CN116252864A - Automobile cabin frame structure and automobile - Google Patents
Automobile cabin frame structure and automobile Download PDFInfo
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- CN116252864A CN116252864A CN202111499766.5A CN202111499766A CN116252864A CN 116252864 A CN116252864 A CN 116252864A CN 202111499766 A CN202111499766 A CN 202111499766A CN 116252864 A CN116252864 A CN 116252864A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D25/00—Superstructure or monocoque structure sub-units; Parts or details thereof not otherwise provided for
- B62D25/08—Front or rear portions
- B62D25/082—Engine compartments
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/40—Engine management systems
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Abstract
Description
技术领域technical field
本发明涉及汽车制造领域,尤其涉及一种汽车机舱框架结构、汽车。The invention relates to the field of automobile manufacturing, in particular to an automobile cabin frame structure and an automobile.
背景技术Background technique
现有技术中,车身前端框架结构形式单一,大部分车型的前纵梁在小偏置碰工况中与壁障重叠过小,未能有效传递碰撞能量,存在因前围受力集中而对乘员舱侵入量过大等安全隐患。In the prior art, the frame structure of the front end of the car body is single, and the front longitudinal beam of most models overlaps too little with the barrier in the small offset collision condition, and the collision energy cannot be effectively transmitted. Safety hazards such as excessive intrusion into the passenger compartment.
此外,现有的汽车机舱框架结构还存在传力结构单一,未能对机舱纵梁进行有效支撑等情况。可见,当前的汽车机舱框架结构已无法满足当前日渐严苛的布置环境与碰撞要求。In addition, the existing automobile engine room frame structure still has a single force transmission structure and fails to effectively support the engine room longitudinal beams. It can be seen that the current automobile cabin frame structure can no longer meet the increasingly stringent layout environment and collision requirements.
发明内容Contents of the invention
本发明所要解决的技术问题在于,提供一种汽车机舱框架结构、汽车,优化碰撞传力结构,提升小偏置碰性能;结构精简,轻量化,降低制造成本。The technical problem to be solved by the present invention is to provide an automobile cabin frame structure and automobile, optimize the collision force transmission structure, improve the small offset collision performance; simplify the structure, reduce the weight, and reduce the manufacturing cost.
为了解决上述技术问题,本发明的实施例提供了一种汽车机舱框架结构,包括:前防撞梁总成;机舱纵梁总成,其包括:机舱纵梁前段和与机舱纵梁前段连为一体的机舱纵梁后段,机舱纵梁前段紧固连接有纵梁立柱,机舱纵梁前段的相对两端设有第一装配端和第二装配端,第一装配端与前防撞梁总成紧固相连;A柱总成;机舱上边梁总成,机舱上边梁总成的一端与纵梁立柱紧固相连,机舱上边梁总成的另一端与A柱总成紧固相连;以及前围加强横梁总成,其包括:前围加强中横梁和与前围加强中横梁紧固相连的前围加强底横梁,其中:第二装配端与前围加强中横梁紧固相连,前围加强底横梁与机舱纵梁后段紧固相连,其中:碰撞能量在机舱纵梁前段通过纵梁立柱和机舱上边梁总成分散至A柱总成,由机舱纵梁前段传递至机舱纵梁后段的碰撞能量分别通过前围加强中横梁和前围加强底横梁向A柱总成及车身的另一侧分散传递,以使机舱纵梁后段区域框架的稳定。In order to solve the above-mentioned technical problems, an embodiment of the present invention provides an automobile cabin frame structure, including: a front anti-collision beam assembly; a cabin longitudinal beam assembly, which includes: a front section of the cabin longitudinal beam and a The rear section of the longitudinal beam of the engine room is integrated, the front section of the longitudinal beam of the cabin is fastened to the longitudinal beam column, the opposite ends of the front section of the longitudinal beam of the cabin are provided with a first assembly end and a second assembly end, the first assembly end is connected with the front anti-collision beam The A-pillar assembly; the engine room upper side beam assembly, one end of the engine room upper side beam assembly is fastened to the longitudinal beam column, and the other end of the engine room upper side beam assembly is fastened to the A-pillar assembly; and the front Reinforced crossbeam assembly, which includes: middle reinforced front crossbeam and bottom reinforced bottom crossbeam fastened to the middle reinforced crossbeam, wherein: the second assembly end is fastened and connected to the middle reinforced middle crossbeam, reinforced The bottom beam is firmly connected with the rear section of the cabin longitudinal beam, wherein: the collision energy is dispersed to the A-pillar assembly at the front section of the cabin longitudinal beam through the longitudinal beam column and the upper side beam assembly of the cabin, and is transmitted from the front section of the cabin longitudinal beam to the rear section of the cabin longitudinal beam The collision energy of the collision is distributed and transferred to the A-pillar assembly and the other side of the vehicle body through the front wall reinforcement center cross member and the front wall reinforcement bottom cross member, so as to stabilize the frame of the rear section of the cabin longitudinal beam.
