Cockpit and vehicle

Abstract

The utility model discloses a cockpit and a vehicle, the cockpit comprises a cabin body and a force dispersion assembly, the force dispersion assembly is arranged on any side face of the cabin body, and the force dispersion assembly is suitable for dispersing impact force to the outside of the side face, where the force dispersion assembly is arranged, of the cabin body after bearing impact. According to the cockpit, the local deformation resistance and energy absorption capacity of the cockpit body can be optimized, sharp objects and a deformed cockpit body part can be prevented from invading the cockpit, and the life and property safety of a driver and passengers is effectively improved.

Description

Technical Field

[0001] The utility model relates to the technical field of automobile seats, in particular to a cockpit and a vehicle. Background Art

[0002] As human society continues to change, society's demand for faster and more efficient transportation of materials is increasing. Therefore, high speed, heavy load, and new energy have become the development trend of future logistics and transportation. The engine compartment of a truck is under the cockpit. There is no engine compartment to act as a buffer and protect during a collision. The above characteristics of freight vehicles or construction machinery increase the danger to drivers and passengers. At present, the cab is equipped with safety devices such as airbags and air curtains. When a vehicle has an accident, the airbag can reduce or avoid injuries. However, in reality, when a serious collision occurs or the cargo slides or rolls from the cargo box to the cockpit, the cockpit will be severely deformed and punctured. At this time, even if the airbag is opened, the fatal injury rate of the driver and passengers is still extremely high. To solve this problem, the main means currently used is to add triangular reinforcement ribs to the cockpit frame structure to stabilize the structure to prevent excessive deformation.

[0003] In the related technology, a stable structure is added to the cockpit. When responding to impacts from different directions and to different degrees, the cockpit frame structure cannot evenly absorb deformation energy and impact energy, resulting in a significant reduction in the cockpit's ability to withstand impact locally. Sharp objects can easily damage local parts of the cockpit and penetrate into the cockpit. Local parts of the cockpit that are severely deformed can also easily penetrate into the cockpit, increasing the risk of casualties to the driver and passengers. Utility Model Content

[0004] The utility model aims to solve at least one of the technical problems existing in the prior art. To this end, one purpose of the utility model is to provide a cockpit that can optimize the local anti-deformation performance and energy absorption capacity of the cabin body, prevent sharp objects and deformed cabin parts from invading the interior of the cockpit, and effectively improve the safety of life and property of drivers and passengers.

[0005] The utility model also provides a vehicle with the driving cabin.

[0006] According to the cockpit of the embodiment of the first aspect of the utility model, the cockpit includes: a cabin body and a force dispersion component, wherein the force dispersion component is arranged on any side of the cabin body, and the force dispersion component is suitable for dispersing the impact force to the outside of the side of the cabin body where the force dispersion component is arranged after being subjected to an impact.

[0007] According to the cockpit of the utility model, the deformation absorption and impact resistance of the cabin body can be improved by setting a force dispersion component, and the local anti-deformation performance of the cabin body can be optimized. This can prevent sharp objects and deformed cabin body parts from invading the interior of the cockpit, and can effectively improve the safety of life and property of the driver and passengers.

[0008] According to some embodiments of the present invention, the force dispersion assembly includes: a plurality of dispersion plates, wherein the plurality of dispersion plates are sequentially arranged in a direction away from the cabin.

[0009] Furthermore, in the direction away from the cabin body, the number of the dispersion plates in each layer gradually decreases, the dispersion plates in the latter layer are connected to the dispersion plates in the former layer, and the plurality of dispersion plates in the latter layer are located between adjacent dispersion plates in the former layer.

[0010] In some embodiments, the dispersion plate is configured as a curved plate, and the curved plate is convex toward the cockpit.

[0011] Furthermore, the force dispersing assembly is disposed on a back plate of the cabin body and is at least partially opposite to the cargo hold at the rear side of the cockpit.

[0012] Furthermore, the cockpit also includes: a frame and a seat, a weakened connecting plate is provided on the back panel corresponding to the force dispersion component, the frame is provided on the weakened connecting plate and is rotatably connected to the cabin body; the seat is provided on the frame.

