Cabin structure and vehicle

Abstract

The utility model provides a cabin structure, and the cabin structure comprises a main housing, the main housing comprises a first side surface located at one side of a first direction, and the first side surface is provided with a module installation hole; 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] This disclosure relates to the field of display technology, and more particularly to a cockpit structure and vehicle. Background Technology

[0002] A head-up display (HUD) projects current driving information, such as speed, RPM, range, tire pressure, navigation, and multimedia information, onto a screen a certain distance ahead through the windshield. Drivers no longer need to look down at the traditional dashboard or infotainment system; they can access driving information directly from the projected image. This allows drivers to keep their attention on the road ahead, significantly improving driving safety and preventing accidents caused by looking down at the instruments. One key challenge for display product developers is how to structurally and securely mount the HUD display within the cockpit.

[0003] The information disclosed in this section is only for understanding the background of the inventive concept of this utility model. Therefore, the above information may include information that does not constitute prior art. Utility Model Content

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

[0005] The main housing includes a first side located in a first direction, and the first side is provided with a module mounting hole;

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

[0007] The bracket, wherein the first display module is connected to the main housing via the bracket; and

[0008] The windshield is located on one side of the main housing along a third direction, which intersects both the first and second directions.

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

[0010] The display surface of the first display module is inclined relative to the horizontal plane, and the side of the first display module closer to the windshield is closer to the second side than the side of the first display module farther from the windshield.

[0011] According to some exemplary embodiments, the main housing includes a receiving space, and 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. The protrusion distance of the skirt structure near the windshield is smaller than the protrusion distance of the skirt structure away from the windshield; and

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

[0013] According to some exemplary embodiments, the bracket is ring-shaped and connected to the edge of the first display module. The bracket includes fixing portions protruding from both 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 along the third direction away from the windshield includes a plurality of fixing sub-parts spaced apart, and an abutting portion is provided between adjacent fixing sub-parts. The abutting portion is perpendicular to the fixing sub-parts and is fixedly connected to the side of the second display module away from the windshield.

[0015] According to some exemplary embodiments, the cockpit structure further includes at least one support member, at least one of said support members being located within the accommodating space; and

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

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

[0018] The first support member comprises a first strip and a second strip, which are vertically connected. The first strip extends parallel to a horizontal plane. The end of the first strip away from the second strip is connected to the side of the first display module away from the windshield. The end of the second strip away from the first strip is connected to the side of the first display module closer to the windshield.

[0019] The second support member includes a third strip, a fourth strip, and a fifth strip. The third strip and the fifth strip are spaced apart along the first direction. The fourth strip is connected between the third strip and the fifth strip. The third strip is connected to the side of the first strip away from the first display module. The fifth strip is connected to the second side.

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

[0021] According to some exemplary embodiments, a first perforation is provided on the second side, and the cockpit structure further includes a metal base plate, which is disposed on the second side and covers the first perforation. The side of the second support member away from the first display module is connected to the metal base plate.

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

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

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

[0025] According to some exemplary embodiments, the main housing includes a third side surface located on the side away from the windshield along the third direction. A second perforation is provided on the third side surface, and the size of the second perforation along the second direction is larger 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 located near the windshield along the third direction. The fourth side surface is provided with at least two third perforations, which are spaced apart along the second direction.

[0027] According to some exemplary embodiments, the 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 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 panels, which are respectively connected to both sides of the main housing along the second direction, and the side panels are arranged to extend away from the windshield.

[0030] The cockpit structure also includes two second display modules, which are respectively disposed on the two side panels, with each second display module located on the side of one side panel away from the other side panel; and

[0031] The side panel is provided with a fourth cutout hole, which exposes the display surface of the second display module.

[0032] According to some exemplary embodiments, the cockpit structure further includes a control panel disposed on the side panel, the control panel being electrically connected to the second display module.

[0033] According to some exemplary embodiments, the side panel is provided with a fifth cutout hole, which exposes at least a portion of the control panel.

[0034] According to some exemplary embodiments, the cockpit structure includes a first cover assembly disposed on the side of the main housing away from the windshield, the first cover assembly being bent on both sides in the second direction away from the windshield and covering the two side panels; and

[0035] The first cover plate assembly is provided with a sixth cutout hole, which 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 strip assembly, wherein the first cover plate and the second cover plate are connected along a first direction, and the light strip assembly is disposed 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 of the main housing, and the first cover plate is provided with a seventh hollow hole, the size of the seventh hollow hole along the second direction being larger than the size of the first display module along the second direction.

[0038] In another aspect, a vehicle is provided, wherein the vehicle includes a cockpit structure as described in any of the preceding claims. Attached Figure Description

[0039] Other objects and advantages of the present invention will become apparent from the following description of the invention with reference to the accompanying drawings, and will help to provide a comprehensive understanding of the invention.

[0040] Figure 1 The diagram schematically illustrates a perspective view of a cockpit structure according to some embodiments of the present invention from one viewpoint.

[0041] Figure 2 A rear view of a cockpit structure according to some embodiments of the present invention is shown schematically.

[0042] Figure 3 A schematic left view of a cockpit structure according to some embodiments of the present invention is shown.

[0043] Figure 4 The schematic diagram illustrates the display principle of a first display module of a cockpit structure according to some embodiments of the present invention.

[0044] Figure 5 The diagram schematically illustrates the structure of the main housing of the cockpit structure according to some embodiments of the present invention.

[0045] Figure 6 The diagram illustrates the assembly of the main housing and the first display module of the cockpit structure according to some embodiments of the present invention.

[0046] Figure 7 The diagram schematically illustrates the combined structure of the main housing and the first display module of the cockpit structure according to some embodiments of the present invention.

[0047] Figure 8 The diagram illustrates the assembly of a first display module and a bracket in a cockpit structure according to some embodiments of the present invention.

[0048] Figure 9 The diagram schematically illustrates the combined structure of a first display module and a bracket in a cockpit structure according to some embodiments of the present invention.

[0049] Figure 10 The illustration schematically shows a side view of a combination of a first display module and a first support member in a cockpit structure according to some embodiments of the present invention.

[0050] Figure 11 The diagram schematically illustrates the combined structure of a first display module, a first support member, and a reinforcing plate in a cockpit structure according to some embodiments of the present invention.

