CN209467213U - Front cabin force transmission structure and automobile - Google Patents

Front cabin force transmission structure and automobile Download PDF

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Publication number
CN209467213U
CN209467213U CN201920127568.8U CN201920127568U CN209467213U CN 209467213 U CN209467213 U CN 209467213U CN 201920127568 U CN201920127568 U CN 201920127568U CN 209467213 U CN209467213 U CN 209467213U
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engine room
connecting plate
longitudinal beam
cabin
front longitudinal
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何玉俊
杨宏
姜叶洁
郑中心
陈宗明
黄兴
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Guangzhou Automobile Group Co Ltd
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Guangzhou Automobile Group Co Ltd
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Abstract

本实用新型公开了前机舱传力结构,包括机舱上边梁、机舱前纵梁、通道总成以及分别与机舱上边梁和机舱前纵梁连接的机舱轮罩,通道总成位于机舱轮罩的后侧且两端分别与机舱上边梁和机舱前纵梁连接,通道总成包括上连接板和连接上连接板的下连接板,上连接板与下连接板之间形成有第一传力腔,第一传力腔的两端分别延伸至机舱上边梁和机舱前纵梁;在机舱轮罩的后侧增设通道总成,有利于应力的吸收和分散;通道总成内设置第一传力腔,有利于吸收整车载荷,在满足整车性能目标的同时,对整车底盘的性能有一定的提升,还实现了通道总成减重,进而有利于车身轻量化;在前悬吸能空间减小时,能有效引导及分解前碰能量,从而实现碰撞力的传递分解。

The utility model discloses a force transmission structure of a front engine room, which comprises an upper side beam of the engine room, a front longitudinal beam of the engine room, a channel assembly and an engine room wheel cover respectively connected with the upper side beam of the engine room and the front longitudinal beam of the engine room, and the channel assembly is located at the rear of the wheel cover of the engine room The side and both ends are respectively connected with the upper side beam of the engine room and the front longitudinal beam of the engine room. The channel assembly includes an upper connecting plate and a lower connecting plate connected to the upper connecting plate. A first force transmission chamber is formed between the upper connecting plate and the lower connecting plate. The two ends of the first force transmission chamber respectively extend to the upper side beam of the engine room and the front longitudinal beam of the engine room; a channel assembly is added on the rear side of the wheel house of the engine room, which is conducive to the absorption and dispersion of stress; the first force transmission cavity is arranged in the channel assembly , which is conducive to absorbing the load of the whole vehicle. While meeting the performance goals of the whole vehicle, the performance of the chassis of the whole vehicle has been improved to a certain extent, and the weight reduction of the channel assembly has also been realized, which is conducive to the weight reduction of the vehicle body; the energy-absorbing space of the front suspension When it is reduced, it can effectively guide and decompose the front impact energy, so as to realize the transmission and decomposition of the collision force.

Description

前机舱传力结构及汽车Front cabin force transmission structure and automobile

技术领域technical field

本实用新型属于汽车领域,特别是涉及前机舱传力结构及汽车。The utility model belongs to the field of automobiles, in particular to a force transmission structure of a front cabin and an automobile.

背景技术Background technique

汽车的机舱轮罩分别与机舱上边梁和机舱前纵梁连接,以此形成前机舱传力结构,存在刚度不足的问题。因此,现有技术中,存在增加一根钢制横梁直接连接机舱上边梁和机舱前纵梁,来满足车身刚度需求,既导致汽车重量增加、成本上升,又难以实现前碰吸能空间不足情况下的碰撞力分解。The engine room wheel housing of the automobile is respectively connected to the upper side beam of the engine room and the front longitudinal beam of the engine room to form a force transmission structure of the front engine room, which has the problem of insufficient rigidity. Therefore, in the prior art, there is a steel crossbeam directly connected to the upper side beam of the cabin and the front longitudinal beam of the cabin to meet the rigidity requirements of the vehicle body, which not only leads to an increase in vehicle weight and cost, but also makes it difficult to realize the lack of energy-absorbing space for the front collision The following collision force decomposition.

实用新型内容Utility model content

本实用新型所要解决的技术问题是:针对现有方案重量重且难以实现前碰吸能空间不足情况下的碰撞力分解的问题,提供一种前机舱传力结构及汽车。The technical problem to be solved by the utility model is: to provide a front engine room force transmission structure and an automobile in view of the problem that the existing scheme is heavy and difficult to realize the decomposition of the collision force when the energy absorption space of the front collision is insufficient.

