Cabin structure and vehicle

Abstract

According to the technical scheme, the cabin structure comprises a main shell, the main shell comprises a first side face located on one side in the first direction, and a module installation hole is formed in the first side face; the first display module is arranged on the main shell, the display surface of the first display module is exposed out of the main shell through the module mounting hole, the ratio of the long side size to the short side size of the display surface is larger than or equal to 4, the long side of the display surface extends in the second direction, and the second direction intersects with the first direction; the first display module is connected with the main shell through the support; the windshield is located on one side, in the third direction, of the main shell, and the third direction intersects with the first direction and the second direction.

Description

Technical Field

[0001] The present disclosure relates to the technical field of cockpits, and in particular, to a cockpit structure and a vehicle. Background Art

[0002] A Head-up Display (HUD) can project current driving information and other information onto a certain distance in front through the windshield, such as vehicle speed, engine speed, remaining range, tire pressure, navigation, multimedia and other interactive information. During driving, the driver no longer needs to look down at the traditional instrument panel or in-vehicle computer, and can obtain driving information through the projected image in front. In this way, the driver can keep their attention on the road ahead all the time, thus avoiding accidents caused by looking down at the instrument during driving and greatly improving driving safety. How to stably install the display screen of the head-up display in the cockpit through structural design is one of the topics that the R & D personnel of display products are concerned about.

[0003] The above information disclosed in this section is only for understanding the background of the inventive concept of the present disclosure. Therefore, the above information may include information that does not constitute the prior art. Summary of the Invention

[0004] In one aspect, there is provided a cockpit structure, the cockpit structure comprising:

[0005] A main housing, the main housing including a first side surface on one side in a first direction, and a module mounting hole is provided on the first side surface;

[0006] A first display module, disposed on the main housing, a display surface of the first display module is exposed outside the main housing through the module mounting hole, a ratio of a long side dimension to a short side dimension of the display surface is greater than or equal to 4, and a long side of the display surface extends along a second direction, and the second direction intersects the first direction;

[0007] A bracket, the first display module is connected to the main housing through the bracket; and

[0008] A windshield, located on one side of the main housing in a third direction, and the third direction intersects both the first direction and the second direction.

[0009] According to some exemplary embodiments, the main housing includes a second side surface, and the second side surface and the first side surface are respectively located on both sides of the first direction; and

[0010] The display surface of the first display module is inclined with respect to the horizontal plane, and a side of the first display module close to the windshield is closer to the second side surface than a side of the first display module away from the windshield.

[0011] According to some exemplary embodiments, a receiving space is included in the main housing, a skirt structure is provided at the module mounting hole, the skirt structure at least partially surrounds the module mounting hole and protrudes into the receiving space of the main housing, and a protruding distance of the skirt structure on a side close to the windshield is less than a protruding distance of the skirt structure on a side away from the windshield; and

[0012] The first display module is connected to the skirt structure through the bracket.

[0013] According to some exemplary embodiments, the bracket is annular, the bracket is connected to an edge of the first display module, the bracket includes fixing portions protruding from two sides of the first display module along the third direction, and the fixing portions are connected to the skirt structure.

[0014] According to some exemplary embodiments, the fixing portion on a side away from the windshield along the third direction includes a plurality of fixing sub-portions arranged at intervals, an abutting portion is provided between adjacent fixing sub-portions, the abutting portion is perpendicularly arranged with respect to the fixing sub-portions, and the abutting portion is fixedly connected to a side surface of the second display module on a side away from the windshield

[0015] According to some exemplary embodiments, the cockpit structure further includes at least one support member, and at least one of the support members is located in the receiving space; and

[0016] One side of the support member is connected to a side of the first display module facing away from the display surface, and one side of the support member is connected to a second side surface of the main housing.

[0017] According to some exemplary embodiments, the support member includes a first support member and a second support member connected along the first direction;

[0018] The first support member includes a first strip-shaped member and a second strip-shaped member, the first strip-shaped member and the second strip-shaped member are perpendicularly connected, an extending direction of the first strip-shaped member is parallel to a horizontal plane, one end of the first strip-shaped member away from the second strip-shaped member is connected to a side of the first display module away from the windshield, and one end of the second strip-shaped member away from the first strip-shaped member is connected to a side of the first display module close to the windshield; and

[0019] The second support member includes a third strip-shaped member, a fourth strip-shaped member, and a fifth strip-shaped member, the third strip-shaped member and the fifth strip-shaped member are arranged at intervals along the first direction, the fourth strip-shaped member is connected between the third strip-shaped member and the fifth strip-shaped member, the third strip-shaped member is connected to a side of the first strip-shaped member away from the first display module, and the fifth strip-shaped member is connected to the second side surface.

[0020] According to some exemplary embodiments, one end of the fourth bar-shaped member is connected to one end of the third bar-shaped member away from the windshield, and the other end of the fourth bar-shaped member is connected to one end of the fifth bar-shaped member away from the windshield.

[0021] According to some exemplary embodiments, a first hollow hole is provided on the second side surface. The cockpit structure further includes a metal bottom plate, the metal bottom plate is provided on the second side surface and covers the first hollow hole, and one side of the second support member away from the first display module is connected to the metal bottom plate.

[0022] According to some exemplary embodiments, the cockpit structure includes at least two of the support members, and at least two of the support members are spaced apart along the second direction; and

[0023] The cockpit structure further includes at least one reinforcing plate, the reinforcing plate is located between at least two of the support members, and the reinforcing plate is connected to a side of the first display module facing away from the display surface.

[0024] According to some exemplary embodiments, the size of the reinforcing plate along the second direction is greater than the size of the support member along the second direction

[0025] According to some exemplary embodiments, the main housing includes a third side surface, along the third direction, the third side surface is located on a side away from the windshield, a second hollow hole is provided on the third side surface, and the size of the second hollow hole along the second direction is greater than the size of the module mounting hole along the second direction.

[0026] According to some exemplary embodiments, the main housing includes a fourth side surface, along the third direction, the fourth side surface is located on a side close to the windshield, at least two third hollow holes are provided on the fourth side surface, and at least two of the third hollow holes are spaced apart along the second direction.

[0027] According to some exemplary embodiments, the included angle between the display surface of the first display module and the horizontal plane is less than or equal to 10°; and / or,

[0028] The included angle between the windshield and the horizontal plane is greater than or equal to 30° and less than or equal to 45°.

[0029] According to some exemplary embodiments, the cockpit structure further includes two side plates, the two side plates are respectively connected to two sides of the main housing along the second direction, and the side plates extend in a direction away from the windshield;

[0030] The cockpit structure further includes two second display modules, which are respectively arranged on the two side plates, and the second display module is arranged on one side of one side plate away from the other side plate; and

[0031] The side plate is provided with a fourth hollow hole, and the fourth hollow hole exposes the display surface of the second display module.

[0032] According to some exemplary embodiments, the cockpit structure further includes a control board, the control board is arranged on the side plate, and the control board is electrically connected to the second display module.

[0033] According to some exemplary embodiments, the side plate is provided with a fifth hollow hole, and the fifth hollow hole exposes at least a part of the control board.

[0034] According to some exemplary embodiments, the cockpit structure includes a first cover plate assembly, the first cover plate assembly is arranged on the side of the main housing away from the windshield, and the first cover plate assembly is bent away from the windshield in both sides in the second direction and covers the two side plates; and

[0035] The first cover plate assembly is provided with a sixth hollow hole, and the sixth hollow hole exposes the display surface of the second display module.

[0036] According to some exemplary embodiments, the first cover plate assembly includes a first cover plate, a second cover plate and a light bar assembly, the first cover plate and the second cover plate are connected along a first direction, and the light bar assembly is arranged between the first cover plate and the second cover plate.