[0051] Figure 12 The diagram schematically illustrates the combined structure of a first display module, a first support member, a reinforcing plate, and an FPGA board in a cockpit structure according to some embodiments of the present invention.

[0052] Figure 13 An exploded view of a metal floor plate of a cockpit structure according to some embodiments of the present invention is shown schematically.

[0053] Figure 14 The diagram schematically illustrates the structure of the metal floor plate of the cockpit structure according to some embodiments of the present invention.

[0054] Figure 15This schematically illustrates another exploded view of the metal floor plate of the cockpit structure according to some embodiments of the present invention.

[0055] Figures 16-18 The diagram illustrates the assembly of the metal floor plate and main shell of the cockpit structure according to some embodiments of the present invention.

[0056] Figure 19 The diagram schematically illustrates the structure of the rear panel of the first display module of the cockpit structure according to some embodiments of the present invention.

[0057] Figure 20 The diagram schematically shows a side view of the rear panel of a first display module of a cockpit structure according to some embodiments of the present invention.

[0058] Figure 21 Schematic illustration Figure 20 A magnified view of region B in the middle.

[0059] Figure 22 An assembly diagram of a first display module of a cockpit structure according to some embodiments of the present invention is shown schematically.

[0060] Figure 23 Schematic illustration Figure 22 A magnified view of region C in the middle.

[0061] Figure 24 An exploded view of a first cover assembly of a cockpit structure according to some embodiments of the present invention is shown schematically.

[0062] Figure 25 The diagram schematically illustrates the structure of a first cover assembly of a cockpit structure according to some embodiments of the present invention.

[0063] Figures 26-27 The diagram illustrates the assembly of the first cover plate assembly with the main housing of a cockpit structure according to some embodiments of the present invention.

[0064] Figure 28 The diagram illustrates the assembly of a first cover plate and a first decorative plate of a cockpit structure according to some embodiments of the present invention.

[0065] Figure 29 The diagram schematically illustrates a light bar assembly structure of a cockpit structure according to some embodiments of the present invention.

[0066] Figure 30 Schematic illustration along Figure 29 A sectional view taken from the center direction DD'.

[0067] Figure 31The diagram schematically illustrates the structure of the A-pillar support member of the cockpit structure according to some embodiments of the present invention.

[0068] Figure 32 The diagram illustrates the assembly of the A-pillar support member and the main shell of the cockpit structure according to some embodiments of the present invention.

[0069] Figure 33 The diagram schematically illustrates the structural composition of the A-pillar support and the main shell of the cockpit structure according to some embodiments of the present invention.

[0070] Figure 34 The diagram illustrates the assembly of the air vent frame and the front shell of the cockpit structure according to some embodiments of the present invention.

[0071] Figure 35 The diagram illustrates the assembly of the air vent frame and the main housing of the cockpit structure according to some embodiments of the present invention.

[0072] Figure 36 The diagram illustrates the assembly of the A-pillar decorative frame and A-pillar support member of a cockpit structure according to some embodiments of the present invention.

[0073] Figure 37 Schematic illustration Figure 36 A magnified view of region E in the middle.

[0074] Figure 38 Schematic illustration along Figure 37 A sectional view taken from the center direction FF'.

[0075] Figure 39 The diagram illustrates the assembly of the second display module and control panel with the side panel of the cockpit structure according to some embodiments of the present invention.

[0076] Figure 40 Schematic illustration Figure 39 A magnified view of region G in the middle.

[0077] Figure 41 The diagram schematically illustrates the combined structure of the second display module and control panel with the side panel of the cockpit structure according to some embodiments of the present invention.

[0078] Figure 42 Schematic illustration Figure 41 A magnified view of region H in the middle.

[0079] Figure 43 An exploded view of a second display module of a cockpit structure according to some embodiments of the present invention is shown schematically.

[0080] Figure 44The illustration shows a physical diagram of a second display module of a cockpit structure according to some embodiments of the present invention.

[0081] Figure 45 The diagram schematically illustrates the internal structure of the main housing of the cockpit structure according to some embodiments of the present invention.

[0082] Figure 46 The diagram illustrates an assembly schematic of a steering wheel grip in a cockpit structure according to some embodiments of the present invention.

[0083] Figure 47 The diagram schematically illustrates the structure of the steering wheel grip of a cockpit structure according to some embodiments of the present invention.

[0084] Figure 48 Schematic illustration along Figure 47 A sectional view taken from the center of JJ'.

[0085] It should be noted that, for clarity, the dimensions of layers, structures, or regions in the drawings used to describe embodiments of the present invention may be enlarged or reduced, i.e., these drawings are not drawn to actual scale. Detailed Implementation

[0086] In the following description, numerous specific details are set forth for illustrative purposes to provide a comprehensive understanding of various exemplary embodiments. However, it will be apparent that various exemplary embodiments may be implemented without these specific details or with one or more equivalent arrangements. In other instances, well-known structures and apparatuses are shown in block diagram form to avoid unnecessarily obscuring the various exemplary embodiments. Furthermore, the various exemplary embodiments may be different, but not necessarily exclusive. For example, specific shapes, configurations, and characteristics of exemplary embodiments may be used or implemented in another exemplary embodiment without departing from the inventive concept.

[0087] In the accompanying drawings, the dimensions and relative dimensions of the elements may be enlarged for clarity and / or descriptive purposes. Thus, the dimensions and relative dimensions of the individual elements are not necessarily limited to those shown in the drawings. When exemplary embodiments can be implemented differently, the specific process sequence may be performed differently than the order described. For example, two consecutively described processes may be performed substantially simultaneously or in the reverse order of description. Furthermore, the same reference numerals denote the same elements.

[0088] When an element is described as being "on" another element, "connected to" another element, or "attached to" another element, the element may be directly on, directly connected to, or directly attached to the other element, or there may be intermediate elements present. However, when an element is described as being "directly on" another element, "directly connected to" another element, or "directly attached to" another element, there are no intermediate elements. Other terms and / or expressions used to describe relationships between elements should be interpreted in a similar manner, such as "between" versus "directly between," "adjacent" versus "directly adjacent," or "on" versus "directly on," etc. Furthermore, the term "connection" can refer to a physical connection, an electrical connection, a communication connection, and / or a fluid connection. Additionally, the X-axis, Y-axis, and Z-axis are not limited to the three axes of a Cartesian coordinate system and can be interpreted in a broader sense. For example, the X-axis, Y-axis, and Z-axis may be perpendicular to each other, or may represent different directions that are not perpendicular to each other. For the purposes of this invention, "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 and all combinations of one or more of the listed related items.