[0013] According to some embodiments of the present invention, the dispersion plate is configured as a circular plate.

[0014] According to a vehicle of an embodiment of the second aspect of the utility model, the vehicle includes: a cockpit as described in any one of the above embodiments.

[0015] Additional aspects and advantages of the present invention will be given in part in the following description, and in part will become apparent from the following description, or will be learned through the practice of the present invention. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] The above and / or additional aspects and advantages of the present invention will become apparent and easily understood from the description of the embodiments in conjunction with the following drawings, in which:

[0017] Figure 1 It is a schematic diagram of the structure of the cockpit part according to some embodiments of the utility model;

[0018] Figure 2 is a cross-sectional schematic diagram of a force dispersion assembly on a cabin according to some embodiments of the utility model;

[0019] Figure 3 is a schematic diagram of a dispersion plate according to some embodiments of the utility model;

[0020] Figure 4 yes Figure 3 Middle AA section view;

[0021] Figure 5It is a schematic diagram of the cooperation between the cabin, the frame and the seat according to some embodiments of the utility model.

[0022] Reference numerals:

[0023] Cockpit 1;

[0024] Cabin 11, back plate 111;

[0025] Force dispersing assembly 12, dispersing plate 121;

[0026] Frame 13, seat 14. DETAILED DESCRIPTION

[0027] In order to make the purpose, technical solution and advantages of the embodiments of the present application clearer, the technical solution in the embodiments of the present application will be clearly described below in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are part of the embodiments of the present application, not all of the embodiments. Based on the embodiments in the present application, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of this application.

[0028] Unless otherwise defined, all technical and scientific terms used in this application have the same meanings as those commonly understood by technicians in the technical field of this application; the terms used in the specification of this application are only for the purpose of describing specific embodiments and are not intended to limit this application; the terms "including" and "having" in the specification and claims of this application and the above-mentioned drawings and any variations thereof are intended to cover non-exclusive inclusions. The terms "first", "second", etc. in the specification and claims of this application or the above-mentioned drawings are used to distinguish different objects, rather than to describe a specific order or a primary and secondary relationship.

[0029] Reference to "embodiment" in this application means that a particular feature, structure, or characteristic described in conjunction with the embodiment may be included in at least one embodiment of the present application. The appearance of the phrase in various places in the specification does not necessarily refer to the same embodiment, nor is it an independent or alternative embodiment that is mutually exclusive with other embodiments.

[0030] In the description of this application, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "connected", "connected", and "attached" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a direct connection, or an indirect connection through an intermediate medium, or it can be the internal communication of two elements. For ordinary technicians in this field, the specific meanings of the above terms in this application can be understood according to specific circumstances.

[0031] The term "and / or" in this application is only a description of the association relationship of associated objects, indicating that there can be three relationships. For example, A and / or B can represent: A exists alone, A and B exist at the same time, and B exists alone. In addition, the character " / " in this application generally indicates that the associated objects before and after are in an "or" relationship.

[0032] In the embodiments of the present application, the same reference numerals represent the same components, and for the sake of brevity, detailed descriptions of the same components are omitted in different embodiments. It should be understood that the thickness, length, width and other dimensions of various components in the embodiments of the present application shown in the drawings, as well as the overall thickness, length, width and other dimensions of the integrated device are only exemplary descriptions and should not constitute any limitation to the present application.

[0033] In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise", "axial", "radial", "circumferential" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the referred device or element must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be understood as a limitation on the present invention.

[0034] In the description of the present invention, a first feature being “above” or “below” a second feature may include that the first and second features are directly in contact with each other, or may include that the first and second features are not in direct contact but are in contact with each other via another feature therebetween.

[0035] In the description of the present invention, a first feature “above”, “over” and “above” a second feature includes the first feature being directly above and obliquely above the second feature, or simply means that the first feature is horizontally higher than the second feature.

[0036] The term "plurality" used in the present application refers to two or more (including two).