[0037] According to some exemplary embodiments, the first cover plate is connected to one side of the first side surface of the main housing, and the first cover plate is provided with a seventh hollow hole, and the dimension of the seventh hollow hole along the second direction is greater than the dimension of the first display module along the second direction.

[0038] On the other hand, a vehicle is provided, wherein the vehicle includes the cockpit structure as described in any one of the above.

[0039] According to some exemplary embodiments, BRIEF DESCRIPTION OF THE DRAWINGS

[0040] Other objects and advantages of the present disclosure will be apparent from the following description with reference to the drawings, and can help to have a comprehensive understanding of the present disclosure.

[0041] Figure 1 Schematically shows a perspective view of a cockpit structure according to some embodiments of the present disclosure.

[0042] Figure 2Schematically shows a rear view of a cockpit structure according to some embodiments of the present disclosure.

[0043] Figure 3 Schematically shows a left view of a cockpit structure according to some embodiments of the present disclosure.

[0044] Figure 4 Schematically shows a display principle diagram of a first display module of a cockpit structure according to some embodiments of the present disclosure.

[0045] Figure 5 Schematically shows a structural diagram of a main housing of a cockpit structure according to some embodiments of the present disclosure.

[0046] Figure 6 Schematically shows an assembly schematic diagram of a main housing and a first display module of a cockpit structure according to some embodiments of the present disclosure.

[0047] Figure 7 Schematically shows a combined structural diagram of a main housing and a first display module of a cockpit structure according to some embodiments of the present disclosure.

[0048] Figure 8 Schematically shows an assembly schematic diagram of a first display module and a bracket of a cockpit structure according to some embodiments of the present disclosure.

[0049] Figure 9 Schematically shows a combined structural diagram of a first display module and a bracket of a cockpit structure according to some embodiments of the present disclosure.

[0050] Figure 10 Schematically shows a combined side view of a first display module, a first support member of a cockpit structure according to some embodiments of the present disclosure.

[0051] Figure 11 Schematically shows a combined structural diagram of a first display module, a first support member, and a reinforcing plate of a cockpit structure according to some embodiments of the present disclosure.

[0052] Figure 12 Schematically shows a combined structural diagram of a first display module, a first support member, a reinforcing plate, and an FPGA board of a cockpit structure according to some embodiments of the present disclosure.

[0053] Figure 13 Schematically shows an exploded view of a metal bottom plate of a cockpit structure according to some embodiments of the present disclosure.

[0054] Figure 14 Schematically shows a structural diagram of a metal bottom plate of a cockpit structure according to some embodiments of the present disclosure.

[0055] Figure 15Schematically shows another exploded view of the metal bottom plate of the cockpit structure according to some embodiments of the present disclosure.

[0056] Figures 16 - 18 Schematically shows an assembly schematic diagram of the metal bottom plate and the main housing of the cockpit structure according to some embodiments of the present disclosure.

[0057] Figure 19 Schematically shows a structural diagram of the back plate of the first display module of the cockpit structure according to some embodiments of the present disclosure.

[0058] Figure 20 Schematically shows a side view of the back plate of the first display module of the cockpit structure according to some embodiments of the present disclosure.

[0059] Figure 21 Schematically shows Figure 20 an enlarged view of area B in

[0060] Figure 22 Schematically shows an assembly diagram of the first display module of the cockpit structure according to some embodiments of the present disclosure.

[0061] Figure 23 Schematically shows Figure 22 an enlarged view of area C in

[0062] Figure 24 Schematically shows an exploded view of the first cover plate assembly of the cockpit structure according to some embodiments of the present disclosure.

[0063] Figure 25 Schematically shows a structural diagram of the first cover plate assembly of the cockpit structure according to some embodiments of the present disclosure.

[0064] Figures 26 - 27 Schematically shows an assembly schematic diagram of the first cover plate assembly and the main housing of the cockpit structure according to some embodiments of the present disclosure.

[0065] Figure 28 Schematically shows an assembly schematic diagram of the first cover plate and the first decorative plate of the cockpit structure according to some embodiments of the present disclosure.

[0066] Figure 29 Schematically shows a structural diagram of the light bar assembly of the cockpit structure according to some embodiments of the present disclosure.

[0067] Figure 30 Schematically shows along Figure 29 a cross-sectional view taken along the direction DD' in

[0068] Figure 31 Schematically shows a structural diagram of the A-pillar support of the cockpit structure according to some embodiments of the present disclosure.

[0069] Figure 32 Schematically shows an assembly diagram of an A-pillar support and a main housing of a cockpit structure according to some embodiments of the present disclosure.

[0070] Figure 33 Schematically shows a structural diagram of a combination of an A-pillar support and a main housing of a cockpit structure according to some embodiments of the present disclosure.

[0071] Figure 34 Schematically shows an assembly diagram of an air outlet frame and a front housing of a cockpit structure according to some embodiments of the present disclosure.

[0072] Figure 35 Schematically shows an assembly diagram of an air outlet frame and a main housing of a cockpit structure according to some embodiments of the present disclosure.

[0073] Figure 36 Schematically shows an assembly diagram of an A-pillar decorative frame and an A-pillar support of a cockpit structure according to some embodiments of the present disclosure.

[0074] Figure 37 Schematically shows Figure 36 An enlarged view of area E in

[0075] Figure 38 Schematically shows along Figure 37 A cross-sectional view taken along the direction FF' in

[0076] Figure 39 Schematically shows an assembly diagram of a second display module, a control board and a side plate of a cockpit structure according to some embodiments of the present disclosure.

[0077] Figure 40 Schematically shows Figure 39 An enlarged view of area G in

[0078] Figure 41 Schematically shows a combined structural diagram of a second display module, a control board and a side plate of a cockpit structure according to some embodiments of the present disclosure.

[0079] Figure 42 Schematically shows Figure 41 An enlarged view of area H in

[0080] Figure 43 Schematically shows an exploded view of a second display module of a cockpit structure according to some embodiments of the present disclosure.

[0081] Figure 44 Schematically shows a physical diagram of a second display module of a cockpit structure according to some embodiments of the present disclosure.

[0082] Figure 45Schematically shows an internal structure diagram of the main housing of a cockpit structure according to some embodiments of the present disclosure.

[0083] Figure 46 Schematically shows an assembly schematic diagram of a steering wheel grip of a cockpit structure according to some embodiments of the present disclosure.

[0084] Figure 47 Schematically shows a structure diagram of a steering wheel grip of a cockpit structure according to some embodiments of the present disclosure.

[0085] Figure 48 Schematically shows along Figure 47 A cross-sectional view taken along the JJ' direction.

[0086] It should be noted that, for clarity, in the drawings used to describe the embodiments of the present disclosure, the dimensions of layers, structures, or regions may be enlarged or reduced, that is, these drawings are not drawn to actual scale. Detailed implementation manners

[0087] In the following description, for purposes of explanation, numerous specific details are set forth to provide a thorough understanding of various exemplary embodiments. However, it is evident that the various exemplary embodiments can be practiced without these specific details or with one or more equivalent arrangements. In other instances, well-known structures and devices are shown in block diagram form to avoid unnecessarily obscuring the various exemplary embodiments. Additionally, the various exemplary embodiments can be different, but not necessarily exclusive. For example, specific shapes, configurations, and characteristics of an exemplary embodiment can be used or implemented in another exemplary embodiment without departing from the inventive concept.