[0089] 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 merely used to distinguish one element from another. For example, without departing from the scope of the exemplary embodiments, a first element may be named a second element, and similarly, a second element may be named a first element.

[0090] Figure 1 The diagram schematically illustrates a perspective view of a cockpit structure according to some embodiments of the present invention from one viewpoint. Figure 2 A rear view of a cockpit structure according to some embodiments of the present invention is shown schematically. Figure 3 A schematic left view of a cockpit structure according to some embodiments of the present invention is shown.

[0091] Figure 4 The schematic diagram illustrates the display principle of a first display module of a cockpit structure according to some embodiments of the present invention. Figure 5 The diagram schematically illustrates the structure of the main housing of the cockpit structure according to some embodiments of the present invention. Figure 6 The diagram illustrates the assembly of the main housing and the first display module of the cockpit structure according to some embodiments of the present invention. Figure 7The diagram schematically illustrates the combined structure of the main housing and the first display module of the cockpit structure according to some embodiments of the present invention. Specifically, 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 the diagram have been flipped up and down. The second side of the main housing located on the upper side should actually be located on the lower side, and the side of the first display module located on the upper side should actually be the lower side located on the back of the display surface.

[0092] Figure 8 The diagram illustrates the assembly of a first display module and a bracket in a cockpit structure according to some embodiments of the present invention. Figure 9 The diagram schematically illustrates the combined structure of a first display module and a bracket in a cockpit structure according to some embodiments of the present invention. Figure 10 The illustration schematically shows a side view of a combination of a first display module and a first support member in a cockpit structure according to some embodiments of the present invention. Figure 11 The diagram schematically illustrates the combined structure of a first display module, a first support member, and a reinforcing plate in a cockpit structure according to some embodiments of the present invention. Figure 12 The diagram schematically illustrates the combined structure of a first display module, a first support member, a reinforcing plate, and an FPGA board in a cockpit structure according to some embodiments of the present invention.

[0093] Combined with reference 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 located in a first direction D1, and the first side surface 11 has a module mounting hole 111. The first display module 21 is mounted on the main housing 10 at the module mounting hole 111 via the bracket 30. 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. The long side of the display surface extends along a second direction D2, which intersects with the first direction D1. The windshield WS is located on one side of the main housing 10 along a third direction D3, which intersects both the first direction D1 and the second direction D2.

[0094] It should be noted that when the driver is seated 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. Furthermore, when this cockpit structure is applied inside a vehicle, the main housing 10 is the main housing 10 of the center console, and the material of the main housing 10 may include at least one of ABS plastic and PC plastic; the windshield WS is the front windshield.

[0095] By concealing the first display module 21 within the main housing 10 and projecting it onto the windshield WS as the image source, and given that the ratio of the long side to the short side 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 large size along the second direction D2. This allows for a panoramic head-up display (PHUD) effect that fully covers the A-pillar from A-pillar to A-pillar. This enables the windshield WS to simultaneously display instrument information, navigation information, and multimedia entertainment information, avoiding the safety hazard caused by having to look down at the central control screen while driving. For example, instrument information can be displayed in front of the driver's seat, multimedia entertainment information can be displayed in front of the passenger's seat, and navigation information can be displayed between the instrument information and multimedia entertainment information.

[0096] According to some exemplary embodiments, in conjunction with reference to Figure 1 , Figure 4 and Figure 7 The main housing 10 includes a second side 12, which is located on both sides of the first side 11 in the first direction D1. The first side 11 is located closer to the windshield WS, and the second side 12 is located further away from the windshield WS. The display surface 21a of the first display module 21 is inclined relative to the horizontal plane. The side of the first display module 21 closer to the windshield WS is closer to the second side 12 than the side of the first display module 21 further away from the windshield WS. That is, the setting height of the side of the first display module 21 further away from the windshield WS is lower than the setting height of the side of the first display module 21 further away from the windshield WS. This satisfies the optical requirements for projecting the display image of the first display module 21 onto the windshield WS.

[0097] According to some exemplary embodiments, refer to Figure 4 According to the inventors' research, in order to ensure that the display image of the first display module 21 can be clearly projected onto the windshield WS, the setting angle and setting position of the first display module 21 and the windshield WS must meet the following requirements:

[0098] The 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 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 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°.

[0099] The distance between the display surface 21a of the first display module 21, near the windshield WS, and the windshield WS along the third direction D3 is L1. L1 must satisfy 10mm≤L1≤40mm. The smaller L1 is, the lower the image is positioned. The distance between the driver's eyeball and the windshield WS along the third direction D3 is L2. L2 must satisfy 600mm≤L2≤900mm and can be adjusted according to the driving habits of different people. The distance between the display surface of the first display module 21, near the windshield WS, and the driver's eyeball along the first direction D1 is L3. L3 must satisfy 200mm≤L3≤400mm.

[0100] According to some exemplary embodiments, refer to Figure 1 A baffle 17 is also provided on the first side 11 of the main housing 10. The baffle 17 is located on the side of the first display module 21 away from the windshield WS, and can be glued and fixed to the main housing 10. The baffle 17 is used to prevent the light emitted by the first display module 21 from affecting the driver's observation of the projected image on the windshield WS. In this way, when using the PHUD, the driver can only see the image data on the windshield WS and will not directly see the image of the first display module 21, thus minimizing the need for the driver to look down while driving, maximizing the driver's driving safety environment, and improving the user's driving experience.

[0101] According to some exemplary embodiments, in conjunction with reference to Figure 1 , Figure 5 , Figure 6 and Figure 7 The main housing 10 has a frame structure and includes a receiving 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 receiving space 10a of the main housing 10. The first display module 21 is connected to the skirt structure 15 via a bracket 30. The skirt structure 15 includes a first skirt 151 near the windshield WS and a second skirt 152 away from the windshield WS. The protrusion distance of the first skirt 151 is smaller than that of the second skirt 152. The skirt structure 15 also includes a third skirt 153 and a fourth skirt 154, which 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 protrusion distance of the third skirt 153 and the fourth skirt 154 gradually decreases. In this way, the first display module 21 can be tightly and securely fixed to the skirt structure 15 of the main housing 10 by the bracket 30, thereby effectively preventing deformation of the first display module 21, and allowing the display surface of the first display module 21 to be tilted in a predetermined direction.

