Cabin and entertainment system

Abstract

The invention discloses a cabin and an entertainment system, the cabin comprises a plurality of splicing assemblies, the plurality of splicing assemblies are spliced to define a riding cavity and a communication port, and the communication port communicates with the riding cavity; the projection of the communication port is pentagonal in the direction from the end, provided with the communication port, of the cabin to the end, deviating from the communication port, of the cabin. According to the technical scheme, the manufacturing cost of the cabin can be reduced.

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] 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 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, thereby resulting in 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 riding cavity and a communication port, and the communication port communicates with the riding cavity;

[0005] In the direction from one end of the cockpit where the communication port is provided to the end away from the communication port, the projection of the communication port is a pentagon.

[0006] Optionally, the projection of the communication port is a regular pentagon.

[0007] Optionally, the communication port is a plane.

[0008] Optionally, it is defined that the cockpit has an up-down direction and a horizontal direction, and the plane where the communication port is located is arranged at an angle with both the up-down direction and the horizontal direction.

[0009] Optionally, it is defined that the angle formed by the plane where the communication port is located and the up-down direction is α, and the relationship is satisfied: 0° < α ≤ 30°.

[0010] Optionally, the cockpit includes five inner sides at the communication port, and two adjacent inner sides enclose an inner angle;

[0011] It is defined that the cockpit has an up-down direction and a horizontal direction, and one of the inner sides extends horizontally and is located below the opposite inner angle.

[0012] Optionally, it is defined that the inner side extending horizontally is the bottom side, and the cockpit further includes a seat, and the seat is arranged in the riding cavity and is connected to the splicing component where the bottom side is formed.

[0013] Optionally, a part of the seat protrudes from the bottom side out of the communication port.

[0014] Optionally, the seat includes:

[0015] A seat cushion part, the seat cushion part is connected to the splicing component formed with the bottom side edge, and one end of the seat cushion part protrudes from the bottom side edge to the communication port; and

[0016] A backrest part, the backrest part protrudes from one end of the seat cushion part away from the communication port.

[0017] Optionally, the cockpit further includes a support structure, the support structure is arranged outside the riding cavity and is connected to the splicing component formed with the bottom side edge.

[0018] Optionally, five of the plurality of splicing components enclose to form the communication port, and one side edge of each of the five splicing components forms the inner side edge.

[0019] Optionally, the shape of each splicing component is a triangle.

[0020] Optionally, the splicing components enclose to form a conical structure with one end being open, and the end with the opening of the conical structure encloses to form the communication port;

[0021] Or, part of the splicing components enclose to form a conical structure with one end being open, and another part of the splicing components enclose to form an annular structure with both ends being open, and one end of the annular structure is connected to the end with the opening 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.

[0022] Optionally, when the splicing components enclose to form a conical structure and an annular structure, define the number of splicing components in the conical structure as X, and the number of splicing components in the annular structure as Y, satisfying the relationship: Y = 2X.

[0023] Optionally, the shape of each splicing component is an isosceles triangle, and the sizes of all the splicing components are equal.

[0024] Optionally, the shape of each splicing component is an equilateral triangle.

[0025] Optionally, the adjacent corners of the plurality of splicing components are connected.

[0026] Optionally, 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.

[0027] Optionally, the connecting member includes an arc-shaped surface protruding towards the outside of the seating cavity, and the adjacent corners of the plurality of splicing components are spaced apart so that the arc-shaped surface is exposed to the outside.

[0028] The present invention also provides an entertainment system, including a cockpit.