其中,第一装配端的一侧设有前副车架装配位,前副车架通过前副车架装配位紧固在机舱纵梁前段,其中:碰撞能量分别通过前副车架和纵梁立柱对机舱纵梁总成进行拉拽,使碰撞能量传递到机舱纵梁总成上。Among them, one side of the first assembly end is provided with a front sub-frame assembly position, and the front sub-frame is fastened to the front section of the longitudinal beam of the cabin through the front sub-frame assembly position, wherein: the collision energy passes through the front sub-frame and the longitudinal beam column respectively Pull the engine room longitudinal beam assembly, so that the collision energy is transferred to the engine room longitudinal beam assembly.
其中,纵梁立柱与机舱上边梁相连的一端朝机舱框架的外后侧方向平顺过渡。Wherein, the end of the longitudinal beam column connected to the upper side beam of the cabin transitions smoothly towards the outer rear side of the cabin frame.
其中,机舱上边梁自与纵梁立柱相连一端向与A柱总成相连另一端截面方向的尺寸逐渐增大,以使分散至A柱总成的碰撞能够分别向A柱总成的上部和下部传递。Among them, the size of the upper side beam of the engine room gradually increases from the end connected to the longitudinal beam column to the other end connected to the A-pillar assembly, so that the collisions dispersed to the A-pillar assembly can be sent to the upper and lower parts of the A-pillar assembly respectively. transfer.
其中,前防撞梁总成包括;前防撞梁本体、吸能盒及用以带动机舱纵梁前段碰撞吸能的碰撞块;吸能盒和碰撞块分别紧固在前防撞梁本体的端部,吸能盒与第一装配端紧固相连,碰撞块装设在吸能盒的外侧。Among them, the front anti-collision beam assembly includes; the front anti-collision beam body, the energy-absorbing box and the collision block used to drive the collision energy absorption of the front section of the cabin longitudinal beam; the energy-absorbing box and the collision block are respectively fastened to the At the end, the energy-absorbing box is fastened to the first assembly end, and the collision block is arranged on the outside of the energy-absorbing box.
其中,机舱纵梁前段自其中部向第一装配端截面方向的尺寸渐变增大,用以使机舱纵梁前段在撞击时受力参与变形吸能和传递能量。Wherein, the size of the front section of the cabin longitudinal beam gradually increases from the middle to the cross-section direction of the first assembly end, so that the front section of the cabin longitudinal beam is subjected to force to participate in deformation, energy absorption and energy transmission during impact.
其中,机舱纵梁后段沿截面方向的尺寸逐渐增大,用以分散纵梁的碰撞稳定性;机舱纵梁后段上隆起用以提升抗弯性能的加强筋。Among them, the size of the rear section of the longitudinal beam of the cabin increases gradually along the cross-sectional direction to disperse the collision stability of the longitudinal beam; the rear section of the longitudinal beam of the cabin is raised to improve the flexural performance of the ribs.