[0102] According to some exemplary embodiments, in conjunction with reference to Figure 6 , Figure 8 and Figure 9 The bracket 30 is ring-shaped and connected to the edge of the first display module 21. The bracket 30 includes a fixing part 31 that protrudes from both sides of the first display module 21 along the third direction D3. The fixing part 31 is connected to the skirt structure 15.

[0103] According to some exemplary embodiments, in conjunction with reference to Figure 1 , Figure 8 and Figure 9 The fixing part 31 along the third direction D3, away from the windshield WS, includes multiple fixing sub-parts 311 spaced apart. An abutment part 32 is provided between adjacent fixing sub-parts 311. The abutment part 32 is perpendicular to the fixing sub-parts 311 and can be fixedly connected to the side of the second display module 22 away from the windshield WS by screws. The abutment part 32 is fixed and abuts against the side of the second display module 22 that is lower in height, effectively preventing the first display module 21 from loosening or sliding over 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 to the back of the second display module 22 by screws.

[0104] For example, the bracket 30 has four abutment parts 32 on the side away from the windshield WS, and the four abutment parts 32 are fixedly connected to the side of the second display module 22 away from the windshield WS by four screws S01. On the other three sides where the abutment parts 32 are not provided, the bracket 30 is fixedly connected to the side of the second display module 21 opposite to its display surface by 12 screws S02.

[0105] According to some exemplary embodiments, in conjunction with reference to Figure 6 , Figure 7 and Figure 9 The second skirt 152 is provided with a plurality of notches 1521 spaced apart, and the plurality of notches 1521 are provided with a plurality of abutment portions 32. The notches 1521 are avoidance structures provided with the abutment portions 32 respectively.

[0106] According to some exemplary embodiments, refer to Figure 6 Before installing the first display module 21 to the main housing 10, a single-sided foam 18 is attached to the contact surface where the main housing 10 and the first display module 21 come into contact. The single-sided foam 18 serves to buffer and dampen shocks, preventing damage caused by hard contact between the main housing 10 and the first display module 21 during assembly.

[0107] Figure 13 An exploded view of a metal floor plate of a cockpit structure according to some embodiments of the present invention is shown schematically. Figure 14 The diagram schematically illustrates the structure of the metal floor plate of the cockpit structure according to some embodiments of the present invention. Figure 15 This schematically illustrates another exploded view of the metal floor plate of the cockpit structure according to some embodiments of the present invention. Figures 16-18 The diagram illustrates the assembly of the metal floor plate and main shell of a cockpit structure according to some embodiments of the present invention. The assembly process of the metal floor plate and main shell is shown in the diagram for clarity. Figure 17 The main casing shown in the diagram has been flipped upside down, and the second side located on the upper side of the main casing should actually be located on the lower side.

[0108] According to some exemplary embodiments, in conjunction with reference to Figure 16 , Figure 17 and Figure 18 A first perforated hole LK1 is provided on the second side 12 of the main housing 10. The dimension of the first perforated hole LK1 along the second direction D2 is larger than the dimension of the module mounting hole 111 along the second direction D2. The cockpit structure also includes a metal base plate 16, which is disposed on the second side 12 and covers the first perforated hole LK1. By providing the metal base plate 16, the strength of the main housing 10 can be improved, and the heat dissipation efficiency of the relevant electronic components installed inside the main housing 10 can be improved. For example, the material of the metal base plate 16 may include aluminum.

[0109] According to some exemplary embodiments, in conjunction with reference to Figure 16 and Figure 17 The metal base plate 16 is fixed to the second side 12 of the main housing 10 by screws S03, for example, by 26 screws S03. The screws are located at the bottom of the metal base plate 16, which makes the metal base plate 16 reliably connected to the main housing 10, while ensuring that no screws are visible on the surface.

[0110] According to some exemplary embodiments, in conjunction with reference to Figure 13 and Figure 14 The metal base plate 16 may include a first base plate 161 and a second base plate 162. The portion with a relatively uniform thickness is processed into the first base plate 161, and the portion exceeding the thickness is separated and processed into the second base plate 162. The second base plate 162 is then assembled onto the first base plate 161 using screws or structural adhesive to obtain the metal base plate 16. Considering energy conservation, low carbon emissions, and environmental protection, the metal base plate 16 is designed with a split structure, which reduces the thickness of the raw material and thus lowers costs. With this design, the material cost of the metal base plate 16 can be reduced by 50%, and the processing cost can be reduced by more than 60% due to the elimination of large areas of material waste, meaning the overall cost can be reduced by more than half.

[0111] According to some exemplary embodiments, in conjunction with reference to Figure 15 and Figure 16A silicone pad 163 is also provided on the side of the metal base plate 16 away from the main housing 10, which can increase the stability and flatness of the main housing 10.

[0112] According to some exemplary embodiments, in conjunction 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 near the main housing 10. The shape of the limiting frame 164 is consistent with the shape of the first hollow hole LK1. The size of the limiting frame 164 is slightly smaller than the size of the first hollow hole LK1. The limiting frame 164 can fit into the first hollow hole LK1. It plays an auxiliary positioning role in the installation process of the metal base plate 16 and the main housing 10, thereby improving the assembly accuracy.

[0113] According to some exemplary embodiments, in conjunction with reference to Figure 7 , Figure 10 , Figure 11 and Figure 18 The cockpit structure also includes at least one support member 40, which is located within the receiving 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 opposite to the display surface, and the other side of the support member 40 is connected to the metal base plate 16 of the second side 12 of the main housing 10. The support member 40 provides support for the back of the first display module 21, effectively preventing deformation of the first display module 21 over time.

[0114] According to some exemplary embodiments, in conjunction 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.

[0115] The first support member 41 includes a first strip 411 and a second strip 412, which are vertically connected in an L-shape. The first strip 411 extends parallel to the horizontal plane. The end of the first strip 411 away from the second strip 412 is connected to the side of the first display module 21 away from the windshield WS, and the end of the second strip 412 away from the first strip 411 is connected to the side of the first display module 21 near the windshield WS. For example, the end of the first strip 411 away from the second strip 412 is connected to the fixing portion 31 of the bracket 30 on the side away from the windshield WS, and the end of the second strip 412 away from the first strip 411 is connected to the fixing portion 31 of the bracket 30 on the side near the windshield WS.

