Cabin and entertainment system

Abstract

The invention discloses a cabin and an entertainment system. The cabin comprises a plurality of splicing assemblies and an atmosphere lamp. The multiple splicing assemblies are spliced to define a sitting cavity and a communicating opening communicating with the sitting cavity, and each splicing assembly is in a triangular shape; every two adjacent splicing assemblies are arranged at an included angle and define a gap communicating with the riding cavity, and the atmosphere lamp is arranged in at least one gap. 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 relates to a cockpit and an entertainment system applying the cockpit. Background Art

[0002] At present, 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:

[0005] A plurality of splicing components, 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 splicing component is triangular; and

[0006] An ambient light, two adjacent splicing components are arranged at an angle and enclose a gap communicating with the riding cavity, and at least one of the gaps is provided with the ambient light.

[0007] Optionally, the ambient light includes:

[0008] A carrier, the carrier is connected to the splicing component and extends along the extending direction of the gap; and

[0009] A plurality of light sources, the plurality of light sources are all arranged on the carrier and are sequentially arranged along the extending direction of the carrier, and the plurality of light sources can all emit light towards the inner side of the riding cavity.

[0010] Optionally, the ambient light further includes a light guide member, the light guide member is arranged on the carrier and encloses an installation cavity with the carrier, and the plurality of light sources are all arranged in the installation cavity.

[0011] Optionally, the carrier is provided with an installation groove, the notch of the installation groove faces the inner side of the riding cavity, the light guide member covers the notch of the installation groove and encloses the installation cavity with the installation groove.

[0012] Optionally, clamping grooves are arranged on the inner sides of the two groove walls of the installation groove parallel to the extending direction of the carrier, and the two sides of the light guide member are respectively clamped in the two clamping grooves;

[0013] And / or, the installation groove penetrates through the opposite sides in the extending direction of the carrier;

[0014] And / or, multiple said light sources are installed on the groove wall of the installation groove facing its notch;

[0015] And / or, multiple said light sources and the light guide member are arranged at intervals.

[0016] Optionally, mounting plates protrude from opposite sides of the carrier member to respectively extend into two adjacent splicing components and be connected to the two adjacent splicing components.

[0017] Optionally, the mounting plate includes a first plate body and a second plate body that are connected and arranged at an angle, and one end of the first plate body far from the second plate body is connected to the carrier member;

[0018] The second plate body is parallel to the plane where the corresponding splicing component is located, the second plate body extends into the corresponding splicing component and is connected to the splicing component.

[0019] Optionally, the atmosphere lamp further includes a lamp board, the lamp board is arranged on the carrier member, and multiple said light sources are all arranged on the lamp board;

[0020] And / or, the light source is an LED lamp bead.

[0021] Optionally, one side of the atmosphere lamp close to the inner side of the riding cavity abuts against two adjacent splicing components.

[0022] Optionally, two adjacent splicing components are arranged at intervals to enclose and form the gap communicating with the outside;

[0023] The cockpit further includes a covering member, the covering member is arranged in the gap and is located on one side of the atmosphere lamp facing the outside of the riding cavity, and the covering member extends along the direction of the gap.

[0024] Optionally, the covering member and the atmosphere lamp are arranged at intervals.

[0025] Optionally, define the position where the corners of multiple adjacent splicing components are close to each other as the connection part, and the cockpit further includes multiple connecting members;

[0026] Each connecting member is arranged at one connection part and connects the corners of multiple splicing components at the connection part, and opposite ends of the covering member in the extending direction of the gap respectively abut against two connecting members.

[0027] Optionally, the covering member includes a middle plate body and two edge plate bodies, the two edge plate bodies are respectively connected to opposite sides of the middle plate body, and opposite ends of the edge plate bodies and the middle plate body in the extending direction of the gap respectively abut against two connecting members;

[0028] The two edge plates respectively extend into two adjacent splicing components and are connected to the two adjacent splicing components, and the edge plates are also parallel to the plane where the corresponding splicing components are located.

[0029] Optionally, the connecting member includes:

[0030] A main body plate;

[0031] A plurality of connecting plates, the plurality of connecting plates are all connected to the edge of the main body, and each corner of each splicing component at the connection is correspondingly connected to one connecting plate. The connecting plate is parallel to the plane where the corresponding splicing component is located, and the edge plate abuts against the connecting plate; and

[0032] A plurality of reinforcing plates, each reinforcing plate connects the main body plate and two adjacent connecting plates, and the intermediate plate abuts against the reinforcing plate.

[0033] Optionally, both the intermediate plate and the reinforcing plate are outwardly convex arc-shaped plates, and the axis of the intermediate plate coincides with the axis of the reinforcing plate, and the main body plate is an outwardly convex arc-shaped plate.

[0034] Optionally, the cockpit further includes a camera module, and the camera module is arranged inside the riding cavity.

[0035] Optionally, a receiving groove is provided on one side of the splicing component facing the inner side of the riding cavity, the camera module is arranged in the receiving groove, and the camera module includes a module housing and a camera arranged in the module housing;

[0036] The cockpit further includes a driving component, and the driving component is used to drive the camera module to rotate so that the module housing covers the notch of the receiving groove, or the camera is exposed from the notch of the receiving groove.

[0037] Optionally, the cockpit further includes a wireless charging module, and the wireless charging module is arranged on the splicing component.

[0038] Optionally, a placement groove is provided on one side of the splicing component facing the inner side of the riding cavity, and the wireless charging module is embedded in the bottom wall of the placement groove;

[0039] And / or, the number of the wireless charging modules is at least two. It is defined that the cockpit has a front-back direction and a left-right direction. The communication port is arranged on the front side of the cockpit, and at least two wireless charging modules are respectively arranged in the splicing components on the left and right sides.

[0040] Optionally, the cockpit further includes a reading lamp, and the reading lamp is arranged in the riding cavity;

[0041] And / or, the cockpit further includes a speaker, the speaker is disposed within the splicing assembly, and the splicing assembly is provided with a sound outlet communicating with the riding cavity at a position corresponding to the speaker;

[0042] And / or, the cockpit further includes a seat, and the seat is disposed within the riding cavity;

[0043] And / or, it is defined that the cockpit has an up-down direction and a horizontal direction, and the communication port is inclined upward; the cockpit further includes a support structure, the support structure is disposed on the lower surface of the lowermost splicing assembly, and the lower surface of the support structure is a plane;

[0044] And / or, a part of the splicing assemblies enclose to form a conical structure with one end being open, and the conical structure is formed by splicing and enclosing 4-6 splicing assemblies;

[0045] And / or, the shape of each splicing assembly is an equilateral triangle, and the sizes of all the splicing assemblies are equal;

[0046] And / or, the cockpit further includes a fan module, the fan module is disposed within the riding cavity, and the splicing assembly is provided with an air inlet corresponding to the fan module.

[0047] The present invention further provides an entertainment system, including the cockpit as described above.