为解决上述技术问题,本实用新型实施例提供了一种前机舱传力结构,包括机舱上边梁、机舱前纵梁、机舱轮罩和通道总成,所述机舱轮罩分别与所述机舱上边梁和所述机舱前纵梁连接,所述通道总成位于所述机舱轮罩的后侧且两端分别与所述机舱上边梁和所述机舱前纵梁连接,所述通道总成包括上连接板和连接所述上连接板的下连接板,所述上连接板与所述下连接板之间形成有第一传力腔,所述第一传力腔的两端分别延伸至所述机舱上边梁和所述机舱前纵梁。In order to solve the above-mentioned technical problems, the embodiment of the utility model provides a force transmission structure of the front nacelle, including the nacelle upper beam, the nacelle front longitudinal beam, the nacelle wheel cover and the channel assembly, and the nacelle wheel house and the nacelle upper side respectively The beam is connected to the front longitudinal beam of the engine room, the channel assembly is located at the rear side of the wheel house of the engine room and its two ends are respectively connected to the upper side beam of the engine room and the front longitudinal beam of the engine room, and the channel assembly includes an upper A connection plate and a lower connection plate connected to the upper connection plate, a first force transmission cavity is formed between the upper connection plate and the lower connection plate, and the two ends of the first force transmission cavity respectively extend to the The nacelle roof rail and the nacelle front stringer.

可选地,所述上连接板的一端连接于所述机舱上边梁的内侧,另一端连接于所述机舱前纵梁的上侧;所述下连接板的一端连接于所述机舱上边梁的下侧,另一端连接于所述机舱前纵梁的内侧。Optionally, one end of the upper connecting plate is connected to the inner side of the roof rail of the cabin, and the other end is connected to the upper side of the front longitudinal beam of the cabin; one end of the lower connecting plate is connected to the side beam of the cabin roof. The lower side, and the other end is connected to the inner side of the front longitudinal beam of the cabin.

可选地,所述上连接板的面向所述下连接板的一侧形成有第一凹腔,所述第一凹腔沿所述上连接板的延伸方向贯通所述上连接板;所述下连接板的面向所述上连接板的一侧形成有第二凹腔,所述第二凹腔沿所述下连接板的延伸方向贯通所述下连接板;所述第一凹腔和所述第二凹腔组合成所述第一传力腔。Optionally, a first concave cavity is formed on a side of the upper connecting plate facing the lower connecting plate, and the first concave cavity penetrates through the upper connecting plate along the extending direction of the upper connecting plate; A second concave cavity is formed on the side of the lower connecting plate facing the upper connecting plate, and the second concave cavity penetrates the lower connecting plate along the extending direction of the lower connecting plate; the first concave cavity and the The second concave cavity is combined to form the first force transmission cavity.

可选地,所述上连接板弯折成几字形,所述下连接板弯折成倒几字形,所述第一传力腔为六边形腔体。Optionally, the upper connecting plate is bent into a zigzag shape, the lower connecting plate is bent into a zigzag shape upside down, and the first force transmission cavity is a hexagonal cavity.

可选地,所述通道总成与所述机舱轮罩间隔设置。Optionally, the channel assembly is spaced apart from the nacelle wheel housing.

可选地,所述上连接板包括上边梁连接板和前纵梁连接板,所述上边梁连接板的一端连接于所述机舱上边梁,所述前纵梁连接板一端连接于所述机舱前纵梁,另一端连接于所述上边梁连接板的远离所述机舱上边梁的一端。Optionally, the upper connection plate includes a roof side sill connection plate and a front side sill connection plate, one end of the roof side sill connection plate is connected to the cabin roof side sill, and one end of the front side sill connection plate is connected to the cabin The other end of the front longitudinal beam is connected to the end of the roof side beam connecting plate away from the cabin roof side beam.