[0088] In the drawings, for clarity and / or descriptive purposes, the dimensions of elements can be enlarged and relative dimensions. Thus, the dimensions and relative dimensions of the respective elements do not have to be limited to the dimensions and relative dimensions shown in the drawings. When the exemplary embodiments can be implemented differently, the specific process sequences can be performed in a different order than described. For example, two consecutively described processes can be performed substantially simultaneously or in an order opposite to the described order. Additionally, the same reference numerals denote the same elements.

[0089] When an element is described as being "on", "connected to", or "coupled to" another element, the element can be directly on, directly connected to, or directly coupled to the other element, or there may be intervening elements. However, when an element is described as being "directly on", "directly connected to", or "directly coupled to" another element, there are no intervening elements. Other terms and / or expressions used to describe the relationship between elements should be interpreted in a similar manner, e.g., "between" versus "directly between", "adjacent" versus "directly adjacent", or "on" versus "directly on", etc. In addition, the term "connected" can refer to physical connection, electrical connection, communication connection, and / or fluid connection. In addition, the X-axis, Y-axis, and Z-axis are not limited to the three axes of a rectangular coordinate system and can be interpreted in a broader sense. For example, the X-axis, Y-axis, and Z-axis can be perpendicular to each other, or can represent different directions that are not perpendicular to each other. For the purposes of this disclosure, "at least one of X, Y, and Z" and "at least one selected from the group consisting of X, Y, and Z" can be interpreted as only X, only Y, only Z, or any combination of two or more of X, Y, and Z such as XYZ, XY, YZ, and XZ. As used herein, the term "and / or" includes any combination and all combinations of one or more of the listed related items.

[0090] It should be understood that although the terms first, second, etc. may be used herein to describe different elements, these elements should not be limited by these terms. These terms are only used to distinguish one element from another. For example, without departing from the scope of the exemplary embodiments, the first element can be named the second element, and similarly, the second element can be named the first element.

[0091] Figure 1 A perspective view of a cockpit structure according to some embodiments of the present disclosure is schematically shown. FIG. Figure 2 A rear view of a cockpit structure according to some embodiments of the present disclosure is schematically shown. Figure 3 A left view of a cockpit structure according to some embodiments of the present disclosure is schematically shown.

[0092] Figure 4 A display principle diagram of a first display module of a cockpit structure according to some embodiments of the present disclosure is schematically shown. Figure 5 A structural diagram of a main housing of a cockpit structure according to some embodiments of the present disclosure is schematically shown. Figure 6 An assembly schematic diagram of a main housing and a first display module of a cockpit structure according to some embodiments of the present disclosure is schematically shown. Figure 7Schematically shows a combined structure diagram of a main housing and a first display module of a cockpit structure according to some embodiments of the present disclosure. Among them, in order to more clearly illustrate the assembly process of the first display module and the main housing, Figure 6 and Figure 7 the main housing and the first display module shown in are turned upside down. The second side surface located on the upper side in the main housing should actually be located on the lower side, and the side surface of the first display module located on the upper side should actually be the lower side surface on the back of the display surface.

[0093] Figure 8 Schematically shows an assembly schematic diagram of a first display module and a bracket of a cockpit structure according to some embodiments of the present disclosure. Figure 9 Schematically shows a combined structure diagram of a first display module and a bracket of a cockpit structure according to some embodiments of the present disclosure. Figure 10 Schematically shows a combined side view of a first display module and a first support member of a cockpit structure according to some embodiments of the present disclosure. Figure 11 Schematically shows a combined structure diagram of a first display module, a first support member, and a reinforcing plate of a cockpit structure according to some embodiments of the present disclosure. Figure 12 Schematically shows a combined structure diagram of a first display module, a first support member, a reinforcing plate, and an FPGA board of a cockpit structure according to some embodiments of the present disclosure.

[0094] With reference to Figure 1 , Figure 5 , Figure 6 and Figure 7 , the cockpit structure includes a main housing 10, a first display module 21, a bracket 30, and a windshield WS. The main housing 10 includes a first side surface 11 on one side in the first direction D1, and the first side surface 11 is provided with a module mounting hole 111. The first display module 21 is mounted at the module mounting hole 111 of the main housing 10 through the bracket 30, and the display surface of the first display module 21 is exposed outside the main housing 10 through the module mounting hole 111. The ratio of the long side dimension to the short side dimension of the display surface is greater than or equal to 4, and the long side of the display surface extends along the second direction D2, and the second direction D2 intersects with the first direction D1. The windshield WS is located on one side of the main housing 10 along the third direction D3, and the third direction D3 intersects with both the first direction D1 and the second direction D2.

[0095] It should be noted that when the driver is sitting in the cockpit structure and facing the windshield WS, the first direction D1 is the up-down direction, the second direction D2 is the left-right direction, and the third direction D3 is the front-back direction. In addition, when the cockpit structure is applied in a vehicle, the main housing 10 is the main housing 10 of the center console, the material of the main housing 10 may include at least one of ABS plastic and PC plastic, and the windshield WS is the front windshield.

[0096] By hiding the first display module 21 inside the main housing 10 and projecting it onto the windshield WS as a picture source, since the ratio of the long side dimension to the short side dimension of the display surface of the first display module 21 is greater than or equal to 4, the display surface of the first display module 21 has a relatively large dimension along the second direction D2, so that a display effect of panoramic head-up display (PHUD) covering from pillar to pillar can be presented. In this way, information such as instrument information, navigation information, and multimedia entertainment information can be simultaneously displayed on the windshield WS, so as to avoid the problem of potential safety hazards caused by looking down at the central control screen during driving. For example, the instrument information can be displayed in front of the driver's seat, the multimedia entertainment information can be displayed in front of the passenger seat, and the navigation information is displayed between the instrument information and the multimedia entertainment information.

[0097] According to some exemplary embodiments, with reference to Figure 1 , Figure 4 and Figure 7 , the main housing 10 includes a second side surface 12. The second side surface 12 and the first side surface 11 are respectively located on both sides of the first direction D1. The first side surface 11 is located closer to the windshield WS, and the second side surface 12 is located farther from the windshield WS. The display surface 21a of the first display module 21 is inclined with respect to the horizontal plane. The side of the first display module 21 closer to the windshield WS is closer to the second side surface 12 than the side of the first display module 21 farther from the windshield WS, that is, the installation height of the side of the first display module 21 farther from the windshield WS is lower than the installation height of the side of the first display module 21 farther from the windshield WS. In this way, the optical requirements for projecting the display picture of the first display module 21 onto the windshield WS can be met.

[0098] According to some exemplary embodiments, with reference to Figure 4 , according to the inventor's research, in order to ensure that the display picture of the first display module 21 can be clearly projected onto the windshield WS, the installation angle and installation position of the first display module 21 and the windshield WS need to meet the following requirements:

[0099] The included angle α between the windshield WS and the horizontal plane is greater than or equal to 30° and less than or equal to 45°, the included angle β between the display surface 21a of the first display module 21 and the horizontal plane is less than or equal to 10°, and the included angle γ between the display surface 21a of the first display module 21 and the windshield WS is greater than or equal to 30° and less than or equal to 55°.

[0100] The distance between the display surface 21a of the first display module 21 and the windshield WS along the third direction D3 is L1. L1 should satisfy 10mm ≤ L1 ≤ 40mm. The smaller L1 is, the lower the imaging will be. The distance between the driver's eyeball and the windshield WS along the third direction D3 is L2. L2 should satisfy 600mm ≤ L2 ≤ 900mm and can be adjusted according to the driving habits of different people. The distance between the side of the display surface of the first display module 21 close to the windshield WS and the driver's eyeball along the first direction D1 is L3. L3 should satisfy 200mm ≤ L3 ≤ 400mm.