[0048] The cockpit of the technical solution of the present invention is formed by splicing and enclosing a plurality of splicing components to form a seating cavity and a communication port communicating with the seating 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. Molds with relatively simple structures and relatively small volumes have a higher service life and lower costs, and thus the manufacturing cost of the cockpit can be relatively low accordingly. That is to say, the optimized design of the structure of the cockpit in this solution is conducive 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 conducive to improving users' usage experience. Further, the splicing components are set as triangles, and triangles are the simplest polygons, so that it is convenient to splice 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 conducive to further improving users' usage experience. And again, an atmosphere lamp is provided in the gap formed by the adjacent splicing components arranged at an angle to enclose and communicate with the seating cavity, which can improve the sense of ceremony during use, and thus is also conducive to improving users' usage experience. That is to say, the structural setting of the cockpit in this solution greatly improves the usage experience by providing a structural basis for splicing and assembling, being portable and flexible during splicing and assembling, and having a high sense of ceremony during use. BRIEF DESCRIPTION OF THE DRAWINGS

[0049] 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 use in the description of the embodiments or the prior art. Obviously, the following drawings 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.

[0050] Figure 1 Structural schematic diagram of an embodiment of the cockpit of the present invention;

[0051] Figure 2 is Figure 1 Another perspective schematic diagram of the cockpit in;

[0052] Figure 3 is Figure 1 Another perspective schematic diagram of the cockpit in;

[0053] Figure 4 is Figure 1 Another perspective schematic diagram of the cockpit in;

[0054] Figure 5 is Figure 1 A partial structural schematic diagram of the cockpit in;

[0055] Figure 6 is Figure 5 Another perspective schematic diagram of the partial structure of the middle cockpit;

[0056] Figure 7 is Figure 6 An exploded structure schematic diagram of the partial structure of the middle cockpit;

[0057] Figure 8 is Figure 7 Another perspective schematic diagram of the exploded structure of the partial structure of the middle cockpit;

[0058] Figure 9 is Figure 1 Another schematic diagram of the partial structure of the middle cockpit;

[0059] Figure 10 is Figure 9 Another perspective schematic diagram of the partial structure of the middle cockpit;

[0060] Figure 11 is Figure 10 An exploded structure schematic diagram of the partial structure of the middle cockpit;

[0061] Figure 12 Schematic diagram of the assembled structure of the splicing component, covering component and atmosphere light;

[0062] Figure 13 is Figure 12 Exploded structure schematic diagram of the splicing component, covering component and atmosphere light;

[0063] Figure 14 is Figure 12 An exploded structure schematic diagram of the atmosphere light;

[0064] Figure 15 is Figure 11 Schematic diagram of the structure of the connecting piece in;

[0065] Figure 16 is Figure 15 Another perspective schematic diagram of the connecting piece in;

[0066] Figure 17 is Figure 16 An exploded structure schematic diagram of the connecting piece and filling piece in;

[0067] Figure 18 is Figure 1 Schematic diagram of the structure of the support structure in;

[0068] Figure 19 is Figure 1 Schematic diagram of the structure of the seat in;

[0069] Figure 20 isFigure 19 A schematic cross-sectional view of a middle seat;

[0070] Figure 21 It is a schematic cross-sectional view of a splicing component.

[0071] Explanation of the reference numerals in the drawings:

[0072]

[0073]

[0074] The realization, functional features and advantages of the object of the present invention will be further described in conjunction with the embodiments with reference to the accompanying drawings. Specific embodiments

[0075] 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 the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the scope of protection of the present application.

[0076] It should be noted that all directional indications (such as up, down, left, right, front, back...) in the embodiments of the present application are only used to explain the relative position relationship and movement conditions between components in a specific posture (as shown in the accompanying drawings). If the specific posture changes, the directional indications will also change accordingly.

[0077] In the present application, unless otherwise clearly defined and limited, the terms "connection", "fixation", etc. should 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 the present application can be understood according to specific situations.

[0078] In addition, the descriptions involving "first", "second", etc. in this application are for descriptive purposes only, and should not be construed as indicating or implying their relative importance or implicitly specifying 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 scenarios. Taking "A and / or B" as an example, it includes scenario A, or scenario B, or the scenario 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 inability to implement, 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.

[0079] A cockpit, as the name implies, is an object that can be used for users to sit on. Currently, the volume of cockpits in related technologies is usually set 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 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 cannot meet the needs of cultivating users' hands-on ability and enhancing the fun.

[0080] 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 the shape of triangles, so as to form a seating cavity and a communication port communicating with the seating cavity by splicing and enclosing the multiple splicing components. Furthermore, when manufacturing the cockpit, relatively simple-structured and relatively small-sized molds can be correspondingly used to reduce the manufacturing cost of the cockpit. At the same time, it is convenient for users to splice and assemble, thus meeting the needs of cultivating users' hands-on ability and enhancing the fun. And further, an atmosphere light is arranged in the gap formed by adjacent splicing components enclosing the communicating seating cavity to improve the sense of ceremony during subsequent use and enhance the user experience.

[0081] Next, the structure of the cockpit proposed in this application will be unlocked and described with embodiments. In an embodiment of this application, please refer to Figure 1 , Figure 5 , Figure 7 , Figure 10 and Figure 11 , the cockpit 100 proposed in this application includes multiple splicing components 10 and an atmosphere light 20. The multiple 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; two adjacent splicing components 10 are arranged at an angle and enclose to form a gap 13 communicating with the seating cavity 11, and at least one gap 13 is provided with an atmosphere light 20.

[0082] The splicing component 10, which is an object that can be used for splicing, and then encloses to form a riding cavity 11 and a connecting opening 12 that connects the riding cavity 11. Among them, the splicing component 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 the conical structure 18 and the annular structure 19 introduced below. The present application does not limit the structural shape formed by the splicing component 10. The connecting opening 12 can be arranged in a plane, and of course, it can also be arranged in an arc surface. The present application does not limit the shape of the connecting opening 12 either. And the shape of each splicing component 10 is a triangle, 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, fillets are made at the corners (that is, the connection 14 between two adjacent sides of the splicing component 10. Since the splicing component 10 is a triangle, each splicing component 10 has three corners). The present 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 multiple stacked plates, and of course, it can also be a single-layer structure including a single plate. The present application does not limit the structural type of the splicing component 10. In addition, when the splicing components 10 are spliced, they can be connected and assembled through the connecting piece 30 introduced below, or the splicing components 10 can be directly connected and assembled with each other.