可选地,所述上边梁连接板与所述下连接板之间焊接密封,所述上边梁连接板的端部与所述机舱上边梁自冲铆连接,所述前纵梁连接板与所述机舱前纵梁热融自攻丝连接;Optionally, the connection plate of the upper side sill is welded and sealed with the lower connection plate, the end of the connection plate of the upper side sill is connected with the upper side sill of the cabin by self-piercing riveting, and the connection plate of the front longitudinal sill is connected to the cabin Hot-melt self-tapping connection of the front longitudinal beam;

所述上边梁连接板的端部与所述前纵梁连接板的端部搭接并焊接;所述上边梁连接板和所述前纵梁连接板中的至少一种板的用于搭接另一种板的端部设有阶梯面。The end of the upper side sill connecting plate overlaps and welds the end of the front side sill connecting plate; at least one of the upper side sill connecting plate and the front longitudinal sill connecting plate is used for overlapping Another type of plate is provided with a stepped surface at the end.

可选地,所述机舱轮罩和所述通道总成上设有减重孔。Optionally, lightening holes are provided on the nacelle wheel cover and the channel assembly.

可选地,所述机舱轮罩的底部的前后两侧均设有第二传力腔;Optionally, the front and rear sides of the bottom of the nacelle wheel cover are provided with a second force transmission chamber;

所述机舱轮罩为铸铝轮罩,所述机舱上边梁的材质为钢材,所述机舱前纵梁的材质为铝材,所述通道总成的材质为铝材。The engine room wheel cover is a cast aluminum wheel cover, the material of the upper side beam of the engine room is steel, the material of the front longitudinal beam of the engine room is aluminum, and the material of the channel assembly is aluminum.

本实用新型实施例还提供了一种汽车,包括副车架安装总成和前机舱传力结构,所述通道总成与副车架安装总成相对。The embodiment of the utility model also provides an automobile, which includes a sub-frame installation assembly and a force transmission structure in the front cabin, and the channel assembly is opposite to the sub-frame installation assembly.

本实用新型实施例提供的前机舱传力结构及汽车,在机舱轮罩的后侧增设了连接机舱上边梁和机舱前纵梁的通道总成,副车架安装板总成受到的Z向载荷传递至机舱前纵梁,再经机舱轮罩和通道总成分解传递至机舱上边梁,前碰受力传递至机舱前纵梁,一部分沿机舱前纵梁传递,另一部分经机舱轮罩和通道总成传递至机舱上边梁,再沿机舱上边梁传递,有利于应力的吸收和分散;通道总成内设置第一传力腔,有利于吸收整车载荷,在满足整车性能目标的同时,对整车底盘的性能有一定的提升,还实现了通道总成减重,进而有利于车身轻量化;在同级别车型前悬吸能空间减小同时,能有效引导及分解前碰能量,从而实现碰撞力的传递分解。The front engine room force transmission structure and the automobile provided by the embodiment of the utility model have added a channel assembly connecting the upper side beam of the engine room and the front longitudinal beam of the engine room on the rear side of the wheel house of the engine room, and the Z-direction load received by the sub-frame mounting plate assembly It is transmitted to the front longitudinal beam of the engine room, and then transmitted to the upper side beam of the engine room through the assembly of the wheel house and the channel. The assembly is transmitted to the upper side beam of the engine room, and then transmitted along the upper side beam of the engine room, which is conducive to the absorption and dispersion of stress; the first force transmission chamber is set in the channel assembly, which is conducive to absorbing the load of the whole vehicle. While meeting the performance goals of the whole vehicle, The performance of the vehicle chassis has been improved to a certain extent, and the weight reduction of the channel assembly has been realized, which is conducive to the lightweight of the vehicle body; while the energy absorption space of the front suspension of the same level of models is reduced, it can effectively guide and decompose the front impact energy, thereby Realize the transmission and decomposition of collision force.

附图说明Description of drawings

图1为本实用新型实施例提供的前机舱传力结构的使用状态参考图;Fig. 1 is the reference diagram of the use state of the front engine room force transmission structure provided by the embodiment of the present invention;

图2为图1的A向视图;Fig. 2 is the A direction view of Fig. 1;

图3为本实用新型实施例提供的前机舱传力结构的爆炸图;Fig. 3 is the exploded view of the force transmission structure of the front nacelle provided by the embodiment of the utility model;

图4为图1中通道总成的截面示意图;Fig. 4 is a schematic cross-sectional view of the channel assembly in Fig. 1;

图5为图1中机舱上边梁、通道总成和机舱前纵梁的截面示意图。Fig. 5 is a schematic cross-sectional view of the upper side beam of the nacelle, the channel assembly and the front longitudinal beam of the nacelle in Fig. 1 .