[0101] According to some exemplary embodiments, with reference to Figure 1 , a shielding plate 17 is further provided on the first side surface 11 of the main housing 10. The shielding plate 17 is disposed on the side of the first display module 21 away from the windshield WS and can be adhesively fixed to the main housing 10. The shielding plate 17 is used to prevent the light emitted by the first display module 21 from affecting the driver's observation of the projection imaging effect on the windshield WS. In this way, when the driver uses the PHUD, the driver can only see the image data on the windshield WS and cannot directly see the image of the first display module 21, thus minimizing the behavior of looking down while driving and maximizing the safety environment for the driver during driving, and improving the user's driving experience.

[0102] According to some exemplary embodiments, in combination with reference to Figure 1 , Figure 5 , Figure 6 and Figure 7 , the main housing 10 is of a frame structure. The main housing 10 includes an accommodation space 10a. A skirt structure 15 is provided at the module mounting hole 111. The skirt structure 15 at least partially surrounds the module mounting hole 111 and protrudes into the accommodation space 10a of the main housing 10. The first display module 21 is connected to the skirt structure 15 through a bracket 30. The skirt structure 15 includes a first skirt 151 on the side close to the windshield WS and a second skirt 152 on the side away from the windshield WS. The protruding distance of the first skirt 151 is less than the protruding distance of the second skirt 152. The skirt structure 15 further includes a third skirt 153 and a fourth skirt 154. The third skirt 153 and the fourth skirt 154 are respectively disposed on both sides of the module mounting hole 111 along the second direction D2. The third skirt 153 and the fourth skirt 154 connect the first skirt 151 and the second skirt 152 respectively. Along the direction from the second skirt 152 to the first skirt 151, the protruding distances of the third skirt 153 and the fourth skirt 154 gradually decrease. In this way, the first display module 21 can be tightly and stably fixed to the skirt structure 15 of the main housing 10 through the bracket 30, thereby effectively preventing the deformation of the first display module 21 and enabling the display surface of the first display module 21 to be inclined in a predetermined direction.

[0103] According to some exemplary embodiments, in combination with reference Figure 6 , Figure 8 and Figure 9 The bracket 30 is annular and connected to the edge of the first display module 21 . The bracket 30 includes fixing portions 31 protruding from both sides of the first display module 21 along the third direction D3 . The fixing portions 31 are connected to the skirt structure 15 .

[0104] According to some exemplary embodiments, in combination with reference Figure 1 , Figure 8 and Figure 9 The fixing portion 31 on the side away from the windshield WS along the third direction D3 includes a plurality of fixing sub-portions 311 arranged at intervals, and an abutting portion 32 is arranged between adjacent fixing sub-portions 311, and the abutting portion 32 is arranged vertically with the fixing sub-portions 311, and the abutting portion 32 can be fixedly connected with the side of the second display module 22 away from the windshield WS by screws. The abutting portion 32 is fixed and abutted with the side of the second display module 22 with a lower height, which can effectively prevent the first display module 21 from loosening, sliding, and other problems with the extension of the use time. On the other side along the third direction D3 and on both sides along the second direction D2, the bracket 30 is fixedly connected with the back of the second display module 22 by screws.

[0105] For example, the bracket 30 is provided with four abutting portions 32 on the side away from the windshield WS, and the four abutting portions 32 are fixedly connected to the side of the second display module 22 away from the windshield WS by four screws S01 respectively. On the other three sides where no abutting portions 32 are provided, the bracket 30 is fixedly connected to the side of the second display module 21 away from its display surface by 12 screws S02.

[0106] According to some exemplary embodiments, in combination with reference Figure 6 , Figure 7 and Figure 9 The second skirt 152 is provided with a plurality of notches 1521 arranged at intervals, and the plurality of notches 1521 are arranged corresponding to the plurality of abutting portions 32 , and the notches 1521 are avoidance structures arranged corresponding to the abutting portions 32 .

[0107] According to some exemplary embodiments, referring to Figure 6 Before installing the first display module 21 and the main shell 10, a single-sided foam 18 is pasted on the contact surface between the main shell 10 and the first display module 21. The single-sided foam 18 plays a role of buffering and shock absorption to avoid damage caused by hard contact between the main shell 10 and the first display module 21 during the assembly process.

[0108] Figure 13 An exploded view of a metal floor panel of a cabin structure according to some embodiments of the present disclosure is schematically shown. Figure 14A structural diagram of a metal bottom plate of a cockpit structure according to some embodiments of the present disclosure is schematically shown. Figure 15 Another exploded view of a metal bottom plate of a cockpit structure according to some embodiments of the present disclosure is schematically shown. Figures 16 - 18 An assembly schematic diagram of a metal bottom plate and a main housing of a cockpit structure according to some embodiments of the present disclosure is schematically shown. Among them, in order to more clearly illustrate the assembly process of the metal bottom plate and the main housing, Figure 17 the main housing shown in the figure is turned upside down, and the second side surface located on the upper side in the main housing should actually be located on the lower side.

[0109] According to some exemplary embodiments, with reference to Figure 16 、 Figure 17 and Figure 18 , a first hollow hole LK1 is provided on the second side surface 12 of the main housing 10. The size of the first hollow hole LK1 along the second direction D2 is larger than the size of the module mounting hole 111 along the second direction D2. The cockpit structure further includes a metal bottom plate 16, and the metal bottom plate 16 is disposed on the second side surface 12 and covers the first hollow hole LK1. By providing the metal bottom plate 16, the strength of the main housing 10 can be improved, and the heat dissipation efficiency of related electronic components installed inside the main housing 10 can be improved. For example, the material of the metal bottom plate 16 may include aluminum.

[0110] According to some exemplary embodiments, with reference to Figure 16 and Figure 17 , the metal bottom plate 16 and the second side surface 12 of the main housing 10 are fixed by screws S03, for example, by 26 screws S03. The screws are disposed at the bottom of the metal bottom plate 16, so that the metal bottom plate 16 is reliably connected to the main housing 10, and at the same time, it is ensured that there are no exposed screws on the appearance.

[0111] According to some exemplary embodiments, with reference to Figure 13 and Figure 14 , the metal bottom plate 16 may include a first bottom plate 161 and a second bottom plate 162. The part with a relatively uniform thickness is processed into the first bottom plate 161, and the part exceeding the thickness is split and processed into the second bottom plate 162, and then the second bottom plate 162 is assembled on the first bottom plate 161 by screws or structural adhesive to obtain the metal bottom plate 16. Considering energy conservation, low carbon and environmental protection, the metal bottom plate 16 is designed as a split structure, so that the thickness of the blank material can be reduced, and thus the cost can be reduced. According to this design, the material cost of the metal bottom plate 16 can be saved by 50%, and the processing cost can be saved by more than 60% because there is no need for large-area stock removal, that is, the overall cost can be reduced by more than half.

[0112] According to some exemplary embodiments, with reference to Figure 15 and Figure 16, a silica gel pad 163 is also provided on the side of the metal base plate 16 away from the main housing 10, so as to increase the stability and flatness of the main housing 10.

[0113] According to some exemplary embodiments, with reference to Figure 14 , Figure 16 and Figure 18 , a limiting frame 164 is provided on the side of the metal base plate 16 close to the main housing 10. The shape of the limiting frame 164 is the same as that of the first hollow hole LK1, and the size of the limiting frame 164 is slightly smaller than that of the first hollow hole LK1. The limiting frame 164 can be exactly engaged into the first hollow hole LK1, playing an auxiliary positioning role in the installation process of the metal base plate 16 and the main housing 10, so as to improve the assembly accuracy.