[0029] 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 with the whole cockpit, and thus relatively simpler and smaller molds can be correspondingly used for production. And the molds with relatively simple structures and relatively small volumes have higher service lives and lower costs, so that the manufacturing cost of the cockpit can be relatively lower accordingly. That is to say, the structural optimization design 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, the hands-on ability of users can be cultivated and the interest can be enhanced, which is beneficial to improving the user experience. Further, in the direction from one end of the cockpit where the communication port is provided to the end away from the communication port, the projection of the communication port is set as a pentagon, so that the cockpit can obtain a seating cavity with a relatively large volume as much as possible inside under the condition of limited overall volume, so as to better meet the use needs of different users and the user experience. At the same time, the shape of the communication port with a pentagonal projection is also relatively novel, which is beneficial to enhancing the visual sensory effect of the cockpit to further improve the user experience. BRIEF DESCRIPTION OF THE DRAWINGS

[0030] 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, other drawings can be obtained based on the structures shown in these drawings without creative efforts.

[0031] Figure 1 is a schematic structural diagram of an embodiment of the cockpit of the present invention;

[0032] Figure 2 is Figure 1 another perspective schematic diagram of the cockpit in ;

[0033] Figure 3 is Figure 1 another perspective schematic diagram of the cockpit in ;

[0034] Figure 4 is Figure 1 a partial structural schematic diagram of the cockpit in ;

[0035] Figure 5 is Figure 4 Another perspective schematic diagram of the partial structure of the cockpit in

[0036] Figure 6 is Figure 5 An exploded structure schematic diagram of the partial structure of the cockpit in

[0037] Figure 7 is Figure 6 Another perspective schematic diagram of the exploded structure of the partial structure of the cockpit in

[0038] Figure 8 is Figure 1 Another schematic diagram of another partial structure of the cockpit in

[0039] Figure 9 is Figure 8 Another perspective schematic diagram of the partial structure of the cockpit in

[0040] Figure 10 is Figure 8 An exploded structure schematic diagram of the partial structure of the cockpit in

[0041] Figure 11 is Figure 1 Schematic diagram of the structure of the seat in

[0042] Explanation of the reference numerals in the drawings:

[0043] 100, cockpit;

[0044] 10, splicing component; 10a, inner side; 10b, inner included angle; 10c, bottom side; 11, riding cavity; 12, communication port; 13, conical structure; 14, annular structure; 15, connection point;

[0045] 30, connecting piece; 30a, arc surface; 31, main body plate; 33, connecting plate; 31, reinforcing plate;

[0046] 40, covering piece;

[0047] 50, support structure;

[0048] 70, seat; 71, cushion part; 73, backrest part; headrest part, 75.

[0049] The realization, functional features and advantages of the object of the present invention will be further described with reference to the embodiments and the accompanying drawings. Detailed implementation manners

[0050] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present invention without creative efforts shall fall within the protection scope of the present invention.

[0051] It should be noted that all directional indications (such as up, down, left, right, front, back...) in the embodiments of the present invention are only used to explain the relative positional 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.

[0052] In the present invention, unless otherwise clearly defined and limited, terms such as "connection" and "fixation" 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 invention can be understood according to specific situations.

[0053] In addition, the descriptions involving "first", "second", etc. in the present invention 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 of such features. 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 a solution that satisfies both A and B at the same time. 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 protection scope required by the present invention.

[0054] 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 fun.

[0055] Therefore, based on the above considerations, in order to solve the problems that the manufacturing cost of the current cockpit is relatively high and it cannot well meet some personalized needs of users, the present application proposes a new type of cockpit. The cockpit is innovatively provided with a plurality of splicing components, and a seating cavity and a communication port communicating with the seating cavity are formed by splicing and enclosing the plurality of splicing components. Furthermore, when manufacturing the cockpit, molds with relatively simple structures and relatively small volumes can be correspondingly used to reduce the manufacturing cost of the cockpit. At the same time, it is convenient for users to perform splicing and assembly to meet the needs of cultivating users' hands-on ability and enhancing the fun. Moreover, in the direction from the end of the cockpit where the communication port is provided to the end away from the communication port, the projection of the communication port is set as a pentagon, so that in the case of a limited overall volume of the cockpit, a seating cavity with a volume that can meet the needs of users can be formed as much as possible on the inside.