[0037] Reference below Figure 1-Figure 5 A cockpit 1 and a vehicle according to embodiments of the present invention are described.

[0038] like Figure 1 As shown, according to the cockpit 1 of the first embodiment of the utility model, the cockpit 1 includes: a cabin body 11 and a force dispersion component 12.

[0039] The force dispersion component 12 is disposed on any side surface of the cabin 11 , and the force dispersion component 12 is suitable for dispersing the impact force outward from the side surface of the cabin 11 where the force dispersion component 12 is disposed after being subjected to an impact.

[0040] Specifically, the force dispersion component 12 can be disposed on any side of the cabin 11, such as the back side, left side, or right side of the cabin 11. When the cabin 11 is hit (for example, the vehicle rolls over, causing the left and right sides of the cabin 11 to be hit, etc.), the force dispersion component 12 can disperse the impact force exerted on the local part of the cabin 11 to the outside of the cabin 11, wherein the impact force is dispersed to the outside of the cabin 11, including but not limited to dispersing outward toward the side of the cabin 11 perpendicular to the side of the cabin 11 on which the force dispersion component 12 is disposed, and dispersing outward toward the side of the cabin 11 parallel to the side of the cabin 11 on which the force dispersion component 12 is disposed, thereby achieving the transmission of the impact force to the cabin 11 as a whole for sharing, and effectively improving the ability of the cabin 11 to absorb deformation energy and impact energy.

[0041] It should be pointed out that the cockpit 1 disclosed in the embodiment of the present application can be used for but not limited to vehicles, ships, spacecraft and other devices. The cockpit 1 having the cabin body 11, force dispersion component 12 and other components disclosed in the present application can be used to form the device. This is conducive to improving the scope of application of the cockpit 1 and improving the safety of riding in the cockpit 1.

[0042] According to the cockpit 1 of the utility model, the force dispersion component 12 can be set to improve the deformation absorption and impact resistance of the cabin body 11, optimize the local deformation resistance of the cabin body 11, avoid sharp objects and deformed cabin body 11 parts from invading the interior of the cockpit 1, and effectively improve the safety of life and property of the driver and passengers.

[0043] like Figure 2 As shown, according to some embodiments of the present invention, the force dispersion assembly 12 includes: a plurality of dispersion plates 121 , and the plurality of dispersion plates 121 are arranged in sequence in a direction away from the cabin 11 .

[0044] Specifically, the dispersion plate 121 can be constructed in multiple layers, and the multiple layers of dispersion plates 121 can be sequentially arranged in the direction away from the cabin 11 (defined by the cockpit 1 space, which is the direction from the inside to the outside of the cockpit 1). For example, if the force dispersion component 12 is arranged on the back side of the cabin 11, the multiple layers of dispersion plates 121 are sequentially arranged in the direction from the front to the back of the cabin 11. If the force dispersion component 12 is arranged on the left side of the cabin 11, the multiple layers of dispersion plates 121 are sequentially arranged in the direction from the right to the left of the cabin 11. In this way, the multiple layers of dispersion plates 121 can transmit and attenuate the impact force in multiple stages, and the force and energy during the collision can be absorbed and dispersed by each layer of dispersion plates 121 in turn, which can effectively reduce the impact force and vibration transmission during the collision. In addition, the multiple layers of dispersion plates 121 can also enhance the structural strength and rigidity of the cabin 11, thereby improving the dispersion and energy absorption effect of the cabin 11 on the impact force, and ensuring that the cabin 11 has good anti-deformation ability.

[0045] like Figure 2 As shown, according to some embodiments of the present invention, in the direction away from the cabin 11, the number of dispersion plates 121 in each layer gradually decreases, the dispersion plates 121 of the latter layer are connected to the dispersion plates 121 of the former layer, and the multiple dispersion plates 121 of the latter layer are located between adjacent dispersion plates 121 in the dispersion plates 121 of the former layer.