[0114] According to some exemplary embodiments, with reference to Figure 7 , Figure 10 , Figure 11 and Figure 18 , the cockpit structure further includes at least one support member 40. At least one support member 40 is located in the accommodation space 10a of the main housing 10. One side of the support member 40 is connected to the side of the first display module 21 away from the display surface, and one side of the support member 40 is connected to the metal base plate 16 of the second side surface 12 of the main housing 10. The support member 40 supports the back surface of the first display module 21, which can effectively avoid the problem that the first display module 21 deforms over time.

[0115] According to some exemplary embodiments, with reference to Figure 1 , Figure 6 , Figure 7 , Figure 10 , Figure 11 and Figure 18 , the support member 40 includes a first support member 41 and a second support member 42 connected along the first direction D1. The first support member 41 is connected to the first display module 21, and the second support member 42 is connected to the metal base plate 16.

[0116] The first support member 41 includes a first strip member 411 and a second strip member 412, and the first strip member 411 and the second strip member 412 are vertically connected to form an L shape. The extending direction of the first strip member 411 is parallel to the horizontal plane, and one end of the first strip member 411 away from the second strip member 412 is connected to the side of the first display module 21 away from the windshield WS, and one end of the second strip member 412 away from the first strip member 411 is connected to the side of the first display module 21 close to the windshield WS. Exemplarily, one end of the first strip member 411 away from the second strip member 412 is connected to the fixing portion 31 on the side of the bracket 30 away from the windshield WS, and one end of the second strip member 412 away from the first strip member 411 is connected to the fixing portion 31 on the side of the bracket 30 close to the windshield WS.

[0117] The second support member 42 includes a third strip member 421, a fourth strip member 422, and a fifth strip member 423. The third strip member 421 and the fifth strip member 423 are arranged at intervals along the first direction D1, and the extending directions of the third strip member 421 and the fifth strip member 423 are both parallel to the horizontal plane. The fourth strip member 422 is connected between the third strip member 421 and the fifth strip member 423. The third strip member 421 is connected to the side of the first strip member 411 away from the first display module 21, and the fifth strip member 423 is connected to the metal base plate at the second side 12. The support member 40 including the first support member 41 and the second support member 42 can provide a stable support effect for the first display module 21 and is not easily deformed during a long-term support process.

[0118] According to some exemplary embodiments, referring to Figure 1 、 Figure 17 and Figure 18 ,the extending direction of the fourth strip member 422 is perpendicular to the horizontal plane. One end of the fourth strip member 422 is connected to the end of the third strip member 421 away from the windshield WS, and the other end of the fourth strip member 422 is connected to the end of the fifth strip member 423 away from the windshield WS. The second support member 42 is generally in a C shape. Supporting the fourth strip member 422 on the lower side of the first display module 21 can further improve the support stability of the support member 40 for the first display module 21.

[0119] According to some exemplary embodiments. Referring to Figure 11, the cockpit structure includes at least two support members 40, and the at least two support members 40 are arranged at intervals along the second direction D2. The cockpit structure further includes at least one reinforcing plate 43, the reinforcing plate 43 is located between the at least two support members 40, and the reinforcing plate 43 is connected to the side of the first display module 21 facing away from the display surface. The at least two support members 40 respectively support both sides of the first display module 21 along the second direction D2, and the reinforcing plate 43 strengthens the strength of the middle part of the first display module 21. In this way, a stable supporting effect can be achieved for the first display module 21, and at the same time, the strengthening effect of the reinforcing plate 43 can effectively prevent the first display module 21 from deforming.

[0120] According to some exemplary embodiments, referring to Figure 11 , the cross-sectional shape of the reinforcing plate 43 can be the same as the cross-sectional shape of the first support member 41, in an L shape, and the dimension of the reinforcing plate 43 along the second direction D2 is greater than the dimension of the support member 40 along the second direction D2.

[0121] According to some exemplary embodiments, the materials of the support member 40 and the reinforcing plate 43 can include metals.

[0122] According to some exemplary embodiments, referring to Figure 12 , an FPGA board 44 can also be arranged on the side of the reinforcing plate 43 away from the first display module 21, and the FPGA board 44 is fixedly connected to the reinforcing plate 43 by four screws S04.

[0123] According to some exemplary embodiments, in combination with reference to Figure 1 , Figure 5 and Figure 7 , the main housing 10 includes a third side surface 13, the third side surface 13 is located on the side away from the windshield WS along the third direction D3, and a second hollow hole LK2 is provided on the third side surface 13. The dimension of the second hollow hole LK2 along the second direction D2 is greater than the dimension of the first display module 21 along the second direction D2. During the later maintenance process, the second hollow hole LK2 serves as a maintenance hole, and through the second hollow hole LK2, the first display module 21 can be conveniently taken and placed.

[0124] According to some exemplary embodiments, in combination with reference to Figure 1 , Figure 5 and Figure 7, the main housing 10 includes a fourth side surface 14. Along the third direction D3, the fourth side surface 14 is located on the side close to the windshield WS. At least two third hollow holes LK3 are provided on the fourth side surface 14, and the at least two third hollow holes LK3 are spaced along the second direction D2. Considering the heat dissipation requirement of the first display module 21, the third hollow holes LK3 are provided on the side of the main housing 10 close to the windshield WS as heat dissipation holes. The two third hollow holes LK3 are spaced along the second direction D2 to avoid affecting the strength of the main housing 10.

[0125] Figure 19 Schematically shows a structural diagram of a back plate of a first display module of a cockpit structure according to some embodiments of the present disclosure. Figure 20 Schematically shows a side view of a back plate of a first display module of a cockpit structure according to some embodiments of the present disclosure. Figure 21 Schematically shows Figure 20 An enlarged view of area B in Figure 22 Schematically shows an assembly diagram of a first display module of a cockpit structure according to some embodiments of the present disclosure. Figure 23 Schematically shows Figure 22 An enlarged view of area C in

[0126] According to some exemplary embodiments, the first display module serves as a projection light source for a head-up display, and there is a relatively high demand for its display brightness. For example, the maximum brightness can be as high as 7000 nit. High-brightness display will cause more heat generation. In order to avoid defects caused by excessive temperature during use, a structure that can improve the heat dissipation efficiency is provided on the back plate 2115 in the first display module.

[0127] With reference to Figure 19 , Figure 20 and Figure 21 , a plurality of fins 21151 are arranged at intervals on the back plate 2115, so as to increase the surface area on the side of the back plate away from the display panel, thereby improving the heat dissipation efficiency.

[0128] According to some exemplary embodiments, with reference to Figure 21 , the plurality of fins 21151 are evenly arranged, and the shape of the fins 21151 can be a cylindrical shape with a hemispherical top. The thickness of the fins 21151 in the direction perpendicular to the back plate 2115 is T1, the thickness of the part of the back plate 2115 where the fins 21151 are not provided is T2, the width of the fins 21151 is D1, and the distance between adjacent fins 21151 is D2. In order to achieve better heat dissipation efficiency, T1, T2, D1, and D2 can be set as shown in Table 1 below.

[0129] Table 1

[0130] T2 (mm) 2-4 4-6 6-8 8-10 10 or more D1 (mm) 1.5 2 2.5 3 4 T1 (mm) ≥6 ≥8 ≥8 ≥10 ≥10 D2 (mm) ≥3 ≥5 ≥5 ≥8 ≥8

[0131] According to some exemplary embodiments, with reference to Figure 19 , a plurality of fins 21151 are arranged in the area where the circuit board 2116 is not provided, and the area where the circuit board 2116 is provided does not have the fin 21151.