[0056] Next, the structure of the cockpit proposed in the present application will be explained and illustrated by way of examples. In an embodiment of the present application, please refer to Figure 1 and Figure 2 , the cockpit 100 proposed in the application includes a plurality of splicing components 10, and the plurality of splicing components 10 are spliced and enclosed to form a seating cavity 11 and a communication port 12, and the communication port 12 communicates with the seating cavity 11; in the direction from the end of the cockpit 100 where the communication port 12 is provided to the end away from the communication port 12, the projection of the communication port 12 is a pentagon.

[0057] 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 to form 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. The present application does not limit the structural shape formed by enclosing the splicing components 10, as long as the projection of the communication port 12 formed by enclosing the splicing components 10 is a pentagon in the direction from the end of the cockpit 100 where the communication port 12 is provided to the end away from the communication port 12. Among them, when the cockpit 100 is in a normal use state, the communication port 12 can be provided on the front side of the cockpit 100 for users to enter and exit the seating cavity 11. The projection of the communication port 12 is a pentagon, including the case where the corners of the pentagon are not chamfered, and of course, it can also include the case where chamfers are made, for example: rounding the corners or chamfering the bevels at the corners of the pentagon. In addition, the communication port 12 can be arranged in a plane, of course, it can also be arranged in an arc surface, or a part of the communication port 12 is located in one plane and the other part is located in another plane.

[0058] In addition, the shape of the splicing component 10 can be triangular, and of course it can also be square, rectangular, pentagonal, etc. The present application does not limit the shape of the splicing component 10. Further, the shapes and sizes of the respective splicing components 10 can be the same, and of course they can also be only partially the same, or the shapes and sizes of the respective splicing components 10 are all different. Each splicing component 10 can also be a single-layer plate structure, and of course it can also be a multi-layer plate structure including a mounting plate and a sound-absorbing plate stacked on the mounting plate. In addition, when the respective splicing components 10 are spliced, they can be directly connected and assembled between the respective splicing components 10, and of course they can also be indirectly connected and assembled through the connecting member 30 introduced below.

[0059] The cockpit 100 of the technical solution of the present invention is formed by splicing and enclosing a plurality of splicing components 10 to form a riding cavity 11 and a communication port 12 communicating with the riding cavity, so that each splicing component 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 entire cockpit, so that a mold with a relatively simple structure and a relatively smaller volume can be correspondingly used for production. A mold with a relatively simple structure and a relatively smaller volume has a higher service life and a lower cost, so that 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, in the direction from one end of the cockpit 100 where the communication port 12 is provided to the end away from the communication port 12, the projection of the communication port 12 is set as a pentagon, so that the cockpit 100 can obtain a riding cavity 11 with a relatively large volume as much as possible inside under the condition of limited overall volume, so as to better meet the use needs of different users and the user experience. At the same time, the shape of the communication port 12 with a pentagonal projection is also relatively novel, which is beneficial to enhancing the visual sensory effect of the cockpit 100 and further improving the user's experience.

[0060] Please refer to Figure 2 , in an embodiment of the present application, the projection of the communication port 12 is a regular pentagon.

[0061] In this embodiment, the projection of the communication port 12 is set as a regular pentagon, which can make the shape of the communication port 12 very regular. So that when the user is sitting in the riding cavity 11, the required space can be formed around the circumference of the communication port 12 with the user as the center, improving the user experience. At the same time, it is also convenient to enclose and form the communication port 12 and enhance the visual sensory effect of the communication port 12. Of course, in other embodiments, in the direction from the end of the cockpit 100 where the communication port 12 is provided to the end away from the communication port 12, the projection of the communication port 12 can also be a pentagon that is not a regular pentagon.

[0062] Please refer to Figure 1 and Figure 3 , in an embodiment of the present application, the communication port 12 is a plane.

[0063] In this embodiment, setting the communication port 12 as a plane can further improve the regularity of the communication port 12, so as to further improve the convenience of enclosing it and enhance the visual sensory effect of the communication port 12.