其中,机舱纵梁后段伸至前围加强底横梁中,由前围加强底横梁进行包覆。Wherein, the rear section of the longitudinal beam of the engine room extends into the reinforced bottom crossbeam of the front wall, and is covered by the bottom reinforced crossbeam of the front wall.
其中,前围加强中横梁和前围加强底横梁的纵截面分别呈三角状。Wherein, the vertical cross-sections of the front wall reinforced middle cross beam and the front wall reinforced bottom cross beam are triangular respectively.
为解决上述技术问题,本发明还公开了一种具有上述机舱框架结构的汽车。In order to solve the above-mentioned technical problems, the present invention also discloses an automobile with the above-mentioned cabin frame structure.
本发明所提供的汽车机舱框架结构、汽车,具有如下有益效果:汽车机舱框架结构,包括:前防撞梁总成;机舱纵梁总成,其包括:机舱纵梁前段和与机舱纵梁前段连为一体的机舱纵梁后段,机舱纵梁前段紧固连接有纵梁立柱,机舱纵梁前段的相对两端设有第一装配端和第二装配端,第一装配端与前防撞梁总成紧固相连;A柱总成;机舱上边梁总成,机舱上边梁总成的一端与纵梁立柱紧固相连,机舱上边梁总成的另一端与A柱总成紧固相连;以及前围加强横梁总成,其包括:前围加强中横梁和与前围加强中横梁紧固相连的前围加强底横梁,其中:第二装配端与前围加强中横梁紧固相连,前围加强底横梁与机舱纵梁后段紧固相连,其中:碰撞能量在机舱纵梁前段通过纵梁立柱和机舱上边梁总成分散至A柱总成,优化碰撞传力结构,提升小偏置碰性能;结构精简,轻量化,降低制造成本。The automobile cabin frame structure and the automobile provided by the present invention have the following beneficial effects: the automobile cabin frame structure includes: a front anti-collision beam assembly; The rear section of the longitudinal beam of the engine room is connected as a whole, and the front section of the longitudinal beam of the cabin is fastened to the column of the longitudinal beam. The opposite ends of the front section of the longitudinal beam of the cabin are provided with a first assembly end and a second assembly end, and the first assembly end is connected to the front anti-collision The beam assembly is fastened; the A-pillar assembly; the engine room upper side beam assembly, one end of the engine room upper side beam assembly is fastened to the longitudinal beam column, and the other end of the engine room upper side beam assembly is fastened to the A-pillar assembly; And the front wall reinforcement beam assembly, which includes: the front wall reinforcement center beam and the front wall reinforcement bottom beam fastened to the front wall reinforcement center beam, wherein: the second assembly end is fastened to the front wall reinforcement center beam, the front The reinforced bottom beam is firmly connected with the rear section of the longitudinal beam of the cabin, wherein: the collision energy is dispersed to the A-pillar assembly at the front section of the longitudinal beam of the cabin through the vertical beam column and the upper side beam assembly of the cabin, optimizing the collision force transmission structure and improving the small offset High impact performance; simplified structure, light weight, and reduced manufacturing costs.
附图说明Description of drawings
为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the following will briefly introduce the drawings that need to be used in the description of the embodiments or the prior art. Obviously, the accompanying drawings in the following description are only These are some embodiments of the present invention. Those skilled in the art can also obtain other drawings based on these drawings without creative work.
图1是本发明实施例的汽车机舱框架的结构示意图。Fig. 1 is a structural schematic diagram of an automobile cabin frame according to an embodiment of the present invention.
图2是本发明实施例的前防撞梁总成的结构示意图。Fig. 2 is a schematic structural view of the front anti-collision beam assembly according to the embodiment of the present invention.
图3是本发明实施例的机舱纵梁总成的结构示意图。Fig. 3 is a schematic structural view of the cabin longitudinal beam assembly according to the embodiment of the present invention.