说明书中的附图标记如下:The reference signs in the instructions are as follows:

1、机舱上边梁;2、机舱前纵梁;1. The upper beam of the engine room; 2. The front longitudinal beam of the engine room;

3、机舱轮罩;31、第二传力腔;3. Engine room wheel cover; 31. The second force transmission chamber;

4、通道总成;41、上连接板;411、第一凹腔;412、上边梁连接板;413、前纵梁连接板;42、下连接板;421、第二凹腔;4. Channel assembly; 41. Upper connecting plate; 411. First concave cavity; 412. Upper side beam connecting plate; 413. Front longitudinal beam connecting plate; 42. Lower connecting plate; 421. Second concave cavity;

43、第一传力腔;44、阶梯面;43. The first force transmission cavity; 44. The stepped surface;

5、减重孔;5. Lightening holes;

6、副车架安装总成。6. Subframe installation assembly.

具体实施方式Detailed ways

为了使本实用新型所解决的技术问题、技术方案及有益效果更加清楚明白,以下结合附图及实施例,对本实用新型进行进一步的详细说明。应当理解,此处所描述的具体实施例仅用以解释本实用新型,并不用于限定本实用新型。In order to make the technical problems, technical solutions and beneficial effects solved by the utility model clearer, the utility model will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the utility model, and are not intended to limit the utility model.

如图1至图4所示,本实用新型实施例提供了前机舱传力结构,包括机舱上边梁1、机舱前纵梁2、机舱轮罩3和通道总成4,机舱轮罩3分别与机舱上边梁1和机舱前纵梁2连接,通道总成4位于机舱轮罩3的后侧且两端分别与机舱上边梁1和机舱前纵梁2连接,通道总成4包括上连接板41和连接上连接板41的下连接板42,上连接板41与下连接板42之间形成有第一传力腔43,第一传力腔43的两端分别延伸至机舱上边梁1和机舱前纵梁2。As shown in Fig. 1 to Fig. 4, the embodiment of the utility model provides the force transmission structure of the front engine room, including the engine room upper beam 1, the engine room front longitudinal beam 2, the engine room wheel cover 3 and the channel assembly 4, and the engine room wheel cover 3 is connected with the engine room respectively. The engine room roof beam 1 is connected to the engine room front longitudinal beam 2, the channel assembly 4 is located at the rear side of the engine room wheel house 3 and its two ends are respectively connected to the engine room roof beam 1 and the engine room front beam 2, and the channel assembly 4 includes an upper connecting plate 41 and the lower connecting plate 42 connecting the upper connecting plate 41, a first force transmission chamber 43 is formed between the upper connecting plate 41 and the lower connecting plate 42, and the two ends of the first force transmission chamber 43 respectively extend to the cabin roof rail 1 and the cabin Front longitudinal beam 2.

本实用新型实施例提供的前机舱传力结构,在机舱轮罩3的后侧增设了连接机舱上边梁1和机舱前纵梁2的通道总成4,副车架安装板总成受到的Z向载荷传递至机舱前纵梁2,再经机舱轮罩3和通道总成4分解传递至机舱上边梁1,前碰受力传递至机舱前纵梁2,一部分沿机舱前纵梁2传递,另一部分经机舱轮罩3和通道总成4传递至机舱上边梁1,再沿机舱上边梁1传递,有利于应力的吸收和分散;通道总成4内设置第一传力腔43,有利于吸收整车载荷,在满足整车性能目标的同时,对整车底盘的性能有一定的提升,还实现了通道总成4减重,进而有利于车身轻量化;在同级别车型前悬吸能空间减小同时,能有效引导及分解前碰能量,从而实现碰撞力的传递分解。In the front engine room power transmission structure provided by the embodiment of the utility model, a channel assembly 4 connecting the upper side beam 1 of the engine room and the front longitudinal beam 2 of the engine room is added on the rear side of the wheel house 3 of the engine room, and the subframe mounting plate assembly is subjected to Z The load is transmitted to the front longitudinal beam 2 of the nacelle, and then decomposed and transmitted to the upper side beam 1 of the nacelle through the wheel house 3 and the channel assembly 4. The other part is transmitted to the cabin roof beam 1 through the cabin wheel cover 3 and the channel assembly 4, and then transmitted along the cabin roof beam 1, which is conducive to the absorption and dispersion of stress; the first force transmission chamber 43 is set in the channel assembly 4, which is beneficial to Absorb the load of the whole vehicle, while meeting the performance target of the whole vehicle, it can improve the performance of the chassis of the whole vehicle to a certain extent, and also realize the weight reduction of the channel assembly 4, which is beneficial to the weight reduction of the body; While the space is reduced, it can effectively guide and decompose the front collision energy, so as to realize the transmission and decomposition of the collision force.