[0064] Please refer to Figure 1 and Figure 3 , 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 plane where the communication port 12 is located is arranged at an angle with both the up-down direction and the horizontal direction.

[0065] In this embodiment, setting the plane where the communication port 12 is located at an angle with both the up-down direction and the horizontal direction can also be said that the communication port 12 is arranged to tilt upward. At this time, the blockage of the user's head can be reduced, and then it is convenient for the user to sit in and leave the riding cavity 11, so as to further improve the user experience. At the same time, such a setting is also convenient for the user's body when sitting in the inclined riding cavity 11, and the user's viewing angle can correspond to the orientation of the communication port 12, so as to facilitate the user in the riding cavity 11 to have a wider viewing angle of the outside world and improve the use experience.

[0066] Please refer to Figure 3 , in an embodiment of the present application, it is defined that the angle formed by the plane where the communication port 12 is located and the up-down direction is α, satisfying the relationship: 0° < α ≤ 30°.

[0067] In this embodiment, the included angle α formed by the plane where the communication port 12 is located and the up-down direction is set to be from 0° to 30°, which can ensure that the inclination angle of the communication port 12 is not too large, facilitating the smooth entry of users and providing a better view outside through the communication port 12 after taking a seat. Among them, the included 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°. Of course, it can also be any value within the above range.

[0068] Please refer to Figure 1 and Figure 4 , in an embodiment of the present application, the cockpit 100 includes five inner sides 10a at the communication port 12, and two adjacent inner sides 10a enclose an inner included angle 10b; it is defined that the cockpit 100 has an up-down direction and a horizontal direction, and one inner side 10a extends along the horizontal direction and is located below the opposite inner included angle 10b.

[0069] In this embodiment, an inner included angle 10b and an inner side 10a at the communication port 12 are arranged in sequence in the up-down direction, which can facilitate the user to take a seat through the splicing component 10 formed with the inner side 10a; or provide a structural basis to facilitate the installation of the seat 70 introduced below and improve the compactness of the distribution of the seat 70 in the riding cavity 11, thereby improving the space utilization rate of the riding cavity 11.

[0070] Please refer to Figure 1 and Figure 4 , in an embodiment of the present application, the inner side 10a extending along the horizontal direction is defined as the bottom side 10c, and the cockpit 100 further includes a seat 70. The seat 70 is arranged in the riding cavity 11 and is connected to the splicing component 10 formed with the bottom side 10c.

[0071] 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 when sitting in the cockpit 100 and further enhancing the user experience. Connecting the seat 70 to the splicing component 10 formed with the bottom side 10c can make the contact area between the two smaller, which is conducive to improving the convenience and stability of the connection between the seat 70 and the splicing component 10. At the same time, it is also convenient to hide the connection structure between the seat 70 and the splicing component 10 between the two, so as to reduce the possibility of the connection structure being damaged by the outside and improve the aesthetics of the appearance of the cockpit 100. Among them, the connection between the seat 70 and the splicing component 10 can be a screw connection, and of course, it can also be a snap connection or a magnetic connection, etc. This application does not limit the connection method between the seat 70 and the splicing component 10.

[0072] Please refer to Figure 1 and Figure 3 , in an embodiment of the present application, a part of the seat 70 protrudes from the bottom side 10c to the communication port 12.

[0073] In this embodiment, setting a part of the seat 70 to protrude from the bottom side 10c to the communication port 12 enables the connection area between the user's thigh and calf to overlap on the upper surface of one end of the seat 70 protruding from the communication port 12 when the user is sitting in the cockpit 100. At this time, it is possible to avoid the connection area between the user's thigh and calf being squeezed by the edge of the communication port 12 to generate a sense of compression, which is conducive to further improving the seating comfort and further enhancing the user experience.

[0074] Please refer to Figure 1 , Figure 3 and Figure 11 , in an embodiment of the present application, the seat 70 includes a seat cushion part 71 and a backrest part 73. The seat cushion part 71 is connected to the splicing component 10 formed with the bottom side 10c, and one end of the seat cushion part 71 protrudes from the bottom side 10c to the communication port 12; the backrest part 73 protrudes from one end of the seat cushion part 71 away from the communication port 12.