[0083] The ambient light 20 can be disposed within the gap 13 formed by enclosing two adjacent splicing components 10, so as to emit light inside the cockpit 100 to enhance the sense of ceremony when using the cockpit 100. Among them, since the two adjacent splicing components 10 are arranged at an angle, the gap 13 formed by enclosing the two splicing components 10 can be only communicated with the riding cavity 11, that is, the two adjacent side edges of the two splicing components 10 are abutted on the outer side facing the riding cavity 11. Of course, the two splicing components 10 can also be arranged at intervals, so that the gap 13 formed by enclosing the two splicing components 10 is communicated with both the riding cavity 11 and the outside (i.e., the outside of the cockpit 100). In addition, an ambient light 20 can be disposed in each gap 13. Of course, it is also possible that only some of the gaps 13 are provided with the ambient light 20. For example, the ambient light 20 is only disposed in the gaps 13 in areas such as the top and side of the riding cavity 11 that are easily observed by the user. In addition, the working mode of the ambient light 20 can be a constant-on mode, a breathing light mode, or a running light mode, etc., and the present application does not limit the working mode of the ambient light 20. In addition, the ambient light 20 can be of the LED lamp type, and of course it can also be a fluorescent lamp, and the present application does not limit the type of the ambient light 20. The installation method of the ambient light 20 can also be any connection method such as screw connection, snap connection, or adhesive connection, as long as the ambient light 20 can be installed and fixed in the gap 13.

[0084] The cockpit 100 of the technical solution of this 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, compared with the overall cockpit 100, the split splicing components 10 have a simpler structure and a relatively smaller volume, so that molds with a relatively simple structure and a relatively smaller volume can be correspondingly used for production. And molds with a relatively simple structure and a relatively smaller volume have a higher service life and a lower cost, so that the manufacturing cost of the cockpit 100 can be relatively lower accordingly. That is, 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 users to splice the cockpit 100. In this way, it can cultivate the user's hands-on ability and enhance the interest, which is beneficial to improving the user's use experience. Further, the splicing component 10 is set as a triangle, and the triangle is the simplest polygon, so that it is convenient to splice the splicing component 10 into the cockpit 100 of the required shape. That is, it improves the convenience and flexibility of splicing, which is beneficial to further improving the user's use experience. And again, an ambient light 20 is provided in the gap 13 formed by the adjacent splicing components 10 at an included angle to enclose the seating cavity 11, which can improve the sense of ceremony during use, and is also beneficial to improving the user's use experience. That is, the structural setting of the cockpit 100 in this solution greatly improves the use experience in three aspects: giving a structural basis for splicing and assembling, being portable and flexible during splicing and assembling, and having a high sense of ceremony during use.

[0085] Please refer to Figures 1 to 6 , in an embodiment of this application, the shapes of the splicing components 10 are all isosceles triangles, and the sizes of the splicing components 10 are equal.

[0086] In this embodiment, setting the splicing component 10 as an isosceles triangle and the sizes of the splicing components 10 being equal can make each splicing component 10 more regular, so as to facilitate the adaptation and splicing between the subsequent splicing components 10, which is beneficial to improving the convenience and flexibility of splicing.

[0087] Please refer to Figure 6 , in an embodiment of this application, the shapes of the splicing components 10 are all equilateral triangles.

[0088] In this embodiment, further setting the splicing component 10 as an equilateral triangle makes the three side lengths of the splicing component 10 the same. In this way, when splicing through the splicing component 10, there is no need to consider the directionality of the splicing component 10, which is beneficial to further improving the convenience and flexibility of splicing.

[0089] Please refer to Figure 6and Figure 8 , in an embodiment of the present application, a part of the splicing components 10 enclose to form a conical structure 18 with one end being open, and the conical structure 18 is formed by splicing and enclosing 4-6 splicing components 10.

[0090] In this embodiment, by enclosing the conical structure 18 with a part of the splicing components 10, the space enclosed by the part of the 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 thus being beneficial to improving the user experience. Further, the conical structure 18 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 18 in this way, both 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 18 can be one, and of course it can also be two or more. The present application does not limit the number of the conical structures 18. In addition, the number of the splicing components 10 in the conical structure 18 can be 4, or 5 or 6, etc.

[0091] Please refer to Figure 6 and Figure 8 , in an embodiment of the present application, a part of the splicing components 10 enclose to form an annular structure 19 with both ends being open, and one end of the annular structure 19 is connected to the open end of the conical structure 18; the annular structure 19 and the conical structure 18 enclose to form the riding cavity 11, and the end of the annular structure 19 away from the conical structure 18 encloses to form a communication port 12.

[0092] In this embodiment, by further setting the annular structure 19 at one end of the conical structure 18, the volume of the riding cavity 11 can be further increased. At the same time, through the annular structure 19, 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), further facilitating the riding of the user. At this time, by setting it in this way, the novelty of the shape of the cockpit 100 can be further improved, and the sense of ritual of use can be further enhanced, which is beneficial to improving the user experience.

[0093] In addition, it should be noted that in some embodiments, the number of conical structures 18 can also be two or more. The structure formed by splicing and enclosing the remaining splicing components 10 except those enclosing to form the conical structure 18 may not be the annular structure 19 introduced above, but other shaped structures. At this time, some of the remaining splicing components 10 can be arranged between the conical structures 18 and some can be spliced with each other, so that the remaining splicing components 10 and the at least two conical structures 18 enclose to form a riding 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 18, any one of the conical structures 18 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 18 is the same. In this way, each conical structure 18 can be made more consistent, which is beneficial to improving the convenience of splicing. Or, at least two conical structures 18 are formed by splicing and enclosing different numbers of splicing components 10. That is, the number of splicing components 10 in each conical structure 18 is different, or only the number of splicing components 10 in some conical structures 18 is the same. In this way, the conical structures 18 can be made more diverse, so as to splice into a more novel cockpit 100.

[0094] Please refer to Figure 8 , in an embodiment of the present application, the number of splicing components 10 in the conical structure 18 is defined as X, and the number of splicing components 10 in the annular structure 19 is defined as Y, satisfying the relationship: Y = 2X.

[0095] In this embodiment, setting the number of splicing components 10 in the annular structure 19 to be twice the number of splicing components 10 in the conical structure 18 can facilitate the adaptation and splicing of the annular structure 19 and the conical structure 18. At the same time, the number of splicing components 10 in the annular structure 19 is not excessive, which is beneficial to improving the convenience of splicing. Among them, the number of splicing components 10 in the conical structure 18 can be 5 as introduced below, and the number of splicing components 10 in the annular structure 19 can be correspondingly 10. Of course, the number of splicing components 10 in the conical structure 18 can also be 6, and the number of splicing components 10 in the annular structure 19 can be correspondingly 12. In addition, the communication port 12 can correspond to an X-sided polygon.

[0096] Please refer to Figure 8 , in an embodiment of the present application, X = 5, Y = 10.

[0097] In this embodiment, the number of splicing components 10 in the conical structure 18 is set to 5, and the number of splicing components 10 in the annular structure 19 is set to 10, so that the communication ports 12 correspondingly form a pentagonal shape. In this way, while ensuring that the riding cavity 11 has a relatively large volume, the number of splicing components 10 can be greatly simplified to improve the convenience of splicing them.

[0098] Please refer to Figures 9 to 14 , in an embodiment of the present application, the ambient light 20 includes a carrier 21 and a plurality of light sources 23. The carrier 21 is connected to the splicing component 10 and extends along the extension direction of the gap 13; the plurality of light sources 23 are all arranged on the carrier 21 and are arranged in sequence along the extension direction of the carrier 21, and the plurality of light sources 23 can all emit light toward the inside of the riding cavity 11.