[0046] Specifically, in the direction away from the cabin 11 (defined by the cockpit 1 space, which is the direction from the inside to the outside of the cockpit 1), the number of dispersion plates 121 in each layer gradually decreases, that is, the number of dispersion plates 121 in the next layer is less than the number of dispersion plates 121 in the previous layer. In addition, the dispersion plates 121 in the next layer are located between the adjacent dispersion plates 121 in the previous layer, forming a structure in which the dispersion plates 121 in the next layer fill the gaps between the dispersion plates 121 in the previous layer, and are arranged in a staggered manner in the inside and outside directions of the cockpit 1. In this way, the force dispersion assembly 12 can be guaranteed to play a good role in force transmission and dispersion, while improving lightweight, which is conducive to reducing costs and increasing efficiency.

[0047] Preferably, in this embodiment, the dispersion plate 121 is constructed into two layers, the first dispersion plate 121 is arranged on any side of the cabin 11, and the second dispersion plate 121 is arranged on the side of the first dispersion plate 121 facing the cockpit 1 to ensure the energy absorption effect and reduce costs and increase efficiency.

[0048] It can be understood that the multiple dispersion plates 121 in each layer can be arranged in an array. For example, the multiple dispersion plates 121 in each layer can be arranged in rows in the horizontal direction and in columns in the height direction to form a rectangular array. The multiple dispersion plates 121 in each layer can also be distributed in a small number in the middle area and in a large number in the peripheral area to form a circular array, etc. This will help to further improve the uniformity of the force dispersion component 12 in transmitting and dispersing the impact force, and will help to further enhance the ability of the cabin 11 to uniformly withstand impact energy.

[0049] It should be pointed out that the above-mentioned arrangement of the dispersion plates 121 is an exemplary description, and the multiple dispersion plates 121 in each layer can also be configured to be staggered up and down to further improve the lightweight, and the multiple dispersion plates 121 in each layer can also be configured to be arranged in a grid-like manner to increase the overall force-bearing area of ​​each layer of dispersion plates 121 and provide greater energy absorption capacity. All structural forms that can be arranged in the same plane are within the scope of protection of this application.

[0050] like Figure 2-Figure 4 As shown, according to some embodiments of the present invention, the dispersion plate 121 is constructed as an arc-shaped plate, and the arc-shaped surface is convex toward the cockpit 1 .

[0051] Specifically, each dispersion plate 121 can be constructed as an arc-shaped plate, and the arc-shaped surface of the arc-shaped plate protrudes toward the cockpit 1, so that the surface of the arc-shaped plate facing the cockpit 1 is a smooth surface. When the cabin 11 is impacted by the outside world, the arc-shaped plate can play a good buffering and protective role, and can protect the driver and passengers from being hurt by sharp objects in the outside world and the cabin 11, thereby providing a higher level of protection for the driver and passengers.

[0052] like Figure 1 and Figure 2 As shown, according to some embodiments of the present invention, the force dispersing assembly 12 is disposed on the back plate 111 of the cabin 11 and is at least partially opposite to the cargo hold at the rear side of the cockpit 1 .

[0053] Specifically, the force dispersing assembly 12 can be disposed on the back plate 111 of the cabin 11, and the force dispersing assembly 12 is at least partially opposite to the cargo hold behind the cockpit 1. In some embodiments, when the vehicle brakes suddenly or a collision occurs, the transported materials in the cargo hold may slide or roll forward and hit the back plate 111 of the cabin 11, and the force dispersing assembly 12 disposed on the back plate 111 can quickly absorb and disperse the impact energy, thereby preventing the transported materials in the cargo hold from piercing the back plate 111 and invading the cockpit 1, and can specifically improve the energy absorption capacity of the vulnerable position of the cabin 11, thereby achieving a better protection effect.

[0054] like Figure 5 As shown, according to some embodiments of the present invention, the cockpit 1 further includes: a frame 13 and a seat 14 .

[0055] Among them, a weakened connecting plate is arranged on the back plate 111 for the stress dispersion component 12 , and the frame 13 is arranged on the weakened connecting plate and is rotatably connected to the cabin body 11 ; the seat 14 is arranged on the frame 13 .