[0075] In this embodiment, the seat 70 is provided to include a seat cushion part 71 and a backrest part 73, so that the seat cushion part 71 can be used for sitting and the backrest part 73 can be used for reclining. At this time, the seat 70 can better abut and support each part of the user, which is conducive to improving the comfort of the user when sitting. In addition, it should be noted that in some embodiments, the seat 70 may only include the seat cushion part 71. Or in some other embodiments, on the basis of including the seat cushion part 71 and the backrest part 73, the seat 70 may further include a headrest part 75 connected to one end of the backrest part 73 away from the seat cushion part 71. At this time, the headrest part 75 can be used to abut and support the user's head.

[0076] Please refer to Figures 1 to 3 , in an embodiment of the present application, the cockpit 100 further includes a support structure 50, and the support structure 50 is disposed outside the riding cavity 11 and connected to the splicing component 10 formed with the bottom side edge 10c.

[0077] In this embodiment, the support structure 50 is further provided, so that the position of the communication port 10 can be lifted by the support structure 50, so as to facilitate the smooth entry and exit of the user and have a comfortable riding posture. At the same time, when the lower surface of the support structure 50 is set as a plane, it is also convenient for the cockpit 100 to be stably placed on a support surface such as the ground through the support structure 50. Among them, the support structure 50 can be a frame structure formed by combining multiple rod bodies, and of course it can also be a body structure or a shell structure, etc. The present application does not limit the structural type and shape of the support structure 50.

[0078] Please refer to Figure 4 , in an embodiment of the present application, five of the plurality of splicing components 10 enclose to form a communication port 12, and one side of each of the five splicing components 10 forms an inner side edge 10a.

[0079] In this embodiment, five splicing components 10 are used to enclose to form the communication port 12, so that the number of splicing components 10 can be relatively small, so as to further improve the convenience of enclosing the communication port 12. Of course, the present application is not limited to this. In other embodiments, it may also be formed by enclosing six or more. At this time, two side edges of at least two splicing components 10 can be cooperated to form an inner side edge 10a.

[0080] Please refer to Figure 4 and Figure 5 , in an embodiment of the present application, the shape of each splicing component 10 is a triangle.

[0081] In this embodiment, the splicing component 10 is set as a triangle, and the triangle is the simplest polygon, so that it is convenient to assemble the splicing component 10 into the cockpit 100 and the communication port 12 of the required shape. That is, it improves the convenience and flexibility of splicing, and thus is conducive to further improving the user experience. Among them, the splicing component 10 is a triangle, including the case where the boundary of the splicing component 10 is not chamfered; of course, it may also include the case where the boundary of the splicing component 10 is chamfered. For example: since the splicing component 10 is a triangle, the splicing component 10 has three corners, and a fillet or an oblique chamfer can be made at the corners.

[0082] Please refer to Figures 4 to 7, in an embodiment of the present application, a part of the splicing component 10 encloses to form a conical structure 13 with one end open, and another part of the splicing component 10 encloses to form an annular structure 14 with both ends open. 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 seating cavity 11, and the end of the annular structure 14 away from the conical structure 13 encloses to form a communication port 12.

[0083] In this embodiment, the conical structure 13 is formed by enclosing the splicing component 10, so that the space enclosed by the splicing component 10 can be increased in the direction towards the user. In this way, the seating cavity 11 can have a relatively large volume to facilitate the subsequent seating 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 ceremony of use and thus being beneficial to improving the user experience. On the basis of enclosing the splicing component 10 to form the conical structure 13, further enclosing to form the annular structure 14 can further increase the volume of the seating cavity 11. At the same time, through this annular structure 14, it is also convenient to directly or indirectly provide a seating position for the user (when indirectly providing a seating position, a seat 70 can be further arranged in the seating cavity 11 as introduced above), further facilitating the seating of the user. At this time, such a setting can also further improve the novelty of the shape of the cockpit 100, further enhancing the sense of ceremony of use and being beneficial to improving the user experience. Of course, the present application is not limited to this. In other embodiments, the splicing component 10 can only enclose to form a conical structure 13 with one end open. At this time, the communication port 12 can be formed by enclosing the open end of the conical structure 13.