[0099] The carrier 21, as the name implies, is an object that can be used to carry the light source 23. Among them, the carrier 21 can be a plate structure, and of course it can also be a cover structure, or a seat structure, etc. The present application does not limit the structural type of the carrier 21. The light source 23 is a device that can emit light after being powered on.

[0100] In this embodiment, the ambient light 20 is set to include a carrier 21 and a plurality of light sources 23, so that the plurality of light sources 23 can emit light, which is conducive to improving the lighting effect of the ambient light 20. On the other hand, the plurality of light sources 23 can be installed on the carrier 21, and after they are assembled into a whole, they can be installed into the gap 13 at one time, which is conducive to improving the convenience of installing the plurality of light sources 23 in the gap 13.

[0101] Please refer to Figure 14 , in an embodiment of the present application, the ambient light 20 further includes a light guide member 24. The light guide member 24 is arranged on the carrier 21 and encloses an installation cavity 241 with the carrier 21, and the plurality of light sources 23 are all arranged in the installation cavity 241.

[0102] In this embodiment, the setting of the light guide member 24 can play a role in transitional diffusion of the light emitted by the light source 23, so that after the light is diffusely reflected in the light guide member 24, the "point light source 23" is transformed into a "surface light source 23", so that the ambient light 20 can emit light more evenly and improve the lighting effect of the ambient light 20. Further enhance the user experience. In addition, the light guide member 24 and the carrier 21 can enclose an installation cavity 241, so that the light source 23 can be installed in a hidden manner, realizing an isolation and protection effect on the light source 23, and thus being able to reduce the possibility of damage to the light source 23 and improve the service life.

[0103] Please refer to Figure 14, in an embodiment of the present application, the carrier 21 is provided with an installation groove 211, the notch of the installation groove 211 faces the inner side of the riding cavity 11, the light guide member 24 covers the notch of the installation groove 211, and together with the installation groove 211, an installation cavity 241 is formed.

[0104] In this embodiment, by providing the installation groove 211 on the carrier 21, the light guide member 24 can be set as a plate structure, and together with the installation groove 211 on the carrier 21, an installation cavity 241 can be formed. At this time, the light guide member 24 can be disposed opposite to a plurality of light sources 23, so that each area of the light guide member 24 can uniformly receive the light emitted by the light sources 23, thereby improving the light homogenization effect of the light guide member 24. At the same time, such a setting also makes the structure of the light guide member 24 relatively simple, which is conducive to improving the convenience of manufacturing it. Of course, in other embodiments, the light guide member 24 can also be a cover structure and cover the outside of a plurality of light sources 23.

[0105] Please refer to Figure 14 , in an embodiment of the present application, clamping grooves 212 are provided on the inner sides of two groove walls of the installation groove 211 parallel to the extending direction of the carrier 21, and two opposite sides of the light guide member 24 are respectively clamped in the two clamping grooves 212.

[0106] In this embodiment, setting the light guide member 24 to be clamped and fixed with the clamping grooves 212 on the groove wall of the installation groove 211 can make the connection method between the light guide member 24 and the carrier 21 relatively simple, which is conducive to improving the convenience of connecting and assembling the light guide member 24 and the carrier 21. Moreover, at this time, it is also unnecessary to provide a connection structure on the light guide member 24, which is conducive to protecting the structure of the light guide member 24 itself to ensure the light guide effect and improving the convenience of manufacturing the light guide member 24. At the same time, the structure of the clamping groove 212 is also relatively simple, so that the structure of the carrier 21 will not be too complex, which is conducive to improving the convenience of manufacturing the carrier 21.

[0107] Please refer to Figure 14 , in an embodiment of the present application, the installation groove 211 penetrates through opposite sides in the extending direction of the carrier 21.

[0108] In this embodiment, making the installation groove 211 penetrate through both sides in the extending direction of the carrier 21, on the one hand, when processing the installation groove 211, it can be directly processed from one side to the other side in the extending direction of the carrier 21 without considering the processing size, which is conducive to improving the convenience of processing and forming the installation groove 211. On the other hand, it also enables the light guide member 24 to be inserted and installed from an opening of the installation groove 211 in the extending direction of the carrier 21 when installing the light guide member 24, which is conducive to further improving the convenience of installing the light guide member 24 on the carrier 21.

[0109] Please refer to Figure 14 , in an embodiment of the present application, a plurality of light sources 23 are installed on the groove wall of the installation groove 211 facing its notch.

[0110] In this embodiment, installing the light source 23 on the groove wall of the installation groove 211 facing its notch can facilitate the setting of connection structures on the groove wall to install a plurality of light sources 23, which is conducive to improving the convenience of installing the light source 23.

[0111] Please refer to in combination with Figure 11 and Figure 14 , in an embodiment of the present application, a plurality of light sources 23 and the light guide member 24 are arranged at intervals.

[0112] In this embodiment, setting an interval between the light source 23 and the light guide member 24 can facilitate the light emitted by the light source 23 to irradiate the light guide member 24 with a larger irradiation angle, so as to increase the light receiving area of the light guide member 24 and improve the subsequent light emitting effect. On the other hand, it also enables a heat dissipation gap to be formed at this place. Especially when cooperating with the relative two sides in the extending direction of the installation groove 211 penetrating the carrier 21, it is more convenient for the heat generated by the light source 23 during operation to be effectively discharged to the outside of the installation cavity 241, which is beneficial to improving the heat dissipation effect of the light source 23.

[0113] Please refer to in combination with Figures 11 to 14 , in an embodiment of the present application, mounting plates 213 protrude from the relative two sides of the carrier 21 to respectively extend into two adjacent splicing components 10 and be connected to the two adjacent splicing components 10.

[0114] In this embodiment, it is convenient to connect with the adjacent splicing components 10 through the mounting plates 213, which is conducive to improving the convenience of connecting the carrier 21 and the splicing components 10. Further, extending the mounting plates 213 into the splicing components 10 can improve the compactness of the distribution of the carrier 21 and the splicing components 10. At the same time, it can also increase the contact area, which is conducive to improving the connection stability of the carrier 21 and the splicing components 10. In addition, such a setting also makes the connection between the carrier 21 and the splicing components 10 be hidden, thereby reducing the possibility of damage to the connection structure of the carrier 21. Among them, in the direction perpendicular to the extending direction of the carrier 21, one of the relative two sides of the carrier 21 can be provided with one mounting plate 213, and of course, multiple mounting plates 213 can also be provided. The multiple mounting plates 213 can be arranged in sequence along the extending direction of the carrier 21 to further improve the connection stability of the carrier 21 and the splicing components 10.

[0115] Please refer to Figure 14, in an embodiment of the present application, the mounting plate 213 includes a first plate body 214 and a second plate body 215 that are connected and arranged at an angle. One end of the first plate body 214 away from the second plate body 215 is connected to the carrier 21; the second plate body 215 is parallel to the plane where the corresponding splicing component 10 is located, and the second plate body 215 extends into the corresponding splicing component 10 and is connected to the splicing component 10.