[0056] Specifically, the weakened connecting plate can be arranged on the back plate 111 of the cabin 11 and correspond to the force dispersion component 12. When the back side of the cabin 11 is hit, the force dispersion component 12 can evenly disperse the impact force and transmit it to the entire weakened connecting plate. The weakened connecting plate can absorb part of the collision energy and reduce or even avoid the impact force being transmitted to the cabin 11 through controllable deformation, thereby improving the impact resistance of the cabin 11 and protecting the safety of the passengers in the cockpit 1. When the impact on the weakened connecting plate exceeds the impact threshold, it can be separated from the cabin 11, and the frame 13 arranged on the weakened connecting plate can rotate relative to the cabin 11 under the impact force, and drive the seat 14 to rotate, so that the seat 14 is separated from the interior of the cockpit 1, so as to improve the safe escape rate of the passengers.

[0057] like Figure 2 As shown, according to some embodiments of the present invention, the dispersion plate 121 is configured as a circular plate.

[0058] Specifically, each dispersion plate 121 is configured as a circular plate, and the projection of each dispersion plate 121 in the inner and outer directions of the cockpit 1 can be configured as a circle. When impacted, the impact force can be evenly dispersed over the entire surface of the circular plate. Compared with plates of other shapes, the circular plate can more evenly transmit the impact force to various parts, reducing local stress concentration, and the circular plate has a large force dispersion area, which can better disperse and absorb external impact force. Therefore, by configuring the dispersion plate 121 as a circular plate, the overall impact resistance and energy absorption capacity of the force dispersion assembly 12 can be improved.

[0059] like Figure 1-Figure 5 As shown, according to the vehicle of the second aspect of the utility model, the vehicle includes: the cockpit 1 described in any one of the above embodiments, and the technical effects produced are consistent with those in the above embodiments, which will not be repeated here.

[0060] In the description of this specification, the description with reference to the terms "one embodiment", "some embodiments", "illustrative embodiments", "examples", "specific examples", or "some examples" means that the specific features, structures, materials or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the utility model. In this specification, the schematic representation of the above terms does not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described can be combined in any one or more embodiments or examples in a suitable manner.

[0061] Although the embodiments of the present invention have been shown and described, those skilled in the art will appreciate that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the claims and their equivalents.

Claims

1. A cockpit, characterized in that: include: Cabin (11); A force dispersing component (12), wherein the force dispersing component (12) is arranged on any side surface of the cabin (11), and the force dispersing component (12) is suitable for dispersing the impact force to the outside of the side surface of the cabin (11) where the force dispersing component (12) is arranged after being subjected to an impact, and the force dispersing component (12) comprises: a plurality of dispersing plates (121), wherein the plurality of dispersing plates (121) are arranged in sequence in a direction away from the cabin (11).

2. The cockpit according to claim 1, characterized in that: In the direction away from the cabin (11), the number of the dispersion plates (121) in each layer gradually decreases, the dispersion plates (121) in a later layer are connected to the dispersion plates (121) in a previous layer, and the plurality of dispersion plates (121) in a later layer are located between adjacent dispersion plates (121) in a previous layer of dispersion plates (121).

3. The cockpit according to claim 1, characterized in that: The dispersion plate (121) is configured as a curved plate, and the curved plate is convex toward the cockpit.

4. The cockpit according to claim 3, characterized in that: The force dispersing assembly (12) is arranged on the back plate (111) of the cabin (11) and is at least partially opposite to the cargo hold at the rear side of the cockpit.

5. The cockpit according to claim 4, characterized in that: Also includes: A frame (13), wherein a weakened connecting plate is provided on the back plate (111) corresponding to the force dispersing component (12), and the frame (13) is arranged on the weakened connecting plate and is rotatably connected to the cabin (11); A seat (14), wherein the seat (14) is arranged on the frame (13).

6. The cockpit according to any one of claims 1 to 5, characterized in that: The dispersion plate (121) is configured as a circular plate.

7. A vehicle, characterized in that: include: The cockpit according to any one of claims 1 to 6.

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