[0084] Please refer to Figure 6 and Figure 7 , in an embodiment of the present application, when the splicing component 10 encloses to form the conical structure 13 and the annular structure 14, define the number of the splicing component 10 in the conical structure 13 as X, and the number of the splicing component 10 in the annular structure 14 as Y, satisfying the relationship: Y = 2X.

[0085] In this embodiment, setting the number of the splicing component 10 in the annular structure 14 to be twice the number of the splicing component 10 in the conical structure 13 can facilitate the adaptation and splicing of the annular structure 14 and the conical structure 13, and at the same time, the number of the splicing component 10 in the annular structure 14 is not too large, which is beneficial to improving the convenience of splicing. Among them, the number of the splicing component 10 in the conical structure 13 can be 5, so that the communication port 12 with a pentagonal projection required can be conveniently enclosed by a relatively small number of splicing components 10.

[0086] Please refer to Figure 8, in an embodiment of the present application, the shapes of the splicing components 10 are all isosceles triangles, and the sizes of the splicing components 10 are equal.

[0087] In this embodiment, the splicing components 10 are set as isosceles triangles, and the sizes of the splicing components 10 are equal, which can make the splicing components 10 more regular, so as to facilitate the subsequent adaptation and splicing between the splicing components 10, and thus is beneficial to improving the convenience of splicing.

[0088] Please refer to Figure 8 , in an embodiment of the present application, the shapes of the splicing components 10 are all equilateral triangles.

[0089] In this embodiment, the splicing components 10 are further set as equilateral triangles, so that the three side lengths of the splicing components 10 are the same. In this way, when splicing through the splicing components 10, there is no need to consider the directionality of the splicing components 10, and thus it is beneficial to further improve the convenience of splicing.

[0090] Please refer to Figure 8 , in an embodiment of the present application, the adjacent corners of the plurality of splicing components 10 are connected.

[0091] In this embodiment, the adjacent corners of the splicing components 10 are connected, so that one connection position can connect a plurality of splicing components 10, which is beneficial to improving the convenience of connecting the splicing components 10. Especially when using the connecting piece 30 for connection and assembly as introduced below, the number of the connecting pieces 30 can be further simplified. Of course, it should be noted that the present application is not limited to this. In other embodiments, the adjacent splicing components 10 can also be connected through adjacent sides.

[0092] Please refer to in combination Figures 8 to 10 , in an embodiment of the present application, the position where the adjacent corners of the plurality of splicing components 10 are close to each other is defined as the connection part 15, and the cockpit 100 further includes a plurality of connecting pieces 30. Each connecting piece 30 is arranged at a connection part 15 and connects the corners of the plurality of splicing components 10 at the connection part 15.

[0093] In this embodiment, the connecting piece 30 facilitates contact with the adjacent corners of the plurality of splicing components 10, and thus facilitates the connection and assembly of the adjacent plurality of splicing components 10. At the same time, such a setting also makes it unnecessary to stack the adjacent splicing components 10, and thus it is more convenient for the cooperation and arrangement between the splicing components 10.

[0094] Please refer to Figure 10, in an embodiment of the present application, the connecting member 30 includes an arc surface 30a protruding towards the outside of the riding cavity 11, and the adjacent corners of the plurality of splicing components 10 are spaced apart so that the arc surface 30a is exposed to the outside.