本申请的前机舱传力结构既适用于左轮罩处的动力传递,又适用于右轮罩处的动力传递;具体地,机舱上边梁1、机舱前纵梁2和机舱轮罩3可分别为机舱左上边梁、机舱左前纵梁和机舱左轮罩,也可分别为机舱右上边梁、机舱右前纵梁和机舱右轮罩。The power transmission structure of the front cabin of the present application is not only suitable for the power transmission at the left wheelhouse place, but also suitable for the power transmission at the right wheelhouse place; The left upper side beam of the engine room, the left front longitudinal beam of the engine room and the left wheel cover of the engine room can also be respectively the right upper side beam of the engine room, the right front longitudinal beam of the engine room and the right wheel cover of the engine room.

在一实施例中,如图1、图2和图5所示,上连接板41的一端连接于机舱上边梁1的内侧(本申请中,机舱上边梁1的内侧指机舱上边梁1的靠近车身宽度方向上的中部的一侧),另一端连接于机舱前纵梁2的上侧;下连接板42的一端连接于机舱上边梁1的下侧,另一端连接于机舱前纵梁2的内侧(本申请中,机舱前纵梁2的内侧指机舱前纵梁2的靠近车身宽度方向上的中部的一侧)。避免碰撞力过大导致结构拉裂,保证完成碰撞力沿上端的有效分解。In one embodiment, as shown in Fig. 1, Fig. 2 and Fig. 5, one end of the upper connecting plate 41 is connected to the inner side of the roof rail 1 of the cabin (in this application, the inner side of the roof rail 1 of the cabin refers to the approaching side of the roof rail 1 of the cabin. One side of the middle part in the width direction of the vehicle body), the other end is connected to the upper side of the front longitudinal beam 2 of the cabin; Inner side (in this application, the inner side of the front side member 2 of the nacelle refers to the side near the middle of the front side member 2 in the vehicle body width direction). Avoid excessive collision force causing structural cracking, and ensure the effective decomposition of collision force along the upper end.

在一实施例中,如图3和图4所示,上连接板41的面向下连接板42的一侧形成有第一凹腔411,第一凹腔411沿上连接板41的延伸方向贯通上连接板41;下连接板42的面向上连接板41的一侧形成有第二凹腔421,第二凹腔421沿下连接板42的延伸方向贯通下连接板42;上连接板41与下连接板42连接后第一凹腔411和第二凹腔421组合成第一传力腔43。第一传力腔43由上连接板41和下连接板42上的凹腔(第一凹腔411和第二凹腔421)组合形成,更有利于通道总成4吸收、分解应力,从而增加承载能力。In one embodiment, as shown in FIG. 3 and FIG. 4 , a first cavity 411 is formed on the side of the upper connecting plate 41 facing the lower connecting plate 42 , and the first cavity 411 penetrates along the extending direction of the upper connecting plate 41 The upper connecting plate 41; the side of the lower connecting plate 42 facing the upper connecting plate 41 is formed with a second concave cavity 421, and the second concave cavity 421 penetrates the lower connecting plate 42 along the extension direction of the lower connecting plate 42; the upper connecting plate 41 and After the lower connection plate 42 is connected, the first cavity 411 and the second cavity 421 are combined to form the first force transmission cavity 43 . The first force transmission cavity 43 is formed by the combination of the concave cavities (the first concave cavity 411 and the second concave cavity 421) on the upper connecting plate 41 and the lower connecting plate 42, which is more conducive to the absorption and decomposition of stress by the channel assembly 4, thereby increasing Carrying capacity.