[0116] The second support member 42 includes a third strip 421, a fourth strip 422, and a fifth strip 423. The third strip 421 and the fifth strip 423 are spaced apart along the first direction D1, and their extension directions are both parallel to the horizontal plane. The fourth strip 422 connects the third strip 421 and the fifth strip 423. The third strip 421 is connected to the side of the first strip 411 away from the first display module 21, and the fifth strip 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 stable support for the first display module 21 and is not easily deformed during long-term support.

[0117] According to some exemplary embodiments, refer to Figure 1 , Figure 17 and Figure 18 The fourth strip 422 extends perpendicular to the horizontal plane. One end of the fourth strip 422 is connected to the end of the third strip 421 away from the windshield WS, and the other end of the fourth strip 422 is connected to the end of the fifth strip 423 away from the windshield WS. The second support member 42 is roughly C-shaped. Supporting the fourth strip 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.

[0118] According to some exemplary embodiments. See also Figure 11The cockpit structure includes at least two support members 40, which are spaced apart along a second direction D2. The cockpit structure also includes at least one reinforcing plate 43, located between the at least two support members 40, and connected to the side of the first display module 21 opposite to the display surface. The at least two support members 40 support both sides of the first display module 21 along the second direction D2, and the reinforcing plate 43 strengthens the middle portion of the first display module 21. This provides stable support for the first display module 21, and the reinforcing effect of the reinforcing plate 43 effectively prevents deformation of the first display module 21.

[0119] According to some exemplary embodiments, refer to Figure 11 The cross-sectional shape of the reinforcing plate 43 can be consistent with the cross-sectional shape of the first support member 41, and is L-shaped. The dimension of the reinforcing plate 43 along the second direction D2 is larger than the dimension of the support member 40 along the second direction D2.

[0120] According to some exemplary embodiments, the materials of the support 40 and the reinforcing plate 43 may include metal.

[0121] According to some exemplary embodiments, refer to Figure 12 An FPGA board 44 can also be installed on the side of the reinforcing plate 43 away from the first display module 21. The FPGA board 44 is fixedly connected to the reinforcing plate 43 by four screws S04.

[0122] According to some exemplary embodiments, in conjunction with reference to Figure 1 , Figure 5 and Figure 7 The main housing 10 includes a third side surface 13, which is located on the side away from the windshield WS along the third direction D3. A second perforation LK2 is provided on the third side surface 13. The size of the second perforation LK2 along the second direction D2 is larger than the size of the first display module 21 along the second direction D2. During later maintenance, the second perforation LK2 serves as a maintenance hole, allowing for convenient access to and from the first display module 21.

[0123] According to some exemplary embodiments, in conjunction with reference to Figure 1 , Figure 5 and Figure 7The main housing 10 includes a fourth side surface 14, which is located near the windshield WS along a third direction D3. At least two third perforated holes LK3 are provided on the fourth side surface 14, spaced apart along a second direction D2. Considering the heat dissipation requirements of the first display module 21, the third perforated holes LK3 are provided on the side of the main housing 10 near the windshield WS as heat dissipation holes. The two third perforated holes LK3 are spaced apart along the second direction D2 to avoid affecting the strength of the main housing 10.

[0124] Figure 19 The diagram schematically illustrates the structure of the rear panel of the first display module of the cockpit structure according to some embodiments of the present invention. Figure 20 The diagram schematically shows a side view of the rear panel of a first display module of a cockpit structure according to some embodiments of the present invention. Figure 21 Schematic illustration Figure 20 A magnified view of region B in the middle. Figure 22 An assembly diagram of a first display module of a cockpit structure according to some embodiments of the present invention is shown schematically. Figure 23 Schematic illustration Figure 22 A magnified view of region C in the middle.

[0125] According to some exemplary embodiments, the first display module, as a projection light source for a head-up display, requires high display brightness, for example, a maximum brightness of up to 7000 nits. High brightness displays generate more heat, and to avoid overheating during use, a structure is provided on the back panel 2115 of the first display module to improve heat dissipation efficiency.

[0126] Combined with reference Figure 19 , Figure 20 and Figure 21 The back panel 2115 is provided with multiple fins 21151 arranged at intervals, which can increase the surface area of ​​the back panel away from the display panel, thereby improving heat dissipation efficiency.

[0127] According to some exemplary embodiments, refer to Figure 21 Multiple fins 21151 are evenly arranged, and the shape of the fins 21151 can be a cylinder with a hemispherical top. The thickness of the fins 21151 along the direction perpendicular to the back plate 2115 is T1, the thickness of the portion of the back plate 2115 without fins 21151 is T2, the width of the fins 21151 is D1, and the spacing between adjacent fins 21151 is D2. To achieve better heat dissipation efficiency, T1, T2, D1, and D2 can be set according to Table 1 below.

[0128] Table 1

[0129]

[0130] According to some exemplary embodiments, refer to Figure 19 Multiple fins 21151 are arranged in the area where the circuit board 2116 is not provided, while the fins 21151 are not provided in the area where the circuit board 2116 is provided.

[0131] According to some exemplary embodiments, in conjunction with reference to Figure 22 and Figure 23 To facilitate rapid assembly of the first display module 21 and improve production line efficiency, the front frame 211 and the rear panel 2115 are connected by snap-fit ​​fasteners. Compared to the traditional screw-fixing design, assembly efficiency can be increased by 70%, and the snap-fit ​​fastening method improves the aesthetics of the first display module 21 compared to the external screw fixing method. For example, a snap-fit ​​fastener can be provided on one side of the rear panel 2115, and a machining notch that mates with the snap-fit ​​fastener can be provided on one side of the front frame 211.

[0132] According to some exemplary embodiments, in conjunction with reference to Figure 1 and Figure 5 The cockpit structure also includes two side plates 51, which are connected to the main housing 10 on both sides along the second direction D2. The side plates 51 extend away from the windshield WS and are flush with the two sides of the main housing 10 along the second direction D2. Each side plate 51 has a fourth cutout LK4 and a fifth cutout LK5, which can be spaced apart along the first direction D1. The cutout area of ​​the fourth cutout LK4 can be larger than that of the fifth cutout LK5. The fourth cutout LK4 is used to house the second display module, and the fifth cutout LK5 is used to house the control board electrically connected to the second display module, as described later.