[0095] In this embodiment, the adjacent corners of the plurality of splicing components 10 are spaced apart, so that the adjacent corners of the plurality of splicing components 10 will not be spliced to form a sharp corner. Especially when the convex arc surface 30a of the connecting member 30 is exposed at the boundary of the plurality of splicing components 10, 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, and thus is beneficial to improving the safety of using the cockpit 100. At the same time, the convex arc surface 30a exposed to the outside, 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 sense of ceremony of using the splicing component 10. Among them, in order to improve the exposure effect of the connecting member 30, 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, thus being beneficial to improving the service life and safety of the splicing component 10.

[0096] Please refer to Figure 10 , in an embodiment of the present application, the connecting member 30 includes a main body plate 31 and a connecting plate 33. The main body plate 31 forms an arc surface 30a; the connecting plate 33 is a flat plate, and the number of the connecting plates 33 is multiple. The multiple connecting plates 33 are all connected to the edge of the main body plate 31, and the corner of each splicing component 10 in the connection part 15 is correspondingly connected to a connecting plate 33.

[0097] In this embodiment, the connecting member 30 is provided to include a main body plate 31 and a connecting plate 33. Through the main body plate 31, a required convex arc surface 30a can be formed. At the same time, a plurality of connecting plates 33 can also be connected through the main body plate 31, so that the plurality of 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. And 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. Moreover, the connecting plate 33 is also a flat plate. At this time, both the connecting plate 33 and the splicing component 10 are plate body structures of the same type, so that the connecting plate 33 can better contact the splicing component 10, which is beneficial to improving the convenience and stability of the connection between the two. Among them, the connecting plate 33 can be stacked on the outside or inside of the splicing component 10, and of course, it can also extend into the splicing component 10. The present application does not limit the connection position of the connecting plate 33 on the splicing component 10. In addition, the connecting plate 33 and the splicing component 10 can be connected by screws, and of course, they can also be connected by buckles, or by adhesive connection, etc. The present application does not limit the connection method between the connecting plate 33 and the splicing component 10. And the connecting plate 33 and the main body plate 31 can be an integral structure to enhance the overall strength of the connecting member 30, and at the same time improve the production efficiency through integral molding manufacturing.

[0098] Please refer to Figure 10 , in an embodiment of the present application, the connecting member 30 further includes a plurality of reinforcing plates 35. Each reinforcing plate 35 connects the main body plate 31 and two adjacent connecting plates 33, and the reinforcing plate 35 is a convex arc plate.

[0099] In this embodiment, 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 carry and connect the adjacent splicing components 10. And by setting the reinforcing plate 35 as a convex arc plate, it is convenient to connect with the main body plate 31 having an arc plate structure and the connecting plates 33 having a flat plate structure at various circumferential positions thereof.

[0100] Please refer to Figure 10, in an embodiment of the present application, in order to better facilitate the exposure of the main body plate 31 of the connecting member 30 at the connection 15 between multiple splicing components 10, two adjacent splicing components 10 may be arranged at intervals. At this time, in order to improve the sealing performance of the riding cavity 11, the cockpit 100 may further include a covering member 40. The covering member 40 may be arranged between two adjacent splicing components 10 and extend along two opposite sides of the two splicing components 10, and both ends of the covering member 40 in its extending direction may be respectively connected to two reinforcing plates 35 of the two connecting members 30. Among them, in order to facilitate the adaptive connection between the covering member 40 and the reinforcing plates 35 of the two connecting members 30, the connecting member 30 may be an arc-shaped plate that is convex as a whole, or an arc-shaped plate that is convex in the area corresponding to the reinforcing plate 35.

[0101] The present application also proposes an entertainment system. The entertainment system includes a cockpit 100. The specific structure of the cockpit 100 refers to the above embodiments. Since this entertainment system adopts all the technical solutions of the above all embodiments, it has at least all the beneficial effects brought by the technical solutions of the above embodiments, which will not be elaborated here one by one. Among them, the entertainment system may further include a head-mounted display device, a VR device or an AR device. At this time, the user can use the head-mounted display device more conveniently while sitting in the cockpit 100. Of course, the entertainment system may also include a projector. At this time, the user can watch the movie projected by the projector while sitting in the cockpit 100.