[0116] In this embodiment, the mounting plate 213 is set as the first plate body 214 and the second plate body 215 arranged at an angle, so that the first plate body 214 is conveniently protruded on the carrier 21, and the second plate body 215 can be parallel to the plane where the splicing component 10 is located, so as to facilitate the adaptation and contact between the two, which is conducive to improving the convenience and stability of the connection between the second plate body 215 and the splicing component 10.

[0117] Please refer to Figure 14 , in an embodiment of the present application, the ambient light 20 further includes a lamp board 25 (i.e., a circuit board), the lamp board 25 is arranged on the carrier 21, and a plurality of light sources 23 are all arranged on the lamp board 25.

[0118] In this embodiment, by setting the lamp board 25, an installation position can be provided, which can conveniently realize the mechanical installation support and electrical power connection of the plurality of light sources 23, thereby greatly improving the convenience of installing the plurality of light sources 23.

[0119] In an embodiment of the present application, the light source 23 is an LED lamp bead.

[0120] In this embodiment, setting the light source 23 as an LED lamp bead can make its volume relatively small, thereby reducing the overall volume of the ambient light 20, so as to improve the convenience of installing it in the limited space of the gap 13.

[0121] Please refer to Figure 12 , in an embodiment of the present application, one side of the ambient light 20 close to the inner side of the riding cavity 11 abuts against two adjacent splicing components 10.

[0122] In this embodiment, abutting one side of the ambient light 20 close to the inner side of the riding cavity 11 against two adjacent splicing components 10 enables the ambient light 20 to seal the gap 13. At this time, it is beneficial to improve the visual sensory effect given on the inner side of the riding cavity 11 and the acoustic effect when listening to music in the riding cavity 11, thereby further enhancing the user experience.

[0123] Please refer to in combination Figures 9 to 13, in an embodiment of the present application, two adjacent splicing components 10 are arranged at intervals to enclose a gap 13 communicating with the outside; the cockpit 100 further includes a covering member 40, the covering member 40 is arranged in the gap 13 and is located on the side of the atmosphere lamp 20 facing the outside of the riding cavity 11, and the covering member 40 extends along the direction of the gap 13.

[0124] In this embodiment, two adjacent splicing components 10 are arranged at intervals so that a relatively large gap 13 can be enclosed to facilitate the installation and accommodation of the atmosphere lamp 20. Further, by arranging the covering member 40 outside the atmosphere lamp 20, the atmosphere lamp 20 can be covered, which is beneficial to improving the isolation and protection effect on the atmosphere lamp 20. In addition, such an arrangement can also prevent the depth of the gap 13 outside the atmosphere lamp 20 from being too large, which is beneficial to improving the visual effect outside the cockpit 100 and thus enhancing the competitiveness of the cockpit 100 in the market. Among them, the covering member 40 can be connected to adjacent splicing components 10, or can of course be connected to the atmosphere lamp 20. In addition, the covering member 40 and the atmosphere lamp 20 can be arranged at intervals to further improve the heat dissipation effect of the atmosphere lamp 20. In addition, it should be noted that when the atmosphere lamp 20 is only arranged in part of the gap 13, the covering member 40 can also be arranged in the gap 13 where the atmosphere lamp 20 is not arranged to ensure the consistency of the outside of the cockpit 100 and improve the visual effect.

[0125] Please refer to Figures 9 to 13 , in an 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 part 14, and the cockpit 100 further includes a plurality of connecting pieces 30; each connecting piece 30 is arranged at a connection part 14 and connects the corners of the multiple splicing components 10 in the connection part 14, and the opposite ends of the covering member 40 in the extending direction of the gap 13 respectively abut against two connecting pieces 30.

[0126] In this embodiment, the arrangement of the connecting piece 30 can, on the one hand, abut against the covering member 40, and thus can cover the position where the corners of multiple adjacent splicing components 10 are close to each other, that is, the connection part 14, so as to improve the sealing performance of the riding cavity 11. On the other hand, through the connecting piece 30, it is also convenient to contact the adjacent corners of the multiple splicing components 10, and thus it is convenient to connect and assemble the adjacent multiple splicing components 10. At the same time, such an arrangement also makes it unnecessary for the adjacent splicing components 10 to be arranged in a stacked manner, which is more convenient for the cooperation and arrangement between the splicing components 10.

[0127] Please refer to Figure 9 and Figure 11, in an embodiment of the present application, the covering member 40 includes a middle plate body 41 and two edge plate bodies 43. The two edge plate bodies 43 are respectively connected to opposite sides of the middle plate body 41. The opposite ends of the edge plate body 43 and the middle plate body 41 in the extending direction of the gap 13 respectively abut against the two connecting members 30. The two edge plate bodies 43 respectively extend into two adjacent splicing components 10 and are connected to the two adjacent splicing components 10. The edge plate body 43 is also parallel to the plane where the corresponding splicing component 10 is located.

[0128] In this embodiment, the covering member 40 is arranged to include a middle plate body 41 and two edge plate bodies 43, so that the two edge plate bodies 43 can be connected by the middle plate body 41, so that the covering member 40 can be formed as a whole for convenient connection and installation. The two edge plate bodies 43 are arranged as flat plates and are parallel to the plane where the corresponding splicing component 10 is located, so that the edge plate body 43 and the splicing component 10 can be better adapted and abutted, which is beneficial to improving the convenience and stability of the connection between the covering member 40 and the splicing component 10. Further, the edge plate bodies 43 are respectively extended into two adjacent splicing components 10, which can improve the compactness of the distribution of the covering member 40 and the splicing component 10. At the same time, the contact area can also be increased, which is beneficial to improving the stability of the connection between the covering member 40 and the splicing component 10. In addition, such an arrangement also makes the connection between the covering member 40 and the splicing component 10 be hidden, thereby reducing the possibility of damage to the connection structure of the covering member 40.

[0129] Please refer to Figure 9 , Figure 11 and Figure 15 , in an embodiment of the present application, the connecting member 30 includes a main body plate 31, a plurality of connecting plates 33 and a plurality of reinforcing plates 35. The plurality of connecting plates 33 are all connected to the edge of the main body. Each corner of each splicing component 10 in the joint 14 is correspondingly connected to a connecting plate 33. The connecting plate 33 is parallel to the plane where the corresponding splicing component 10 is located. The edge plate body 43 abuts against the connecting plate 33. Each reinforcing plate 35 connects the main body plate 31 and two adjacent connecting plates 33. The middle plate body 41 abuts against the reinforcing plate 35.