[0133] Figure 24 An exploded view of a first cover assembly of a cockpit structure according to some embodiments of the present invention is shown schematically. Figure 25 The diagram schematically illustrates the structure of a first cover assembly of a cockpit structure according to some embodiments of the present invention. Figures 26-27 The diagram illustrates the assembly of the first cover plate assembly with the main housing of a cockpit structure according to some embodiments of the present invention. Figure 28 The diagram illustrates the assembly of a first cover plate and a first decorative plate of a cockpit structure according to some embodiments of the present invention. Figure 29 The diagram schematically illustrates a light bar assembly structure of a cockpit structure according to some embodiments of the present invention. Figure 30 Schematic illustration along Figure 29 A sectional view taken from the center direction DD'.

[0134] According to some exemplary embodiments, in conjunction with reference to Figure 1 , Figure 26 and Figure 27 The cockpit structure includes a first cover assembly 60, which is located on the side of the main housing 10 away from the windshield WS. The first cover assembly 60 is bent on both sides of the second direction D2 away from the windshield WS and covers the two side panels 51. The first cover assembly 60 is provided with two sixth hollow holes LK6 on both sides of the second direction D2. The two sixth hollow holes LK6 expose a portion of the two fourth hollow holes LK4 provided on the two side panels 51.

[0135] According to some exemplary embodiments, in conjunction with reference to Figure 1 , Figure 24 , Figure 25 , Figure 26 and Figure 28 The first cover plate assembly 60 includes a first cover plate 61, a first decorative panel 63, a second cover plate 62, a second decorative panel 64, and a light strip assembly 65. The first decorative panel 63 is disposed on the side of the first cover plate 61 away from the main housing 10, and the second decorative panel 64 is disposed on the side of the second cover plate 62 away from the main housing 10. The first cover plate 61 and the second cover plate 62 are connected along a first direction D1, and the light strip assembly 65 is disposed between the first cover plate 61 and the second cover plate 62. The first cover plate 61 is disposed on the side closer to the windshield WS and is connected to the first side 11 of the main housing 10. The second cover plate 62 is disposed on the side further away from the windshield WS and is connected to the second side 12 of the main housing 10.

[0136] It should be noted that, in order to more clearly illustrate the structure of the first cover plate 61 and the second cover plate 62, in Figure 24 The first decorative panel 63 and the second decorative panel 64 are omitted in the text. Figures 25-27 The first decorative panel 63 is omitted in the text.

[0137] According to some exemplary embodiments, in conjunction with reference to Figure 26 and Figure 27 The first cover plate 61 has a sixth perforated hole LK6 on each side along the second direction D2.

[0138] According to some exemplary embodiments, in conjunction with reference to Figure 26The first cover plate 61 is also provided with a seventh perforated hole LK7, which is located between the two sixth perforated holes LK6. The maximum dimension of the seventh perforated 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 to say, the maximum dimension of the seventh perforated 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 perforated hole LK7 provided in the first cover plate 61 and the second perforated hole LK2 provided in the main housing 10 together serve as maintenance holes for the first display module 21.

[0139] According to some exemplary embodiments, in conjunction with reference to Figure 29 and Figure 30 The light strip assembly 65 includes an LED light panel 651, RGB LED beads 652, a light diffuser 653, and a light guide strip 654. The LED light panel 651 can be made of aluminum, and the RGB LED beads 652 can be adjusted to different colors and brightness levels as needed. The light diffuser 653 is made of transparent PC or PMMA material, and a matte texture is required to prevent light leakage from the light guide strip. The light guide strip 654 is made of transparent plastic, such as PC or PMMA. The light strip assembly 65 can serve as an ambient light in the vehicle, creating a comfortable and warm environment for the driver and passengers, reducing driving fatigue, improving the riding experience, and enhancing in-vehicle comfort.

[0140] According to some exemplary embodiments, refer to Figure 24 The first cover plate 61, the light strip assembly 65, and the second cover plate 62 are connected together by eight screws S06 using a sandwich structure.

[0141] According to some exemplary embodiments, in conjunction with reference to Figure 26 and Figure 27 The assembled first cover plate assembly 60 is fastened to the main housing 10 using internal hidden screws, ensuring that no screw is exposed, thus achieving a hidden connection.

[0142] Figure 31 The diagram schematically illustrates the structure of the A-pillar support member of the cockpit structure according to some embodiments of the present invention. Figure 32 The diagram illustrates the assembly of the A-pillar support member and the main shell of the cockpit structure according to some embodiments of the present invention. Figure 33 The diagram schematically illustrates the structural composition of the A-pillar support and the main shell of the cockpit structure according to some embodiments of the present invention.

[0143] According to some exemplary embodiments, in conjunction with reference to Figure 3 , Figure 31 , Figure 32 and Figure 33The cockpit structure also includes an A-pillar support 52, which includes two support portions 521 located on both sides of the second direction D2 and a connecting portion 522 connecting the two support portions 521. The support portions 521 are triangular in shape and have a triangular hollow structure inside to enhance aesthetics. The A-pillar support 52 is fixed to the first side 11 of the main housing 10 by screws. The inclination of the surface of the A-pillar support 52 near the windshield WS matches the inclination of the windshield WS to provide support for the windshield WS.

[0144] Figure 34 The diagram schematically illustrates the assembly of the air vent frame and the front shell of the cockpit structure according to some embodiments of the present invention. Figure 34 This diagram illustrates the assembly as viewed from above. Figure 35 The diagram schematically illustrates the assembly of the air outlet frame and the main housing of the cockpit structure according to some embodiments of the present invention. Figure 35 This diagram illustrates the assembly as viewed from above.

[0145] According to some exemplary embodiments, in conjunction with reference to Figure 34 and Figure 35 The cockpit structure also includes a front shell 53 and an air vent frame 54. The front shell 53 has a ninth perforated hole LK9, and the air vent frame 54 has a tenth perforated hole LK10. The air vent frame 54 is fixed to the front shell 53 around the ninth perforated hole LK9 by screws, with all screws concealed. Both the ninth and tenth perforated holes LK9 and LK10 are strip-shaped perforations extending along the second direction D2, and they are connected, serving as heat dissipation channels for the electronic components inside the main housing 10.