图4是本发明实施例的机舱上边梁总成的结构示意图。Fig. 4 is a schematic structural view of the roof rail assembly of the cabin according to the embodiment of the present invention.
图5是本发明实施例的前围加强横梁总成的结构示意图。Fig. 5 is a schematic structural view of a cowl reinforcement beam assembly according to an embodiment of the present invention.
图6是本发明实施例的A柱总成的结构示意图。Fig. 6 is a schematic structural view of the A-pillar assembly of the embodiment of the present invention.
图7是本发明实施例汽车机舱框架的碰撞传力路径的第一角度的效果示意图。Fig. 7 is a schematic diagram showing the effect of the first angle of the collision force transmission path of the automobile cabin frame according to the embodiment of the present invention.
图8是本发明实施例汽车机舱框架的碰撞传力路径的第二角度的效果示意图。Fig. 8 is a schematic diagram showing the effect of the second angle of the collision force transmission path of the automobile cabin frame according to the embodiment of the present invention.
图9是本发明实施例前防撞梁总成的碰撞传力路径效果示意图。Fig. 9 is a schematic diagram showing the effect of the collision force transmission path of the front anti-collision beam assembly according to the embodiment of the present invention.
图10是本发明实施例机舱纵梁总成的机舱纵梁前段的碰撞传力路径效果示意图。Fig. 10 is a schematic diagram showing the effect of the collision force transmission path of the front section of the cabin longitudinal beam of the cabin longitudinal beam assembly according to the embodiment of the present invention.
具体实施方式Detailed ways
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有作出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.
图1-图10所示,为本发明汽车机舱框架结构的实施例一。Figures 1-10 show the first embodiment of the frame structure of the automobile cabin of the present invention.
本实施例中的汽车机舱框架结构,包括:前防撞梁总成1、机舱纵梁总成2、A柱总成3、机舱上边梁总成4以及前围加强横梁总成5。The frame structure of the automobile cabin in this embodiment includes: a front
机舱纵梁总成2包括:机舱纵梁前段21和与机舱纵梁前段21连为一体的机舱纵梁后段22,机舱纵梁前段21紧固连接有纵梁立柱23,机舱纵梁前段21的相对两端设有第一装配端21a和第二装配端21b,第一装配端21a与前防撞梁总成1紧固相连。The engine room
机舱上边梁总成4的一端与纵梁立柱23紧固相连,机舱上边梁总成4的另一端与A柱总成3紧固相连。One end of the cabin upper
前围加强横梁5包括:前围加强中横梁51和与前围加强中横梁51紧固相连的前围加强底横梁52,其中:第二装配端21b与前围加强中横梁51紧固相连,前围加强底横梁52与机舱纵梁后段22紧固相连,其中:The
机舱框架与壁障在碰撞工况中产生碰撞能量,该碰撞能量在机舱纵梁前段21通过纵梁立柱23和机舱上边梁总成4分散至A柱总成3,由机舱纵梁前段21传递至机舱纵梁后段22的碰撞能量分别通过前围加强中横梁51和前围加强底横梁52向A柱总成3及车身的另一侧分散传递,以使机舱纵梁后段区域框架的稳定。具体请参见图7-10中,碰撞传力在各零构件上的传递路径Y。The engine room frame and the barrier generate collision energy in the collision condition, and the collision energy is dispersed to the