[0132] According to some exemplary embodiments, in combination with reference to Figure 22 and Figure 23 , for the convenience of the rapid assembly of the first display module 21 and to improve the production line work efficiency, the front frame 211 and the back plate 2115 are connected by buckles. Compared with the traditional screw fixing design, the assembly efficiency can be increased by 70%, and the snap fixing method can improve the aesthetics of the first display module 21 compared with the fixing method of exposed screws. For example, buckles can be provided on one side of the back plate 2115, and a processing notch matching the buckles can be provided on one side of the front frame 211.

[0133] According to some exemplary embodiments, in combination with reference to Figure 1 and Figure 5 , the cockpit structure further includes two side plates 51. The two side plates 51 are respectively connected to both sides of the main housing 10 along the second direction D2, and the side plates 51 extend in a direction away from the windshield WS. The two side plates 51 are respectively flush with the two side surfaces of the main housing 10 along the second direction D2. The side plates 51 are provided with a fourth hollow hole LK4 and a fifth hollow hole LK5. The fourth hollow hole LK4 and the fifth hollow hole LK5 can be arranged at intervals along the first direction D1. The hollow area of the fourth hollow hole LK4 can be larger than the hollow area of the fifth hollow hole LK5. The second display module is arranged at the fourth hollow hole LK4, and a control board electrically connected to the second display module is arranged at the fifth hollow hole LK5. See the following description for details.

[0134] Figure 24 Schematically shows an exploded view of a first cover assembly of a cockpit structure according to some embodiments of the present disclosure. Figure 25 Schematically shows a structural diagram of a first cover assembly of a cockpit structure according to some embodiments of the present disclosure. Figures 26 - 27 Schematically shows an assembly schematic diagram of a first cover assembly of a cockpit structure and a main housing according to some embodiments of the present disclosure. Figure 28 Schematically shows an assembly schematic diagram of a first cover and a first decorative plate of a cockpit structure according to some embodiments of the present disclosure. Figure 29 Schematically shows a structural diagram of a light bar assembly of a cockpit structure according to some embodiments of the present disclosure. Figure 30 Schematically shows along Figure 29 A cross-sectional view taken along the direction DD' in

[0135] According to some exemplary embodiments, in combination with reference to Figure 1, Figure 26 and Figure 27 , the cockpit structure includes a first cover assembly 60. The first cover assembly 60 is disposed on a side of the main housing 10 away from the windshield WS. The first cover assembly 60 bends away from the windshield WS on both sides in the second direction D2 and covers two side plates 51. Two sixth hollow holes LK6 are respectively disposed on both sides of the first cover assembly 60 along the second direction D2, and a part of two fourth hollow holes LK4 disposed on the two side plates 51 are respectively exposed through the two sixth hollow holes LK6.

[0136] According to some exemplary embodiments, with reference to Figure 1 , Figure 24 , Figure 25 , Figure 26 and Figure 28 , the first cover assembly 60 includes a first cover 61, a first decorative plate 63, a second cover 62, a second decorative plate 64 and a light bar assembly 65. The first decorative plate 63 is disposed on a side of the first cover 61 away from the main housing 10, and the second decorative plate 64 is disposed on a side of the second cover 62 away from the main housing 10. The first cover 61 and the second cover 62 are connected along the first direction D1, and the light bar assembly 65 is disposed between the first cover 61 and the second cover 62. The first cover 61 is disposed on a side closer to the windshield WS, and the first cover 61 is connected to one side of the first side surface 11 of the main housing 10. The second cover 62 is disposed on a side farther from the windshield WS, and the second cover 62 is connected to one side of the second side surface 12 of the main housing 10.

[0137] It should be noted that, in order to more clearly show the structures of the first cover 61 and the second cover 62, the first decorative plate 63 and the second decorative plate 64 are omitted in Figure 24 , and the first decorative plate 63 is omitted in Figures 25 - 27 .

[0138] According to some exemplary embodiments, with reference to Figure 26 and Figure 27 , one sixth hollow hole LK6 is respectively disposed on both sides of the first cover 61 along the second direction D2.

[0139] According to some exemplary embodiments, with reference to Figure 26 , a seventh hollow hole LK7 is further disposed on the first cover 61. The seventh hollow hole LK7 is located between the two sixth hollow holes LK6. The maximum dimension of the seventh hollow hole LK7 along the second direction D2 is greater than the dimension of the module mounting hole 111 along the second direction D2, that is, the maximum dimension of the seventh hollow hole LK7 along the second direction D2 is greater than the dimension of the first display module 21 along the second direction D2. The seventh hollow hole LK7 disposed on the first cover 61 and the second hollow hole LK2 disposed on the main housing 10 together serve as a maintenance hole for the first display module 21.

[0140] According to some exemplary embodiments, with reference to Figure 29 and Figure 30 , the light bar assembly 65 includes an LED light board 651, RGB light beads 652, a light homogenizing plate 653, and a light guide bar 654. The LED light board 651 can be made of aluminum, and the RGB light beads 652 can adjust different colors and brightness according to requirements. The light homogenizing plate 653 is made of transparent PC or PMMA material. In order to place the light leakage points of the light guide bar, the light homogenizing plate 653 needs to have a matte texture. The light guide bar 654 is processed from transparent plastic material and can be made of materials such as PC or PMMA. The light bar assembly 65 can be used as an in-vehicle atmosphere light to create a comfortable and warm environment for drivers and passengers, reduce driving fatigue, improve the riding experience, and enhance the in-vehicle comfort.

[0141] According to some exemplary embodiments, with reference to Figure 24 , the first cover plate 61, the light bar assembly 65, and the second cover plate 62 are connected together by 8 screws S06 using a sandwich structure.

[0142] According to some exemplary embodiments, with reference to Figure 26 and Figure 27 , the assembled first cover plate assembly 60 and the main housing 10 are fixedly connected by internal hidden screws to ensure that each screw is not exposed and achieve a hidden connection.

[0143] Figure 31 Schematically shows a structural diagram of the A-pillar support of the cockpit structure according to some embodiments of the present disclosure. Figure 32 Schematically shows an assembly diagram of the A-pillar support and the main housing of the cockpit structure according to some embodiments of the present disclosure. Figure 33 Schematically shows a structural diagram of the combination of the A-pillar support and the main housing of the cockpit structure according to some embodiments of the present disclosure.

[0144] According to some exemplary embodiments, with reference to Figure 3 , Figure 31 , Figure 32 and Figure 33 , the cockpit structure further includes an A-pillar support 52. The A-pillar support 52 includes two support portions 521 located on both sides of the second direction D2 and a connecting portion 522 connected between the two support portions 521. The support portions 521 are triangular and have a triangular hollow structure inside to increase the aesthetics. The A-pillar support 52 is fixed to the first side surface 11 of the main housing 10 by screws. The inclination degree of the surface of the A-pillar support 52 close to the windshield WS side matches the inclination degree of the windshield WS, and is used to provide support for the windshield WS.

[0145] Figure 34Schematically shows an assembly diagram of an air outlet frame and a front shell of a cockpit structure according to some embodiments of the present disclosure. Among them, Figure 34 Schematically shows the assembly diagram viewed from the upper side. Figure 35 Schematically shows an assembly diagram of an air outlet frame and a main housing of a cockpit structure according to some embodiments of the present disclosure. Among them, Figure 35 Schematically shows the assembly diagram viewed from the upper side.

[0146] According to some exemplary embodiments, with reference to Figure 34 and Figure 35 , the cockpit structure further includes a front shell 53 and an air outlet frame 54. A ninth hollow hole LK9 is provided in the front shell 53, and a tenth hollow hole LK10 is provided in the air outlet frame 54. The four sides of the air outlet frame 54 are respectively fixed around the ninth hollow hole LK9 of the front shell 53 by screws, and all the fixing screws are not exposed. Both the ninth hollow hole LK9 and the tenth hollow hole LK10 are strip-shaped hollow holes extending along the second direction D2, and the ninth hollow hole LK9 and the tenth hollow hole LK10 are communicated with each other to serve as a heat dissipation channel for the internal electronic components of the main housing 10.