[0146] According to some exemplary embodiments, in conjunction 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 shell 10 with screws. The ninth cutout LK9 and the tenth cutout LK10 are connected to at least two third cutouts LK3.

[0147] Figure 36 The diagram illustrates the assembly of the A-pillar decorative frame and A-pillar support member of the cockpit structure according to some embodiments of the present invention. Figure 37 Schematic illustration Figure 36 A magnified view of region E in the middle. Figure 38 Schematic illustration along Figure 37 A sectional view taken from the center direction FF'.

[0148] According to some exemplary embodiments, in conjunction with reference to Figure 3 , Figure 36, Figure 37 and Figure 38 In the A-pillar support 52, two support portions 521 are respectively provided with A-pillar decorative frames 55 along the outer side of the second direction D2. The A-pillar decorative frames 55 are triangular rings. A fixing groove 5211 is provided on the side of the support portion 521 near the windshield WS. The A-pillar decorative frame 55 is provided with a fixing protrusion 551 that mates with the fixing groove 5211. The fixing protrusion 551 is installed in the fixing groove 5211 with an interference fit and is fixed in the fixing groove 5211 by screws S07.

[0149] According to some exemplary embodiments, refer to Figure 37 The A-pillar decorative frame 55 is provided with a first positioning post 552 on the inner side near the support part 521. The support part 521 is also provided with a first positioning groove 5212 that cooperates with the first positioning post 552. When the A-pillar decorative frame 55 is installed on the support part 521, the first positioning post 552 and the first positioning groove 5212 play an auxiliary positioning role.

[0150] In the cockpit structure of this embodiment, the first display module 21, which has a relatively large size along the second direction D2, is cleverly designed and arranged to be hidden inside the control panel. It then acts as a light source projected onto the windshield, creating a large display effect that covers the entire area from A-pillar to A-pillar, allowing the windshield to simultaneously display instrument, navigation, and multimedia entertainment information. Through this structural design, the first display module 21 can be securely fixed to the main housing 10, effectively preventing the first display module 21 from loosening or deforming during long-term use, which could affect the display effect.

[0151] Figure 39 The diagram illustrates the assembly of the second display module and control panel with the side panel of the cockpit structure according to some embodiments of the present invention. Figure 40 Schematic illustration Figure 39 A magnified view of region G in the middle. Figure 41 The diagram schematically illustrates the combined structure of the second display module and control panel with the side panel of the cockpit structure according to some embodiments of the present invention. Figure 42 Schematic illustration Figure 41 A magnified view of region H in the middle.

[0152] According to some exemplary embodiments, in conjunction with reference to Figure 39 , Figure 40 , Figure 41 and Figure 42The second display module 22 is connected to the side of the side plate 51 away from the first cover plate assembly 60. The second display module 22 is fixed to the fourth cutout hole LK4 of the side plate 51 by a half-buckle and half-pressing block locking method. Buckles 511 are provided on the outer sides of the two adjacent sides of the fourth cutout hole LK4. The edge of the second display module 22 slides into the two buckles 511, and then the edge of the second display module 22 is pressed down by two pressing blocks 512, and fixed to the side plate 51 by screws S13. One pressing block 512 is located on the other side of one buckle 511 along the first direction D1, and the other pressing block 512 is located on the other side of the other buckle 511 along the third direction D3. The fourth cutout hole LK4 of the side plate 51 and the sixth cutout hole LK6 of the first cover plate assembly 60 expose the display surface of the second display module 22.

[0153] The two second display modules 22 located on either side of the second direction D2 can function as electronic rearview mirrors while driving, providing blind-spot-free electronic display inside the vehicle and thus improving driving safety. According to some exemplary embodiments, in conjunction with reference to... Figure 39 , Figure 40 , Figure 41 and Figure 42 The cockpit structure also includes two control boards 58, which are respectively arranged adjacent to two second display modules 22. The control boards 58 are electrically connected to the adjacent second display modules 22 via flexible flat cables, and can control the second display modules 22 to display in conjunction with the first display module. The control board 58 is connected to the side of the side plate 51 away from the first cover plate assembly 60, and is fixed to the fifth cutout hole LK5 of the side plate 51 by screws S14. The fifth cutout hole LK5 can serve as an inspection hole for the control board 58.

[0154] Figure 43 An exploded view of a second display module of a cockpit structure according to some embodiments of the present invention is shown schematically. Figure 44 The illustration shows a physical diagram of a second display module of a cockpit structure according to some embodiments of the present invention.

[0155] According to some exemplary embodiments, in conjunction with reference to Figure 43 and Figure 44 The second display module 22 also has a touch-sensitive glass 224 and a touch-sensitive decorative film 225 on one side of the light-emitting surface. 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 plate assembly 60 can be consistent, for example, both are wood grain, so that when the second display module 22 is turned off, it presents a seamless hidden effect with the first cover plate assembly 60, which can effectively reduce the interference of the reflection of the second display module 22 on the driver. Figure 45 The diagram schematically illustrates the internal structure of the main housing of the cockpit structure according to some embodiments of the present invention.

[0156] According to some exemplary embodiments, refer to Figure 2 and Figure 45 The main housing 10 contains several electronic components within its accommodating space 10a, including a first fan 81, a second fan 82, and a third fan 83. The first fan 81 and second fan 82 are intake fans, and the third fan 83 is an exhaust fan. The first fan 81 and second fan 82 are located on either side of the third fan 83 along the second direction D2, allowing air to enter from both sides and exit from the center, achieving a bidirectional circulating heat dissipation effect. The circulation direction can be referenced... Figure 2 The direction indicated by the middle arrow.

[0157] Figure 46 The diagram illustrates an assembly schematic of a steering wheel grip in a cockpit structure according to some embodiments of the present invention. Figure 47 The diagram schematically illustrates the structure of the steering wheel grip of a cockpit structure according to some embodiments of the present invention. Figure 48 Schematic illustration along Figure 47 A cross-sectional view taken along the center line of JJ'. According to some exemplary embodiments, in conjunction with reference to... Figure 46 , Figure 47 and Figure 48 The cockpit structure also includes a steering wheel 90, which includes a steering wheel grip 91. The steering wheel grip 91 can be octagonal in shape, including a left grip 911 and a right grip 912. The left grip 911 and the right grip 912 can be made of PC or ABS plastic as the base material, and the surface is covered with two-tone organic leather 915. Both the left grip 911 and the right grip 912 have clearance grooves 91a, and the edges of the leather 915 are hidden in the clearance grooves 91a so that the leather 915 can be covered smoothly.