[0130] In this embodiment, the connecting member 30 is provided to include a main body plate 31, a connecting plate 33, and a reinforcing plate 35. Through the main body plate 31, multiple connecting plates 33 can be connected so that the multiple connecting plates 33 can form a whole, thereby facilitating the picking and placing of the whole connecting member 30 and improving the convenience of installation. Through the connecting plate 33, it can better correspond to the corners in each splicing component 10, so as 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 and is parallel to the plane where the corresponding splicing component 10 is located, so that the connecting plate 33 can better abut against the splicing component 10, which is beneficial to improving the convenience and stability of the connection between the two. By connecting the main body plate 31 and two adjacent connecting plates 33 through the reinforcing plate 35, the overall strength of the connecting member 30 can be enhanced, so that the connecting member 30 can more stably bear and connect the adjacent splicing components 10. In addition, the middle plate body 41 correspondingly abuts against the reinforcing plate 35, and the edge plate body 43 correspondingly abuts against the connecting plate 33, which can improve the abutting and matching effect between the covering member 40 and the connecting member 30, and is beneficial to improving the covering and sealing effect of the riding cavity 11.

[0131] Please refer to Figure 9 , Figure 11 and Figure 15 , in an embodiment of the present application, both the middle plate body 41 and the reinforcing plate 35 are outwardly convex arc-shaped plates, and the axes of the middle plate body 41 and the reinforcing plate 35 coincide, and the main body plate 31 is an outwardly convex arc-shaped plate.

[0132] In this embodiment, the middle plate body 41 is set as an arc-shaped plate, which can make the connection 14 between it and the two edge plate bodies 43 smoother, so that the shape of the covering member 40 can be more regular and the manufacturing convenience thereof can be improved. At the same time, the depth of the gap 13 outside the covering member 40 can be reduced by outward convexity, so as to further reduce the height difference between the outside of the splicing assembly 10 and the outside of the covering member 40. And the reinforcing plate 35 is also set as an arc-shaped plate, which can facilitate its fitting and abutting with the middle plate body 41. Further, the main plate body 31 is set as an outward convex arc-shaped plate, which can facilitate its fitting connection with a plurality of arc-shaped reinforcing plates 35. In addition, a smooth curved surface can be formed at the connection 14 to reduce the risk of injury when the user collides with this place, which is beneficial to improving the safety of using the cockpit 100. At the same time, the main plate body 31 exposed to the outside as an outward convex arc-shaped plate, in cooperation with the triangular shape of the splicing assembly 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 assembly 10. Among them, in order to improve the exposure effect of the main plate body 31, the corners of the splicing assembly 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, thus being beneficial to improving the service life and usage safety of the splicing assembly 10. In addition, in order to improve the visual sense effect inside the cockpit 100, please refer to Figure 16 and Figure 17 , a filling member 37 can be provided inside the connecting member 30, and the side of the filling member 37 facing away from the main plate body 31 can be set as a plane.

[0133] Please refer to Figure 3 , in an embodiment of the present application, the cockpit 100 further includes a camera module 60, and the camera module 60 is arranged in the riding cavity 11.

[0134] In this embodiment, by setting the camera module 60, the user located in the seating cavity 11 can be photographed, identified, and sensed. Then, when it is identified and sensed that there is someone in the seating cavity 11, the user arrival signal can be transmitted to the controller of the cockpit 100, so that the controller of the cockpit 100 can timely control functional modules such as the ambient light 20 (the functional module can also be the speaker 171, wireless charging module 80, reading light 90, and fan module introduced below) to work, thereby realizing the automatic opening of the cockpit 100. In this way, the intelligence level of the cockpit 100 can be improved, which is conducive to further improving the user experience. Among them, a standard image when there is a user in the seating cavity 11 is pre-stored in the camera module 60. Then, when the camera module 60 performs the photographing and identifying work, the photographed image can be compared with the standard image to identify whether there is a user in the seating cavity 11. In addition, the camera module 60 can be installed on the splicing component 10. Of course, other objects can also be provided in the seating cavity 11 to support its installation.

[0135] Please refer to Figure 21 , in an embodiment of the present application, a receiving groove 15 is provided on the inner side of the splicing component 10 facing the seating cavity 11. The camera module 60 is disposed in the receiving groove 15. The camera module 60 includes a module housing 61 and a camera 63 disposed on the module housing 61; a driving component 65 is further included, and the driving component 65 is used to drive the camera module 60 to rotate, so that the module housing 61 covers the notch of the receiving groove 15, or the camera 63 is exposed from the notch of the receiving groove 15.

[0136] In this embodiment, the camera module 60 is disposed in the accommodation groove 15, which can improve the compactness of the installation of the camera module 60 and the splicing component 10. Further, the camera module 60 is also arranged to be rotatable, so that when in need of use, the camera module 60 can be rotated by the driving component 65, so that the camera 63 in the camera module 60 corresponds to the notch of the accommodation groove 15, and thus external shooting can be realized. When not in use, the driving component 65 can be used to drive the camera module 60 to rotate, so that the module housing 61 in the camera module 60 covers the notch of the accommodation groove 15. In this way, the camera 63 can be hidden when not in use, which is beneficial to improving the isolation and protection effect on it. At the same time, the notch of the accommodation groove 15 can also be covered, which is beneficial to ensuring the consistency of the inner appearance of the riding cavity 11 and improving the visual sense effect. Among them, the driving component 65 may include a rotation driving member, for example: a motor or a rotary cylinder. Of course, it may also further include a transmission component on this basis. For example: the transmission component may include a driving gear and a driven gear, the driving gear can be connected to the rotation driving member, the driven gear can be connected to the module housing 61 in the camera module 60, and meshed with the driving gear. Of course, the transmission component may also be a combination of a driving wheel, a driven wheel and a belt.

[0137] Please refer to Figure 1 and Figure 2 , in an embodiment of the present application, the cockpit 100 further includes a wireless charging module 80, and the wireless charging module 80 is disposed in the splicing component 10.

[0138] In this embodiment, the setting of the wireless charging module 80 enables portable wireless charging of the user's mobile phone or other electrical devices. In this way, the function of the cockpit 100 is enhanced, which is beneficial to further improving the user experience. Among them, the number of the wireless charging modules 80 is one. Of course, to improve the convenience of use. The number of the wireless charging modules 80 is also at least two. It is defined that the cockpit 100 has a front-back direction and a left-right direction, the communication port 12 is disposed on the front side of the cockpit 100, and at least two wireless charging modules 80 are respectively disposed in the splicing components 10 on the left and right sides. In this way, when the user is sitting in the riding cavity 11, charging can be carried out on both the left and right sides. Among them, the types of at least two wireless charging modules 80 may be the same, or of course different, so as to realize charging of electrical devices such as mobile phones of Android and Apple systems respectively.

[0139] Please refer to Figure 1 and Figure 2 , in an embodiment of the present application, an accommodation groove 16 is provided on the side of the splicing component 10 facing the inner side of the riding cavity 11, and the wireless charging module 80 is embedded in the bottom wall of the accommodation groove 16.