[0102] The above are only the preferred embodiments of the present invention, and do not limit the patent scope of the present invention accordingly. Any equivalent structural transformation made by using the specification and drawings of the present invention under the inventive concept of the present invention, or direct / indirect application in other related technical fields, is included in the patent protection scope of the present invention.

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 seating cavity and a communication port, and the communication port communicates with the seating cavity; In the direction from the end of the cockpit where the communication port is provided to the end away from the communication port, the projection of the communication port is a pentagon.

2. The cockpit according to claim 1, characterized in that, The projection of the communication port is a regular pentagon.

3. The cockpit according to claim 1, characterized in that, The communication port is a plane.

4. The cockpit according to claim 3, characterized in that, It is defined that the cockpit has an up-down direction and a horizontal direction, and the plane where the communication port is located is arranged at an angle with both the up-down direction and the horizontal direction.

5. The cockpit according to claim 4, characterized in that, It is defined that the angle formed by the plane where the communication port is located and the up-down direction is α, and it satisfies the relationship: 0° < α ≤ 30°.

6. The cockpit according to any one of claims 1 to 5, characterized in that The cockpit includes five inner sides at the communication port, and two adjacent inner sides enclose an inner angle; It is defined that the cockpit has an up-down direction and a horizontal direction, and one of the inner sides extends horizontally and is located below the opposite inner angle.

7. The cockpit according to claim 6, characterized in that, It is defined that the inner side extending horizontally is the bottom side, and the cockpit further includes a seat, and the seat is arranged in the seating cavity and is connected to the splicing component forming the bottom side.

8. The cockpit according to claim 7, characterized in that, Part of the seat protrudes from the bottom side out of the communication port.

9. The cockpit according to claim 8, characterized in that, The seat includes: a cushion part, the cushion part is connected to the splicing component forming the bottom side, and one end of the cushion part protrudes from the bottom side out of the communication port; and a backrest part, the backrest part protrudes from one end of the cushion part away from the communication port.

10. The cockpit according to claim 7, characterized in that, The cockpit further includes a support structure, and the support structure is arranged outside the seating cavity and is connected to the splicing component forming the bottom side.

11. The cockpit according to claim 6, characterized in that, Five of the plurality of splicing components enclose to form the communication port, and one side of each of the five splicing components forms the inner side.

12. The cockpit according to any one of claims 1 to 5, characterized in that, The shape of each splicing component is a triangle.

13. The cockpit according to claim 12, characterized in that, The splicing components enclose to form a conical structure with one end open, and the end of the conical structure with the opening encloses to form the communication port; Alternatively, part of the splicing components enclose to form a conical structure with one end open, and another part 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 end of the conical structure with the opening; 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.

14. The cockpit according to claim 13, characterized in that, When the splicing components enclose to form a conical structure and an annular structure, it is defined that the number of splicing components in the conical structure is X, and the number of splicing components in the annular structure is Y, and it satisfies the relationship: Y = 2X.

15. The cockpit according to claim 14, characterized in that, The shape of each splicing component is an isosceles triangle, and the size of each splicing component is equal.

16. The cockpit according to claim 15, characterized in that, The shape of each splicing component is an equilateral triangle.

17. The cockpit according to claim 12, characterized in that, The adjacent corners of the plurality of splicing components are connected.

18. The cockpit according to claim 17, wherein It is defined that the position where the adjacent corners of the plurality of splicing components are close to each other is the connection part, and the cockpit further includes a plurality of connectors, and each connector is arranged at one connection part and connects the corners of the plurality of splicing components at the connection part.

19. The cockpit according to claim 18, characterized in that, The connecting member includes an arc surface protruding toward the outside of the riding cavity, and the adjacent corners in the plurality of splicing components are spaced apart so that the arc surface is exposed to the outside.

20. An entertainment system, characterized in that, It includes a cockpit according to any one of claims 1 to 19.

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