在一实施例中,如图3和图4所示,上连接板41弯折成几字形,几字形上连接板41的内部凹腔即第一凹腔411,下连接板42弯折成倒几字形,倒几字形下连接板42的内部凹腔即第二凹腔421,第一传力腔43为六边形腔体(即上连接板41与下连接板42连接后形成的整体结构在车身XZ平面内的截面的空腔呈六边形,参见图4),能够增加连接通道自身刚度,减重的同时,满足承载需求。In one embodiment, as shown in Fig. 3 and Fig. 4, the upper connecting plate 41 is bent into a several-shaped shape, the inner cavity of the upper connecting plate 41 in the shape of a few characters is the first cavity 411, and the lower connecting plate 42 is bent into an inverted shape. The inner cavity of the lower connecting plate 42 is the second concave cavity 421 in the shape of a few characters, and the inner cavity of the lower connecting plate 42 is the second cavity 421. The cavity of the section in the XZ plane of the vehicle body is hexagonal, see Figure 4), which can increase the stiffness of the connecting channel itself, reduce weight and meet the load-bearing requirements.

在一实施例中,如图1所示,通道总成4与机舱轮罩3间隔设置,如此机舱上边梁1、机舱前纵梁2、机舱轮罩3和通道总成4形成封闭式框架传力结构,增加结构稳定性。In one embodiment, as shown in FIG. 1 , the channel assembly 4 is spaced apart from the nacelle wheel house 3, so that the nacelle upper beam 1, the nacelle front longitudinal beam 2, the nacelle wheel house 3 and the channel assembly 4 form a closed frame transmission. Force structure, increase structural stability.

在一实施例中,如图3和图5所示,上连接板41包括上边梁连接板412和前纵梁连接板413,上边梁连接板412的一端连接于机舱上边梁1,前纵梁连接板413一端连接于机舱前纵梁2,另一端连接于上边梁连接板412的远离机舱上边梁1的一端;如此将上连接板41设为两段式结构,方便通道总成4的拼装、以及通道总成4与机舱上边梁1和机舱前纵梁2的连接。In one embodiment, as shown in FIG. 3 and FIG. 5 , the upper connecting plate 41 includes a roof side sill connecting plate 412 and a front longitudinal beam connecting plate 413, one end of the roof side beam connecting plate 412 is connected to the cabin roof side beam 1, and the front side beam One end of the connecting plate 413 is connected to the front longitudinal beam 2 of the engine room, and the other end is connected to the end of the upper side sill connecting plate 412 away from the upper side beam 1 of the engine room; in this way, the upper connecting plate 41 is set as a two-stage structure, which facilitates the assembly of the channel assembly 4 , and the connection of the channel assembly 4 with the cabin roof rail 1 and the cabin front longitudinal beam 2.

在一实施例中,上边梁连接板412与下连接板42之间焊接密封(优选SPR连接),上边梁连接板412的端部与机舱上边梁1自冲铆连接(即SPR连接),前纵梁连接板413与机舱前纵梁2热融自攻丝连接(即FDS连接)。实现前机舱传力结构的轻量化连接。In one embodiment, the upper side sill connecting plate 412 and the lower connecting plate 42 are welded and sealed (preferably SPR connection), the end of the upper side sill connecting plate 412 is self-piercing riveted to the cabin upper side sill 1 (that is, SPR connection), and the front The longitudinal beam connecting plate 413 is thermally melted and self-tapping connected to the front longitudinal beam 2 of the engine room (ie FDS connection). Realize the lightweight connection of the force transmission structure of the front cabin.

在一实施例中,上边梁连接板412和前纵梁连接板413之间焊接,下连接板42的一端与机舱上边梁1自冲铆连接(即SPR连接),另一端与机舱前纵梁2热融自攻丝连接(即FDS连接),能实现前机舱传力结构的轻量化连接。In one embodiment, the upper side beam connecting plate 412 and the front longitudinal beam connecting plate 413 are welded, one end of the lower connecting plate 42 is self-piercingly riveted to the cabin upper side beam 1 (i.e. SPR connection), and the other end is connected to the cabin front longitudinal beam 2. Hot-melt self-tapping connection (FDS connection), which can realize the lightweight connection of the force transmission structure of the front cabin.