[0140] In this embodiment, the placement groove 16 can be used to place and position the electrical devices that need to be charged by the user, so that the user can quickly and accurately place electrical devices such as mobile phones into the placement groove 16, which is conducive to further improving the convenience of the charging process. At the same time, the placement groove 16 can also ensure the stable placement of electrical devices such as mobile phones, which is conducive to improving the stability of charging electrical devices such as mobile phones. Among them, the wireless charging module 80 can be embedded in the bottom wall of the installation groove 211 in an exposed manner, or can also be embedded in the bottom wall of the installation groove 211 in a hidden manner.

[0141] Please refer to Figure 3 , in an embodiment of the present application, the cockpit 100 further includes a reading lamp 90, and the reading lamp 90 is arranged in the riding cavity 11.

[0142] In this embodiment, the setting of the reading lamp 90 can facilitate the user to read while sitting in the cockpit 100. This makes the usage scenarios of the cockpit 100 more diverse, which is conducive to further enhancing the user experience. Among them, the reading lamp 90 can be installed on the splicing component 10, or of course, other objects can be provided in the riding cavity to support its installation. In addition, the number of reading lamps 90 can be one. Of course, the reading lamp 90 can also be at least two. At this time, among the three splicing components 10 at the top of the annular structure 19, two of the reading lamps 90 can be arranged on the two side splicing components 10, so that when the two splicing components 10 form an angle, the light emitting directions of the two reading lamps 90 can also form an angle to effectively irradiate the area where the user is sitting in the riding cavity 11. And the middle splicing component 10 can be provided with the camera module 60 introduced above, so that it can also be in the middle and can better face the user in the riding cavity 11 for effective shooting and recognition.

[0143] Please refer to Figure 1 , in an embodiment of the present application, the cockpit 100 further includes a speaker 171, the speaker 171 is arranged in the splicing component 10, and the splicing component 10 is provided with a sound outlet 17 communicating with the riding cavity 11 at a position corresponding to the speaker 171.

[0144] In this embodiment, the setting of the speaker 171 enables the cockpit 100 to provide the user with more scenarios and more high-quality and perfect sounds (such as: game music or movie music) through the speaker, which is conducive to further enhancing the user experience. Among them, the number of speakers 171 can be one, or of course, multiple.

[0145] In an embodiment of the present application, the cockpit 100 further includes a fan module, the fan module is arranged in the riding cavity 11, and the splicing component 10 is provided with an air inlet corresponding to the fan module.

[0146] In this embodiment, the fan module can drive the external air flow to enter the riding cavity 11 from the air inlet, and then can play a role in ventilating the air flow in the riding cavity 11, so as to ensure the freshness of the air in the riding cavity 11 and further improve the user experience.

[0147] Please refer to Figure 1 , Figure 2 and Figure 19 , in an embodiment of the present application, the cockpit 100 further includes a seat 70, and the seat 70 is disposed in the riding cavity 11.

[0148] In this embodiment, by providing the seat 70, a more comfortable seating position can be given to the user, which is conducive to improving the comfort of the user sitting in the cockpit 100 and further enhancing the user experience. Among them, when the cockpit 100 is in a normal use and placement state, it is defined that the cockpit 100 has an up-down direction and a horizontal direction, and the seat 70 can be connected to the upper surface of the splicing component 10 located at the bottom.

[0149] Please refer to Figure 19 , 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.

[0150] In this embodiment, the seat 70 is provided to include a seat cushion portion 71, a backrest portion 73 and a headrest portion 75, so that the seat cushion portion 71 can be used for sitting, the backrest portion 73 can be used for leaning back, and the headrest portion 75 can be used for abutting and supporting the user's head. In this way, the seat 70 can better abut and support each part of the user, which is conducive to improving the comfort of the user's sitting. Further, in order to facilitate the user to sit more comfortably on the seat 70 with the body in an inclined posture, please refer to Figure 20 , it is defined that the seat cushion portion 71 has a sitting surface 711, and the sitting surface 711 can be an outwardly 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 an inwardly concave arc surface, and the second surface 735 is an outwardly convex arc surface; it is defined that the headrest portion 75 has a headrest surface 751, and the headrest surface 751 can be an outwardly convex arc surface.

[0151] Please refer to 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.

[0152] In this embodiment, one end of the seat cushion portion 71 away from the backrest portion 73 protrudes from the communication port 12, so that when the user is sitting in the cockpit 100, the connection 14 between the user's thigh and calf can be lapped on the seat cushion portion 71, avoiding the squeezing feeling caused by the edge of the communication port 12, which is beneficial to further improve the riding comfort and further enhance the user experience.

[0153] Please refer to Figure 1 and Figure 4 , in an embodiment of the present application, it is defined that the cockpit 100 has an up-down direction and a horizontal direction, and the communication port 12 is arranged to incline upwards; the cockpit 100 further includes a support structure 50, and the support structure 50 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.

[0154] In this embodiment, arranging the communication port 12 to incline upwards can reduce the blockage of the user's head, and then facilitate the user to get on and off the riding cavity 11, so as to further enhance 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 sitting in the inclined riding cavity 11, and then facilitates the user in the riding cavity 11 to have a wider viewing angle of 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 structural type of the support processed by the present application is not limited.

[0155] Please refer to Figure 4 , in an embodiment of the present application, it is defined that the included angle formed by the plane where the communication port 12 is located and the up-down direction is α, and the relationship is satisfied: 0° < α ≤ 30°.

[0156] In this embodiment, setting the included 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 make the inclination angle of the communication port 12 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 sitting. Among them, the included angle α formed by the plane where the communication port 1212 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.

[0157] Please refer toFigure 1 and Figure 18 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 sets of support frames 51, and the two sets 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.

[0158] In this embodiment, the support structure 50 is set as two sets of support frames 51, and each set 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 made relatively simple 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.

[0159] Please refer to Figure 18 In an embodiment of the present application, the distance between the two support rods 511 located on the front side in the two sets of support frames 51 is greater than the distance between the two support rods 511 located on the rear side.

[0160] In this embodiment, the distance between the two support rods 511 located on the front side 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 support rod 511 on the front side. 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.

[0161] Please refer to Figure 18 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.

[0162] In this embodiment, the connecting rod 513 is set to include a first section 515 and a second section 517 arranged at 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 adaptable abutting support for the triangular splicing component 10. For example, the two side edges of the triangular splicing component 10 can be abutted and supported by the first section 515 of the two connecting rods 513.

[0163] Please refer to Figure 3 and Figure 18 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 splicing assembly 10 located at the bottommost.

[0164] In this embodiment, the setting of the fixing plate 53 can, on the one hand, be used for adaptive abutment with the splicing assembly 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 whole, so that the installation of the two sets of support frames 51 can be completed at one time, thereby improving the installation convenience.

[0165] 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 all embodiments, it at least has all the beneficial effects brought by the technical solutions of the above embodiments, which will not be elaborated one by one here. Among them, the entertainment system may further include a head-mounted display device (VR device or AR device). At this time, the user can sit in the cockpit 100 and use the head-mounted display device more conveniently. Of course, the entertainment system may also include a projector. At this time, the user can sit in the cockpit 100 and watch the movie projected by the projector.

