximum projection distance L2 of the support structure 50 in the front-back direction is not too small, which may affect the stability of the support for the combined structure formed by splicing multiple splicing components 10. On the other hand, it also ensures that the maximum projection distance L2 of the support structure 50 in the front-back direction is not too large, which may increase the overall volume of the cockpit 100 and thus increase the subsequent required occupied space. Therefore, setting L2 / L1 to 0.8 to 1 takes into account both the stability of the support for the combined structure formed by splicing multiple splicing components 10 and the compactness of the overall volume of the cockpit 100, so that users can sit stably in the cockpit 100 and it is convenient to place the cockpit 100 in a limited space. Among them, L2 / L1 can be 0.8, 0.85, 0.9, 0.95 or 1. Of course, it can also be any value within the above range. To achieve the same effect, in an embodiment of the present application, please refer to Figure 3 , it is defined that on a projection plane perpendicular to the front-back direction, the maximum projection distance of the cavity wall of the riding cavity 11 in the left-right direction is L3, and the maximum projection distance of the support structure 50 in the left-right direction is L4, satisfying the relationship: 0.65 ≤ L4 / L3 ≤ 0.85. Among them, the ratio of the maximum projection distance L4 of the support structure 50 in the left-right direction to the maximum projection distance L3 of the cavity wall of the riding cavity 11 in the left-right direction can be 0.65, 0.7, 0.75, 0.8 or 0.85. Of course, it can also be any value within the above range.

[0126] Please refer to in combination Figures 1 to 3 , and Figure 16 , in an embodiment of the present application, it is defined that the cockpit 100 includes a front-back direction and a left-right direction in the horizontal direction, and the communication port 12 is provided on the front side of the cockpit 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-right direction. The support frame 51 includes a support rod 511 and a connecting rod 513. The number of support rods 511 is two and they are arranged in sequence in the front-back direction. The opposite ends of the connecting rod 513 are respectively connected to the two support rods 511.

[0127] In this embodiment, the support structure 50 is set to 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 four support rods 511, the structure of the support structure 50 can be relatively simple, so as to improve the lightweight effect of the support structure 50 and at the same time reduce the raw materials required for manufacturing and thus reduce the manufacturing cost.

[0128] Please refer to Figure 16, in an embodiment of the present application, the distance between the two front-side support rods 511 in the two sets of support frames 51 is greater than the distance between the two rear-side support rods 511.

[0129] In this embodiment, the distance between the two front-side support rods 511 in the two sets of support frames 51 is set to be relatively large, and the center of gravity of the cockpit 100 is also arranged close to the front-side support rods 511. Therefore, at this time, the stability of the support for the cockpit 100 can be improved by the two support rods 511 with a larger distance.

[0130] Please refer to Figure 16 , in an embodiment of the present application, define the distance between the two front-side support rods 511 in the two sets of support frames 51 as D1, and the distance between the two rear-side support rods 511 as D2, satisfying the relationship: 0.5 ≤ D2 / D1 ≤ 0.7.

[0131] In this embodiment, setting the ratio of the distance D2 between the two rear-side support rods 511 to the distance D1 between the two front-side support rods 511 to be 0.5 to 0.7 can prevent the distance D2 between the two rear-side support rods 511 from being too small, which may affect the stability of the support of the support structure 50. At the same time, it also prevents the distance D2 between the two rear-side support rods 511 from being too large, which may cause excessive space occupation. Therefore, setting the ratio range of the distance D2 between the two rear-side support rods 511 to the distance D1 between the two front-side support rods 511 in this way takes into account both the stability of the support of the support structure 50 and the compactness of the structure. Among them, the ratio of the distance D2 between the two rear-side support rods 511 to the distance D1 between the two front-side support rods 511 can be 0.5, 0.55, 0.6, 0.65 or 0.7. Of course, it can also be any value within the above range.

[0132] Please refer to Figure 16 , in an embodiment of the present application, the connecting rod 513 includes a first section 515 and a second section 517 that are connected and arranged at an angle. The ends of the first section 515 and the second section 517 that are away from each other are respectively connected to the two support rods 511. The angle formed by the first section 515 and the second section 517 of the connecting rod 513 in one set of support frames 51 and the angle formed by the first section 515 and the second section 517 of the connecting rod 513 in the other set of support frames 51 are arranged back to back.

[0133] In this embodiment, the connecting rod 513 is set to include a first body 515 and a second body 517 that form an angle, and the angles formed by the two connecting rods 513 are arranged back to back, which can make the two connecting rods 513 more compactly distributed. At the same time, such a setting can also provide a more suitable abutting support for the triangular splicing component 10. For example, the two sides of the triangular splicing component 10 can be abutted and supported by the first body 515 of the two connecting rods 513.

[0134] Please refer to Figure 16 , in an embodiment of the present application, the support structure 50 further includes a fixing plate 53. The fixing plate 53 is connected to two sets of support frames 51, and the fixing plate 53 is also connected to the lowermost splicing component 10.