具体实施时,前防撞梁总成1与机舱纵梁总成2为螺栓连接,其余元件均通过翻边点焊连接,满足碰撞、耐久、强度以及刚度等要求。During specific implementation, the front
前防撞梁总成1包括:前防撞梁本体11、吸能盒12及用以带动机舱纵梁前段碰撞吸能的碰撞块13;吸能盒12和碰撞块13分别紧固在前防撞梁本体11的端部,吸能盒12与第一装配端21a紧固相连,碰撞块13装设在吸能盒12的外侧。The front
本实施例中,前防撞梁本体11采用铝合金材料制成,为了更好吸能并向机舱纵梁总成2传递碰撞能量,前防撞梁本体11的横向尺寸在不影响造型及布置条件下尽量加大。吸能盒12的长度设置可以适当加长,例如终止于前副车架的前点位置,如此设置能够进一步增加吸能的空间。也就是说,前防撞梁总成1两侧长度与吸能盒12的长度设置也能够影响碰撞重叠量以及碰撞吸能效率。In this embodiment, the front
碰撞块13为挤压铝型材结构,焊接于前防撞梁本体11。碰撞块13的作用是:碰撞块13在受撞击后内收并向机舱纵梁前段21挤压,从而带动机舱纵梁总成2参与受力吸能。The
进一步的,机舱纵梁总成2包括:机舱纵梁前段21和与机舱纵梁前段21连为一体的机舱纵梁后段22,机舱纵梁前段21的相对两端设有第一装配端21a和第二装配端21b。第一装配端21a与吸能盒12紧固相连,使机舱纵梁前段21与碰撞壁障重叠,在撞击时能直接受力参与变形吸能和传递能量。Further, the
进一步的,纵梁立柱23装设在机舱纵梁前段21的第一装配端21a,第一装配端21a的底部设有前副车架装配位,前副车架6通过前副车架装配位紧固在机舱纵梁前段21。Further, the
本实施例中,前副车架装配位位于机舱纵梁前段21的正下方,该装配位安装点往车外延伸,结合前副车架6整体向车外延伸。In this embodiment, the assembly position of the front sub-frame is located directly below the
如此能够带来以下有益效果:在小偏置碰撞时,碰撞能量分别通过前副车架6和纵梁立柱23对机舱纵梁总成2进行拉拽,使碰撞能量传递到机舱纵梁总成2上。同时,机舱纵梁总成2及副车架也能够更多参与碰撞传力与吸能。This can bring the following beneficial effects: in the case of a small offset collision, the collision energy pulls the cabin
优选的,纵梁立柱23与机舱上边梁4相连的一端朝机舱框架的外后侧方向平顺过渡。Preferably, the end of the
如此设置的作用是:碰撞能量能够向上边梁总成4传递,其中:机舱纵梁总成2、纵梁立柱23、机舱上边梁4以及A柱总成3之间的连接形成环形,互相作用,使机舱前端的框架结构更稳定,从而提升碰撞传力的传力效率。The effect of such setting is: the collision energy can be transmitted to the upper
优选的,机舱纵梁前段21自其中部向第一装配端21a的截面方向的尺寸渐变增大,如此设置的作用是:使机舱纵梁总成2在小偏置碰壁障时的重叠量加大,可使机舱纵梁前段21在撞击时受力参与变形吸能和传递能量。Preferably, the size of the
优选的,机舱纵梁后段22的截面方向的尺寸逐渐增大,具体为从机舱纵梁前段21的第二装配端21b开始往后逐渐增大,呈喇叭状。如此设置的作用是:用以分散前防撞梁总成1的碰撞能量,保证纵梁整体碰撞稳定性。Preferably, the size of the cross-sectional direction of the
优选的,机舱纵梁后段22上隆起用以提升抗弯性能的加强筋220。加强筋220能够提升机舱纵梁后段22的抗弯性能。Preferably, the
进一步的,机舱上边梁总成4的一端与纵梁立柱23紧固相连,机舱上边梁总成4的另一端与A柱总成3紧固相连。Further, one end of the cabin
优选的,机舱上边梁4自与纵梁立柱相连一端向与A柱总成3相连的另一端42的截面方向的尺寸逐渐增大。如此设置的作用是:与A柱总成3实现翻边搭接,进而实现其之间稳定的三角形结构,该结构能够分别向A柱总成3上部沿顶盖边梁传递碰撞能量,以及向A柱总成3下部沿门槛分散传递碰撞能量。Preferably, the dimension of the
进一步的,前围加强横梁5包括:前围加强中横梁51和与前围加强中横梁51紧固相连的前围加强底横梁52,其中:第二装配端21b与前围加强中横梁51紧固相连,前围加强底横梁52与机舱纵梁后段22紧固相连。Further, the
具体实施时,前围加强中横梁51和前围加强底横梁52分别贯穿车身左右两侧,机舱纵梁前段21的第二装配端21b与前围加强中横梁51的位置相适配装,如此能够在小偏置碰工况中起到支撑机舱纵梁总成2的作用,保证机舱纵梁总成2的变形模式合理,并使碰撞力往A柱总成3以及车身另一侧传递。During specific implementation, the front wall reinforcement