在一实施例中,如图5所示,上边梁连接板412的端部与前纵梁连接板413的端部搭接并焊接,保证了连接处的力学性能。优选地,上边梁连接板412和前纵梁连接板413中的至少一种板的用于搭接另一种板的端部设有阶梯面44,即上边梁连接板412用于连接前纵梁连接板413的一端和/或前纵梁连接板413的用于连接上边梁连接板412的一端设有阶梯面44,有利于增加处的承载能力,避免撕裂。In one embodiment, as shown in FIG. 5 , the end of the upper side sill connecting plate 412 is overlapped with the end of the front side sill connecting plate 413 and welded to ensure the mechanical properties of the joint. Preferably, at least one of the upper side sill connecting plate 412 and the front longitudinal sill connecting plate 413 is provided with a stepped surface 44 at the end of at least one of the plates used to overlap the other, that is, the upper side sill connecting plate 412 is used to connect the front longitudinal One end of the beam connecting plate 413 and/or one end of the front longitudinal sill connecting plate 413 used to connect to the upper side sill connecting plate 412 is provided with a stepped surface 44, which is beneficial to increase the bearing capacity and avoid tearing.

在一实施例中,如图3所示,机舱轮罩3和通道总成4上设有减重孔5,有利于车身轻量化。In one embodiment, as shown in FIG. 3 , a lightening hole 5 is provided on the nacelle wheel cover 3 and the channel assembly 4 , which is beneficial to the weight reduction of the vehicle body.

在一实施例中,如图2所示,机舱轮罩3的底部的前后两侧均设有第二传力腔31,增加机舱轮罩3吸收、分散应力的能力,有效引导及分解碰撞能量。In one embodiment, as shown in FIG. 2 , the front and rear sides of the bottom of the nacelle wheel house 3 are provided with second force transmission chambers 31 to increase the ability of the nacelle wheel house 3 to absorb and disperse stress, and effectively guide and decompose the collision energy. .

在一实施例中,机舱轮罩3为铸铝轮罩,机舱上边梁1的材质为钢材,机舱前纵梁2的材质为铝材,通道总成4的材质为铝材。如此形成钢铝车身的局部结构,多个结构采用铝材,既方便加工,又有利于减重。In one embodiment, the nacelle wheel housing 3 is a cast aluminum wheel housing, the nacelle upper side beam 1 is made of steel, the nacelle front longitudinal beam 2 is made of aluminum, and the material of the channel assembly 4 is aluminum. In this way, the partial structure of the steel-aluminum body is formed, and multiple structures are made of aluminum, which is not only convenient for processing, but also conducive to weight reduction.

如图1和图2所示,本实用新型实施例还提供了汽车,包括前述任一实施例述及的前机舱传力结构。通过具有第一传力腔43的通道总成4,实现减重,同时满足各项性能需求,尤其适用于钢铝车身;实现了前碰吸能空间不足情况下,有效引导及分解前碰能量,从而实现碰撞力的传递分解满足五星需求。As shown in Fig. 1 and Fig. 2, the embodiment of the present utility model also provides a car, including the force transmission structure of the front cabin mentioned in any of the foregoing embodiments. The channel assembly 4 with the first force transmission chamber 43 realizes weight reduction and meets various performance requirements at the same time, especially suitable for steel and aluminum bodies; realizes the effective guidance and decomposition of front collision energy in the case of insufficient energy absorption space for front collision , so as to realize the transmission and decomposition of the collision force to meet the five-star requirements.

在一实施例中,如图1和图2所示,通道总成4与副车架安装总成6相对,实现机舱前纵梁2的连接副车架安装总成6的部位的加强,同时有利于Z向载荷的引导及分解。优选通道总成4与副车架安装总成6正对。In one embodiment, as shown in FIG. 1 and FIG. 2 , the channel assembly 4 is opposite to the sub-frame installation assembly 6 to realize the reinforcement of the part of the front longitudinal beam 2 connected to the sub-frame installation assembly 6 of the cabin, and at the same time It is conducive to the guidance and decomposition of Z-direction loads. Preferably, the channel assembly 4 is directly opposite to the subframe mounting assembly 6 .

以上仅为本实用新型的较佳实施例而已,并不用以限制本实用新型,凡在本实用新型的精神和原则之内所作的任何修改、等同替换和改进等,均应包含在本实用新型的保护范围之内。The above are only preferred embodiments of the present utility model, and are not intended to limit the present utility model. Any modifications, equivalent replacements and improvements made within the spirit and principles of the present utility model should be included in the utility model. within the scope of protection.