[0158] exist Figure 48 In this context, m represents the width of the clearance groove, and n represents the depth of the clearance groove. m and n are adjusted according to different thicknesses of leather, and usually need to meet the requirements of 2≤m≤5mm and 1≤n≤2mm.

[0159] After the leather is wrapped, insert the left grip 911 and the right grip 912 into the first connector 913 and the second connector 914 at the same time, and fix the left grip 911 and the right grip 912 to the first connector 913 with screw S18, and fix the left grip 911 and the right grip 912 to the second connector 914 with screw S19.

[0160] This application also provides a vehicle, which may include a body and a cabin structure located within the body as provided in the above embodiments.

[0161] As used herein, the terms “substantially,” “approximately,” “about,” and other similar terms are used as terms of approximation rather than as terms of degree, and they are intended to account for inherent deviations in measured or calculated values ​​that would be recognized by one of ordinary skill in the art. Taking into account factors such as process variations, measurement problems, and errors associated with the measurement of a particular quantity (i.e., limitations of the measurement system), “approximately” or “about” as used herein includes the stated value and indicates that the particular value is within an acceptable range of deviation for one of ordinary skill in the art. For example, “approximately” may mean within one or more standard deviations, or within ±10% or ±5% of the stated value.

[0162] While some embodiments of the general inventive concept of this utility model have been illustrated and described, those skilled in the art will understand that changes may be made to these embodiments without departing from the principles and spirit of the general inventive concept of this utility model, the scope of which is defined by the claims and their equivalents.

Claims

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

2. The cockpit structure according to claim 1, wherein The main housing includes a second side surface, which is located on opposite sides of the first side surface in the first direction; and The display surface of the first display module is inclined relative to the horizontal plane, and the side of the first display module closer to the windshield is closer to the second side than the side of the first display module farther from the windshield.

3. The cockpit structure according to claim 2, wherein The main housing includes a receiving space. 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. The protrusion distance of the skirt structure on the side closer to the windshield is smaller than the protrusion distance of the skirt structure on the side farther from the windshield. The first display module is connected to the skirt structure via the bracket.

4. The cockpit structure according to claim 3, wherein The bracket is ring-shaped and connected to the edge of the first display module. The bracket includes a fixing part that protrudes from both sides of the first display module along the third direction and is connected to the skirt structure.

5. The cockpit structure according to claim 4, wherein The fixing part along the third direction away from the windshield includes a plurality of fixing sub-parts spaced apart, and an abutting part is provided between adjacent fixing sub-parts. The abutting part is perpendicular to the fixing sub-part and is fixedly connected to the side of the second display module away from the windshield.

6. The cockpit structure according to any one of claims 3-5, wherein, The cockpit structure further includes at least one support member, wherein at least one support member is located within the accommodating space; and One side of the support member is connected to the side of the first display module that is away from the display surface, and the other side of the support member is connected to the second side of the main housing.

7. The cockpit structure according to claim 6, wherein The support includes a first support and a second support connected along the first direction; The first support member comprises a first strip and a second strip, which are vertically connected. The first strip extends parallel to a horizontal plane. The end of the first strip away from the second strip is connected to the side of the first display module away from the windshield. The end of the second strip away from the first strip is connected to the side of the first display module closer to the windshield. The second support member includes a third strip, a fourth strip, and a fifth strip. The third strip and the fifth strip are spaced apart along the first direction. The fourth strip is connected between the third strip and the fifth strip. The third strip is connected to the side of the first strip away from the first display module. The fifth strip is connected to the second side.

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

9. The cockpit structure according to claim 7 or 8, wherein The second side is provided with a first hollow hole. The cockpit structure also includes a metal base plate, which is disposed on the second side and covers the first hollow hole. The side of the second support member away from the first display module is connected to the metal base plate.

10. The cockpit structure according to claim 6, wherein The cockpit structure includes at least two support members, which are spaced apart along the second direction; and The cockpit structure also includes at least one reinforcing plate located between at least two of the support members, and the reinforcing plate is connected to the side of the first display module opposite to the display surface.

11. The cockpit structure of claim 10, wherein, The dimension of the reinforcing plate along the second direction is larger than the dimension of the support member along the second direction.

12. The cockpit structure according to any one of claims 1-5, 7-8, 10-11, wherein, The main housing includes a third side surface, which is located on the side away from the windshield along the third direction. A second perforation is provided on the third side surface, and the size of the second perforation along the second direction is larger than the size of the module mounting hole along the second direction.

13. The cockpit structure of any of claims 1-5, 7-8, 10-11, wherein, The main housing includes a fourth side surface, which is located near the windshield along the third direction. At least two third hollow holes are provided on the fourth side surface, and the at least two third hollow holes are spaced apart along the second direction.

14. The cockpit structure of any of claims 2-5, 7-8, 10-11, 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 of any of claims 1-5, 7-8, 10-11, wherein, The cockpit structure also includes two side panels, which are respectively connected to the two sides of the main shell along the second direction, and the side panels extend away from the windshield. The cockpit structure also includes two second display modules, which are respectively disposed on the two side panels, with each second display module located on the side of one side panel away from the other side panel; and The side panel is provided with a fourth cutout hole, which exposes the display surface of the second display module.

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

17. The cockpit structure of claim 16, wherein, The side panel is provided with a fifth cutout hole, which exposes at least a portion of the control panel.

18. The cockpit structure of claim 15, wherein, The cockpit structure includes a first cover assembly disposed on the side of the main housing away from the windshield, the first cover assembly being bent on both sides in the second direction away from the windshield and covering the two side panels; and The first cover plate assembly is provided with a sixth cutout hole, which exposes the display surface of the second display module.

19. The cockpit structure of claim 18, wherein, The first cover plate assembly includes a first cover plate, a second cover plate, and a light strip assembly. The first cover plate and the second cover plate are connected along a first direction, and the light strip assembly is disposed between the first cover plate and the second cover plate.

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

21. A vehicle, wherein, The vehicle includes a cockpit structure according to any one of claims 1-20.

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