[0147] According to some exemplary embodiments, with reference to Figure 34 and Figure 35 , after the air outlet frame 54 and the front shell 53 are assembled together, they are then fixed to the main housing 10 by screws. The ninth hollow hole LK9 and the tenth hollow hole LK10 are communicated with at least two third hollow holes LK3.

[0148] Figure 36 Schematically shows an assembly diagram of an A-pillar decorative frame and an A-pillar support member of a cockpit structure according to some embodiments of the present disclosure. Figure 37 Schematically shows Figure 36 An enlarged view of the area E in Figure 38 Schematically shows a cross-sectional view taken along the Figure 37 Direction FF' in

[0149] According to some exemplary embodiments, with reference to Figure 3 , Figure 36 , Figure 37 and Figure 38 , in the A-pillar support member 52, A-pillar decorative frames 55 are respectively provided on the outer sides of the two support portions 521 along the second direction D2. The A-pillar decorative frame 55 is triangular and annular. A fixing groove 5211 is provided on the side surface of the support portion 521 close to the windshield WS. The A-pillar decorative frame 55 is provided with a fixing convex block 551 that cooperates with the fixing groove 5211. The fixing convex block 551 is installed in the fixing groove 5211, and the cooperation method is interference fit, and the fixing convex block 551 is fixed in the fixing groove 5211 by a screw S07.

[0150] According to some exemplary embodiments, with reference to Figure 37 , a first positioning post 552 is further provided inside the A-pillar trim frame 55 near the support portion 521, and a first positioning groove 5212 that cooperates with the first positioning post 552 is further provided on the support portion 521. When the A-pillar trim frame 55 is installed on the support portion 521, the first positioning post 552 and the first positioning groove 5212 play an auxiliary positioning role.

[0151] In the cockpit structure of the embodiments of the present disclosure, the first display module 21 with a larger size in the second direction D2 is ingeniously designed and arranged through the structure, and the first display module 21 is hidden inside the operation console and used as a light source to project onto the windshield, presenting a super-large display effect that covers the entire area from A-pillar to A-pillar, so that information such as instruments, navigation, and multimedia entertainment can be simultaneously displayed on the windshield. Through the structural design, the first display module 21 can be firmly fixed on the main housing 10, effectively avoiding the problem that the first display module 21 loosens or deforms during long-term use, which affects the display effect.

[0152] Figure 39 Schematically shows an assembly schematic diagram of the second display module, the control board and the side plate of the cockpit structure according to some embodiments of the present disclosure. Figure 40 Schematically shows Figure 39 An enlarged view of region G in Figure 41 Schematically shows a combined structure diagram of the second display module, the control board and the side plate of the cockpit structure according to some embodiments of the present disclosure. Figure 42 Schematically shows Figure 41 An enlarged view of region H in

[0153] According to some exemplary embodiments, with reference to Figure 39 , Figure 40 , Figure 41 and Figure 42 , the second display module 22 is connected to the side of the side plate 51 away from the first cover assembly 60, and the second display module 22 is fixed at the fourth hollow hole LK4 of the side plate 51 by a half snap + half press block locking method. Snap fasteners 511 are provided on the outer sides of two adjacent sides of the fourth hollow hole LK4. The edge of the second display module 22 slides into the two snap fasteners 511, and then the edge of the second display module 22 is pressed by two press blocks 512 and fixed to the side plate 51 by screws S13. One press block 512 is located on the other side of one snap fastener 511 along the first direction D1, and the other press block 512 is located on the other side of the other snap fastener 511 along the third direction D3. The fourth hollow hole LK4 of the side plate 51 and the sixth hollow hole LK6 of the first cover assembly 60 expose the display surface of the second display module 22.

[0154] Two second display modules 22 located on both sides of the second direction D2 can be used as electronic rearview mirrors when driving, realizing a blind - spot - free electronic display inside the vehicle, thereby improving driving safety. According to some exemplary embodiments, with reference to Figure 39 , Figure 40 , Figure 41 and Figure 42 , the cockpit structure further includes two control boards 58. The two control boards 58 are respectively arranged adjacent to the two second display modules 22, and the control board 58 is electrically connected to the adjacent second display module 22 through a flexible cable, and can control the second display module 22 to display in linkage with the first display module. The control board 58 is connected to the side of the side plate 51 away from the first cover assembly 60, and the control board is fixed to the fifth hollow hole LK5 of the side plate 51 through a screw S14. The fifth hollow hole LK5 can be used as an access hole for the control board 58.

[0155] Figure 43 Schematically shows an exploded view of the second display module of the cockpit structure according to some embodiments of the present disclosure. Figure 44 Schematically shows a physical diagram of the second display module of the cockpit structure according to some embodiments of the present disclosure.

[0156] According to some exemplary embodiments, with reference to Figure 43 and Figure 44 , a touch - sensitive glass 224 and a touch - sensitive decorative film 225 are further arranged on one side of the light - emitting surface of the second display module 22. The texture of the touch - sensitive decorative film 225 of the second display module 22 and the decorative film on the surface of the first cover assembly 60 can be kept consistent, for example, both are wood grain, so that when the second display module 22 is turned off, it presents an integrated hidden effect with the first cover assembly 60, which can effectively improve the interference of the reflection of the second display module 22 to the driver. Figure 45 Schematically shows an internal structure diagram of the main housing of the cockpit structure according to some embodiments of the present disclosure.

[0157] According to some exemplary embodiments, with reference to Figure 2 and Figure 45 , some electronic components are arranged in the accommodation space 10a of the main housing 10, such as including a first fan 81, a second fan 82 and a third fan 83. The first fan 81 and the second fan 82 are intake fans, and the third fan 83 is an exhaust fan. The first fan 81 and the second fan 82 are respectively located on both sides of the third fan 83 along the second direction D2, so that the air enters from both sides and exits from the middle, realizing a two - way circulation heat dissipation effect. The circulation direction can refer to the direction indicated by the arrow in Figure 2 .

[0158] Figure 46 Schematically shows an assembly diagram of the steering wheel grip of the cockpit structure according to some embodiments of the present disclosure.Figure 47 Schematically shows a structural diagram of a steering wheel grip of a cockpit structure according to some embodiments of the present disclosure. Figure 48 Schematically shows along Figure 47 A cross-sectional view taken along the middle direction JJ'. According to some exemplary embodiments, with reference to Figure 46 , Figure 47 and Figure 48 , the cockpit structure further includes a steering wheel 90, and the steering wheel 90 includes a steering wheel grip 91. The steering wheel grip 91 can be an octagonal structure, including a left grip 911 and a right grip 912. The left grip 911 and the right grip 912 can use plastic PC or ABS material as the base material, and the surface is covered with two-tone spliced organic leather 915. Avoidance grooves 91a are provided on both the left grip 911 and the right grip 912, and the edge of the leather 915 is hidden in the avoidance grooves 91a so that the leather 915 can be smoothly covered.

[0159] In Figure 48 , m represents the width of the avoidance groove, n represents the depth of the avoidance groove, and m and n will be adjusted according to different thicknesses of the leather. Generally, it is necessary to satisfy 2 ≤ m ≤ 5 mm and 1 ≤ n ≤ 2 mm.