Claims (10)

1. a kind of forward engine room force transferring structure, including cabin roof side rail, engine room front longitudinal beam and cabin wheel cover, the cabin wheel cover difference It is connect with the cabin roof side rail and the engine room front longitudinal beam, which is characterized in that further include channel assembly, channel assembly position In the cabin wheel cover rear side and both ends connect respectively with the cabin roof side rail and the engine room front longitudinal beam, the channel is total At including upper junction plate and the lower connecting plate for connecting the upper junction plate, formed between the upper junction plate and the lower connecting plate There is the first power transmission chamber, the both ends of the first power transmission chamber extend respectively to the cabin roof side rail and the engine room front longitudinal beam.
2. forward engine room force transferring structure according to claim 1, which is characterized in that one end of the upper junction plate is connected to institute The inside of cabin roof side rail is stated, the other end is connected to the upside of the engine room front longitudinal beam;One end of the lower connecting plate is connected to The downside of the cabin roof side rail, the other end are connected to the inside of the engine room front longitudinal beam.
3. forward engine room force transferring structure according to claim 1, which is characterized in that the upper junction plate towards the lower company The side of fishplate bar is formed with the first cavity, and first cavity penetrates through the upper connection along the extending direction of the upper junction plate Plate;The side towards the upper junction plate of the lower connecting plate is formed with the second cavity, and second cavity is along the lower company The extending direction of fishplate bar penetrates through the lower connecting plate;First cavity and second cavity combination are at first power transmission Chamber.
4. forward engine room force transferring structure according to claim 3, which is characterized in that the upper junction plate is bent into zigzag shape, The lower connecting plate is bent into down zigzag shape, and the first power transmission chamber is hexagon cavity.
5. forward engine room force transferring structure according to claim 1, which is characterized in that the channel assembly and the cabin wheel cover Interval setting.
6. forward engine room force transferring structure according to claim 1-5, which is characterized in that the upper junction plate includes upper Side bar connecting plate and front longitudinal beam connecting plate, one end of the roof side rail connecting plate is connected to the cabin roof side rail, vertical before described Beam one end of the connection board is connected to the engine room front longitudinal beam, and the other end is connected in the separate cabin of the roof side rail connecting plate One end of side bar.
7. forward engine room force transferring structure according to claim 6, which is characterized in that the roof side rail connecting plate and the lower company Welded seal between fishplate bar, the end of the roof side rail connecting plate are connect with the cabin roof side rail self-pierce riveting, the front longitudinal beam Connecting plate melts thread tapping with the engine room front longitudinal beam heat and connect;
The lapping ends of the end of the roof side rail connecting plate and the front longitudinal beam connecting plate and welding;The roof side rail connecting plate Cascaded surface is equipped with the end for overlapping another plate of at least one of front longitudinal beam connecting plate plate.
8. forward engine room force transferring structure according to claim 1, which is characterized in that the cabin wheel cover and the channel assembly It is equipped with lightening hole.
9. forward engine room force transferring structure according to claim 1, which is characterized in that the front and back two of the bottom of the cabin wheel cover Side is equipped with the second power transmission chamber;
The cabin wheel cover is cast aluminium wheel cover, and the material of the cabin roof side rail is steel, and the material of the engine room front longitudinal beam is Aluminium, the material of the channel assembly are aluminium.
10. automobile, including subframe installation assembly, which is characterized in that including forward engine room described in any one of claim 1-9 Force transferring structure, the channel assembly are opposite with subframe installation assembly.
CN201920127568.8U 2019-01-24 2019-01-24 Front cabin force transmission structure and automobile Active CN209467213U (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110626427A (en) * 2019-11-05 2019-12-31 威马智慧出行科技(上海)有限公司 Automobile small offset collision force transmission mechanism and automobile including it
CN112278088A (en) * 2020-09-15 2021-01-29 东风汽车集团有限公司 An engine compartment stabilizer bar assembly and engine compartment
CN116923557A (en) * 2023-07-11 2023-10-24 东风柳州汽车有限公司 Vehicle body structure and vehicle

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110626427A (en) * 2019-11-05 2019-12-31 威马智慧出行科技(上海)有限公司 Automobile small offset collision force transmission mechanism and automobile including it
CN112278088A (en) * 2020-09-15 2021-01-29 东风汽车集团有限公司 An engine compartment stabilizer bar assembly and engine compartment
CN116923557A (en) * 2023-07-11 2023-10-24 东风柳州汽车有限公司 Vehicle body structure and vehicle

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