[0166] The above are only the preferred embodiments of the present application, and do not limit the patent scope of the present application. Any equivalent structural transformation made by using the content of the specification and drawings of the present application under the inventive concept of the present application, or direct / indirect application in other related technical fields are all included in the patent protection scope of the present application.

Claims

1. A cockpit, characterized in that, Including: A plurality of splicing components, which are spliced and enclosed to form a seating cavity and a communication port communicating with the seating cavity, and the shapes of the splicing components are all triangular; And An ambient light, two adjacent splicing components are arranged at an angle and enclose a gap communicating with the seating cavity, and at least one of the gaps is provided with the ambient light.

2. The cockpit according to claim 1, characterized in that, The ambient light includes: A carrier, which is connected to the splicing component and extends along the extending direction of the gap; and A plurality of light sources, which are all arranged on the carrier and are arranged in sequence along the extending direction of the carrier, and the plurality of light sources can all emit light toward the inner side of the seating cavity.

3. The cockpit according to claim 2, characterized in that, The ambient light further includes a light guide member, which is arranged on the carrier and encloses an installation cavity with the carrier, and the plurality of light sources are all arranged in the installation cavity.

4. The cockpit according to claim 3, characterized in that, The carrier is provided with an installation groove, the notch of the installation groove faces the inner side of the seating cavity, the light guide member covers the notch of the installation groove, and encloses the installation cavity with the installation groove.

5. The cockpit according to claim 4, characterized in that, Clamping grooves are arranged on the inner sides of the two groove walls of the installation groove parallel to the extending direction of the carrier, and the two opposite sides of the light guide member are respectively clamped in the two clamping grooves; And / or, the installation groove penetrates through the opposite sides in the extending direction of the carrier; And / or, the plurality of light sources are installed on the groove wall of the installation groove facing its notch; And / or, the plurality of light sources and the light guide member are arranged at intervals.

6. The cockpit according to claim 2, characterized in that, Installation plates protrude from the opposite sides of the carrier to respectively extend into two adjacent splicing components and are connected to the two adjacent splicing components.

7. The cockpit according to claim 6, characterized in that, The installation plate includes a first plate body and a second plate body which are connected and arranged at an angle, and one end of the first plate body far from the second plate body is connected to the carrier; The second plate body is parallel to the plane where the corresponding splicing component is located, the second plate body extends into the corresponding splicing component and is connected to the splicing component.

8. The cockpit according to claim 2, characterized in that, The ambient light further includes a lamp board, which is arranged on the carrier, and the plurality of light sources are all arranged on the lamp board; And / or, the light source is an LED lamp bead.

9. The cockpit according to claim 1, characterized in that, One side of the ambient light close to the inner side of the seating cavity abuts against two adjacent splicing components.

10. The cockpit according to any one of claims 1 to 9, characterized in that, Two adjacent splicing components are arranged at intervals to enclose the gap communicating with the outside; The cockpit further includes a covering member, which is arranged in the gap and is located on the outer side of the ambient light facing the seating cavity, and the covering member extends along the direction of the gap.

11. The cockpit according to claim 10, characterized in that, The covering member and the ambient light are arranged at intervals.

12. The cockpit according to claim 10, characterized in that, Define the position where the corners of a plurality of adjacent splicing components are close to each other as a connection point, and the cockpit further includes a plurality of connecting members; Each connecting member is arranged at one connection point and connects the corners of the plurality of splicing components at the connection point, and the opposite ends of the covering member in the extending direction of the gap respectively abut against the two connecting members.

13. The cockpit according to claim 12, characterized in that, The covering member includes a middle plate body and two edge plate bodies. The two edge plate bodies are respectively connected to opposite sides of the middle plate body. The opposite ends of the edge plate body and the middle plate body in the extending direction of the gap respectively abut against the two connecting members. The two edge plate bodies respectively extend into two adjacent splicing components and are connected to the two adjacent splicing components. The edge plate body is also parallel to the plane where the corresponding splicing component is located.

14. The cockpit according to claim 13, characterized in that, The connecting member includes: A main body plate; A plurality of connecting plates. The plurality of connecting plates are all connected to the edge of the main body. Each corner of each splicing component at the connection is correspondingly connected to a connecting plate. The connecting plate is parallel to the plane where the corresponding splicing component is located. The edge plate body abuts against the connecting plate; and A plurality of reinforcing plates. Each reinforcing plate connects the main body plate and two adjacent connecting plates. The middle plate body abuts against the reinforcing plate.

15. The cockpit according to claim 14, characterized in that, Both the middle plate body and the reinforcing plate are outwardly convex arc-shaped plates, and the axes of the middle plate body and the reinforcing plate coincide. The main body plate is an outwardly convex arc-shaped plate.

16. The cockpit according to any one of claims 1 to 9, characterized in that, The cockpit further includes a camera module, and the camera module is arranged in the riding cavity.

17. The cockpit according to claim 16, characterized in that, On one side of the splicing component facing the inner side of the riding cavity, there is a receiving groove, and the camera module is arranged in the receiving groove. The camera module includes a module housing and a camera arranged in the module housing. The cockpit further includes a driving component, and the driving component is used to drive the camera module to rotate so that the module housing covers the notch of the receiving groove, or the camera is exposed from the notch of the receiving groove.

18. The cockpit according to any one of claims 1 to 9, characterized in that, The cockpit further includes a wireless charging module, and the wireless charging module is arranged in the splicing component.

19. The cockpit according to claim 18, characterized in that, On one side of the splicing component facing the inner side of the riding cavity, there is an installation groove, and the wireless charging module is embedded in the bottom wall of the installation groove. And / or, the number of the wireless charging modules is at least two. Defining that the cockpit has a front-back direction and a left-right direction, the communication port is arranged on the front side of the cockpit, and at least two of the wireless charging modules are respectively arranged in the splicing components on the left and right sides.

20. The cockpit according to any one of claims 1 to 9, characterized in that, The cockpit further includes a reading lamp, and the reading lamp is arranged in the riding cavity. And / or, the cockpit further includes a speaker, the speaker is arranged in the splicing component, and the splicing component is provided with a sound outlet communicating with the riding cavity at a position corresponding to the speaker. And / or, the cockpit further includes a seat, and the seat is arranged in the riding cavity. And / or, defining that the cockpit has an up-down direction and a horizontal direction, the communication port is inclined upward; the cockpit further includes a support structure, and the support structure is arranged on the lower surface of the lowermost splicing component, and the lower surface of the support structure is a plane. And / or, a part of the splicing components enclose a conical structure with one end open, and the conical structure is formed by splicing and enclosing 4-6 splicing components. And / or, the shape of each splicing component is an equilateral triangle, and the sizes of all the splicing components are equal. And / or, the cockpit further includes a fan module, the fan module is disposed in the riding cavity, and the splicing assembly is provided with an air inlet corresponding to the fan module.

21. An entertainment system, characterized in that, Comprising a cockpit according to any one of claims 1 to 20.

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