[0160] After wrapping the leather, the left grip 911 and the right grip 912 are simultaneously inserted into the first connector 913 and the second connector 914, and the left grip 911 and the right grip 912 are fixed to the first connector 913 by screws S18, and the left grip 911 and the right grip 912 are fixed to the second connector 914 by screws S19.

[0161] An embodiment of the present application further provides a vehicle, which may include a vehicle body and a cockpit structure as provided in the above embodiments located inside the vehicle body.

[0162] As used herein, the terms "substantially", "about", "approximately" and other similar terms are used as approximate terms rather than terms of degree, and they are intended to explain the inherent deviations of measured or calculated values that will be recognized by those of ordinary skill in the art. Considering factors such as process fluctuations, measurement problems, and errors related to the measurement of a specific quantity (i.e., limitations of the measurement system), "about" or "approximately" as used herein includes the stated value and represents within an acceptable deviation range for a specific value determined by those of ordinary skill in the art. For example, "about" may mean within one or more standard deviations, or within ±10% or ±5% of the stated value.

[0163] Although some embodiments according to the general inventive concept of the present disclosure have been illustrated and described, those of ordinary skill in the art will understand that changes can be made to these embodiments without departing from the principles and spirit of the general inventive concept of the present disclosure, and the scope of the present disclosure is defined by the claims and their equivalents.

Claims

1. A cockpit structure, wherein: The cockpit structure comprises: A main housing, the main housing comprising a first side surface located on one side in a first direction, the first side surface being provided with a module mounting hole; A first display module is arranged on the main housing, wherein a display surface of the first display module is exposed outside the main housing through the module mounting hole, a ratio of a long side dimension to a short side dimension of the display surface is greater than or equal to 4, and a long side of the display surface extends along a second direction, and the second direction intersects the first direction; a bracket, wherein the first display module is connected to the main housing through the bracket; and A windshield is located at one side of the main shell along a third direction, and the third direction intersects both the first direction and the second direction.

2. The cockpit structure according to claim 1, wherein: The main housing includes a second side surface, and the second side surface and the first side surface are respectively located on two sides of the first direction; and The display surface of the first display module is inclined relative to a horizontal plane, and a side of the first display module close to the windshield is closer to the second side surface than a side of the first display module far from the windshield.

3. The cockpit structure according to claim 2, wherein: The main shell includes a storage space, the module mounting hole is provided with a skirt structure, the skirt structure at least partially surrounds the module mounting hole and protrudes toward the storage space of the main shell, and the protruding distance of the skirt structure close to the windshield is smaller than the protruding distance of the skirt structure away from the windshield; and The first display module is connected to the skirt structure through the bracket.

4. The cockpit structure according to claim 3, wherein: The bracket is annular and connected to the edge of the first display module. The bracket includes fixing parts protruding from both sides of the first display module along the third direction, and the fixing parts are connected to the skirt structure.

5. The cockpit structure according to claim 4, wherein: The fixing portion along the third direction away from the windshield side includes a plurality of fixing sub-portions arranged at intervals, an abutting portion is arranged between adjacent fixing sub-portions, the abutting portion is arranged vertically with the fixing sub-portions, and the abutting portion is fixedly connected to the side of the second display module away from the windshield side.

6. The cockpit structure according to any one of claims 2 to 5, wherein: The cabin structure further comprises at least one support member, and at least one of the support members is located in the accommodation space; and One side of the support member is connected to a side of the first display module that is away from the display surface, and one side of the support member is connected to the second side surface of the main housing.

7. The cockpit structure according to claim 6, wherein: The support member includes a first support member and a second support member connected along the first direction; The first support member comprises a first strip member and a second strip member, the first strip member and the second strip member are vertically connected, an extension direction of the first strip member is parallel to a horizontal plane, an end of the first strip member away from the second strip member is connected to a side of the first display module away from the windshield, and an end of the second strip member away from the first strip member is connected to a side of the first display module close to the windshield; and The second supporting member includes a third strip member, a fourth strip member and a fifth strip member, the third strip member and the fifth strip member are arranged at intervals along the first direction, the fourth strip member is connected between the third strip member and the fifth strip member, the third strip member is connected to a side of the first strip member away from the first display module, and the fifth strip member is connected to the second side surface.

8. The cockpit structure according to claim 7, wherein: One end of the fourth strip is connected to an end of the third strip away from the windshield, and the other end of the fourth strip is connected to an end of the fifth strip away from the windshield.

9. The cockpit structure according to claim 7 or 8, wherein: The second side surface is provided with a first hollow hole, the cockpit structure further comprises a metal bottom plate, the metal bottom plate is provided on the second side surface and covers the first hollow hole, and the second support member is connected to the metal bottom plate at a side away from the first display module.

10. The cockpit structure according to any one of claims 6 to 9, wherein: The cabin structure comprises at least two supporting members, and the at least two supporting members are spaced apart along the second direction; and The cockpit structure further includes at least one reinforcing plate, which is located between at least two of the supporting members and is connected to a side of the first display module that is away from the display surface.

11. The cockpit structure according to claim 10, wherein: A dimension of the reinforcing plate along the second direction is greater than a dimension of the supporting member along the second direction.

12. The cockpit structure according to any one of claims 1 to 11, wherein: The main shell includes a third side surface, which is located on a side away from the windshield along the third direction. A second hollow hole is provided on the third side surface, and a size of the second hollow hole along the second direction is larger than a size of the module mounting hole along the second direction.

13. The cockpit structure according to any one of claims 1 to 11, wherein: The main shell includes a fourth side surface, the fourth side surface is located on a side close to the windshield along the third direction, at least two third hollow holes are arranged on the fourth side surface, and at least two of the third hollow holes are spaced apart along the second direction.

14. The cockpit structure according to any one of claims 2 to 13, wherein: The angle between the display surface of the first display module and the horizontal plane is less than or equal to 10°; and / or, The angle between the windshield and the horizontal plane is greater than or equal to 30° and less than or equal to 45°.

15. The cockpit structure according to any one of claims 1 to 14, wherein: The cockpit structure further includes two side panels, which are respectively connected to two sides of the main shell along the second direction, and the side panels are extended in a direction away from the windshield; The cockpit structure further includes two second display modules, which are respectively arranged on the two side panels, and the second display modules are arranged on a side of one side panel away from the other side panel; and The side plate is provided with a fourth hollow hole, and the fourth hollow hole exposes the display surface of the second display module.

16. The cockpit structure according to claim 15, wherein: The cockpit structure also includes a control panel, which is arranged on the side panel and is electrically connected to the second display module.

17. The cabin structure according to claim 15 or 16, wherein: The side plate is provided with a fifth hollow hole, and the fifth hollow hole exposes at least a portion of the control plate.

18. The cockpit structure according to any one of claims 15 to 17, wherein: The cockpit structure comprises a first cover plate assembly, the first cover plate assembly is arranged on a side of the main shell away from the windshield, the first cover plate assembly is located on both sides of the second direction and is bent in a direction away from the windshield and covers the two side panels; and A sixth hollow hole is disposed on the first cover plate assembly, and the sixth hollow hole exposes the display surface of the second display module.

19. The cockpit structure according to claim 18, wherein: The first cover plate assembly includes a first cover plate, a second cover plate and a light bar assembly, the first cover plate and the second cover plate are connected along a first direction, and the light bar assembly is arranged between the first cover plate and the second cover plate.

20. The cockpit structure according to claim 19, wherein: The first cover plate is connected to one side of the first side surface of the main shell, and the first cover plate is provided with a seventh hollow hole, and the size of the seventh hollow hole along the second direction is larger than the size of the module installation hole along the second direction.

21. A vehicle, wherein: The vehicle comprises a cabin structure according to any one of claims 1-20.

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