[0135] In this embodiment, the setting of the fixing plate 53 can, on the one hand, be used for adapting to abut against the splicing component 10, which is conducive to 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 an integral body, so as to be able to complete the installation of the two sets of support frames 51 at one time and improve the installation convenience.

[0136] Please refer to in combination Figure 1 and Figure 3 , in an embodiment of the present application, the cockpit 100 further includes a seat 70, and the seat 70 is arranged in the riding cavity 11.

[0137] In this embodiment, by setting the seat 70, a more comfortable seating position can be provided for the user, which is conducive to improving the comfort of the user when riding in the cockpit 100 and further enhancing the user experience. Among them, the seat 70 can be connected to the upper surface of the lowermost splicing component 10. At this time, this splicing component 10 can be set the same as other splicing components 10, and all include a mounting plate 16, a sound-absorbing block 17, a protective net 19, a second reinforcing plate 20, and a decorative cover 21. Of course, it can also be set differently from other splicing components 10, and only include the second reinforcing plate 20 and the decorative cover 21, so as not to cause excessive thickness at this place after being connected to the seat 70.

[0138] Please refer to Figure 17 , in an embodiment of the present application, the seat 70 includes a seat cushion portion 71, a backrest portion 73, and a headrest portion 75; the backrest portion 73 protrudes from the edge of the seat cushion portion 71; the headrest portion 75 is connected to one end of the backrest portion 73 away from the seat cushion portion 71.

[0139] In this embodiment, the seat 70 is provided to include a seat cushion portion 71, a backrest portion 73, and a headrest portion 75, such that the seat cushion portion 71 can be used for sitting, the backrest portion 73 can be used for reclining, and the headrest portion 75 can be used for abutting and supporting the user's head. In this way, the seat 70 can provide good abutting and support for various parts of the user, which is conducive to improving the comfort of the user when sitting. Further, please refer to Figure 18 , in order to facilitate the user to sit more comfortably on the seat 70 with a tilted body posture, it is defined that the seat cushion portion 71 has a seating surface 711, and the seating surface 711 can be a convex arc surface; it is defined that the backrest portion 73 has a backrest surface 731, and the backrest surface 731 can include a connected first surface 733 and a second surface 735. The first surface 733 is disposed closer to the seat cushion portion 71 than the second surface 735. The first surface 733 is a concave arc surface, and the second surface 735 is a convex arc surface; it is defined that the headrest portion 75 has a headrest surface 751, and the headrest surface 751 can be a convex arc surface.

[0140] Please refer to in combination Figure 1 and Figure 2 , in an embodiment of the present application, one end of the seat cushion portion 71 away from the backrest portion 73 extends out from the communication port 12.

[0141] In this embodiment, one end of the seat cushion portion 71 away from the backrest portion 73 protrudes from the communication port 12, such that when the user is sitting in the cockpit 100, the joint 15 between the user's thigh and calf can be lapped on the seat cushion portion 71, avoiding being squeezed by the edge of the communication port 12 to generate a sense of oppression, thereby being conducive to further improving the comfort of sitting and further enhancing the user's experience.

[0142] The present application also proposes an entertainment system, which includes a cockpit 100. The specific structure of the cockpit 100 refers to the above embodiment. Since this entertainment system adopts all the technical solutions of the above embodiments, it at least has all the beneficial effects brought by the technical solutions of the above embodiments, and will not be elaborated here one by one. Among them, the entertainment system can 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 can also include a projector. At this time, the user can watch the movie projected by the projector while sitting in the cockpit 100.

[0143] The above are only the preferred embodiments of the present application, and do not limit the patent scope of the present application accordingly. Any equivalent structural transformation made using the content of the specification and drawings of the present application under the inventive concept of the present application, or any direct / indirect application in other related technical fields is 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, and the relationship is satisfied: 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 splicing components with different numbers.

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, wherein, 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 at the 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 at 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, characterized in that, 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 groups of support frames, the two groups 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, characterized in that, The distance between the two support rods located on the front side in the two groups of support frames is greater than the distance between the two support rods located on the rear side.

22. The cockpit according to claim 21, characterized in that, Define the distance between the two support rods located on the front side in the two groups of support frames as D1, and the distance between the two support rods located on the rear side as D2, and satisfy the relationship: 0.5 ≤ D2 / D1 ≤ 0.7; And / or, the connecting rod includes a first section body and a second section body that are connected and arranged at an angle, the ends of the first section body and the second section body that are away from each other are respectively connected to the two support rods, and the included angle formed by the first section body and the second section body of the connecting rod in one group of support frames and the included angle formed by the first section body and the second section body of the connecting rod in the other group 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 groups 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 cushion part; A backrest part, the backrest part protrudes from the edge of the cushion part; and A headrest part, the headrest part is connected to the end of the backrest part away from the cushion part.

26. The cockpit according to claim 25, wherein The end of the cushion part away from the backrest part extends out from the communication port; And / or, the 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 connected first surface and a second surface, the first surface is arranged closer to the 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 according to any one of claims 1 to 26.

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