优选的,机舱纵梁后段22伸至前围加强底横梁52中,由前围加强底横梁52进行包覆。前围加强中横梁51和前围加强底横梁52的纵截面分别呈三角状。Preferably, the
如此设置的作用是:在长续航纯电动车型中,前地板下部空间因需要提供给动力电池安装,无法像传统车型一样可以设计大截面加强梁,且能够延伸到前地板下部。因此,在本机舱框架结构中,前围加强底横梁52替代了传统车型纵梁后段的功能,贯穿前围底部,与A柱总成3和门槛连接。如此,当碰撞能量传递至机舱纵梁后段22时,前围加强底横梁52能分散碰撞能量至A柱总成3,保证整个纵梁后段区域框架稳定。The effect of such setting is: in long-endurance pure electric models, the space under the front floor needs to be provided for the installation of power batteries, so it is impossible to design large cross-section reinforcement beams like traditional models, and can extend to the lower part of the front floor. Therefore, in the frame structure of the cabin, the cowl reinforced
本实施例中的汽车机舱框架结构在具体实施时,碰撞能量在机舱纵梁前段21通过纵梁立柱23和机舱上边梁总成4分散至A柱总成3,前防撞梁总成1和机舱纵梁总成2形成前端吸能区域,使提升了机场框架前部的碰撞效率。由机舱纵梁前段21传递至机舱纵梁后段22的碰撞能量分别通过前围加强中横梁51和前围加强底横梁52向A柱总成3及车身的另一侧分散传递,以使机舱纵梁后段区域框架的稳定。参见图7-10中,碰撞传力在各零构件上的传递路径Y,进一步优化传力通道,使保证了框架后部的碰撞稳定性。When the frame structure of the automobile cabin in this embodiment is implemented, the collision energy is distributed to the
实施本发明的汽车机舱框架结构、汽车,具有如下有益效果:Carrying out the automobile cabin frame structure of the present invention, automobile, have following beneficial effect:
第一、机舱框架与壁障在碰撞工况中产生碰撞能量,该碰撞能量在机舱纵梁前段通过纵梁立柱和机舱上边梁总成分散至A柱总成,优化了前防撞梁总成和机舱纵梁总成前端吸能区域的结构,提升了框架前部碰撞效率。First, the engine room frame and the barrier generate collision energy in the collision condition, and the collision energy is dispersed to the A-pillar assembly at the front section of the engine room longitudinal beam through the longitudinal beam column and the upper side beam assembly of the cabin, optimizing the front anti-collision beam assembly The structure of the energy-absorbing area at the front end of the cabin longitudinal beam assembly improves the front collision efficiency of the frame.
第二、由机舱纵梁前段传递至机舱纵梁后段的碰撞能量分别通过前围加强中横梁和前围加强底横梁向A柱总成及车身的另一侧分散传递,在满足纯电动车型的布置空间、长续航需求的基础上,机舱框架结构有更好的轻量化表现,降低了车身制造成本。Second, the collision energy transmitted from the front section of the cabin longitudinal beam to the rear section of the cabin longitudinal beam is distributed and transmitted to the A-pillar assembly and the other side of the body through the front wall reinforced middle cross beam and the front wall reinforced bottom cross beam respectively. On the basis of the large layout space and long battery life requirements, the cabin frame structure has better lightweight performance and reduces the body manufacturing cost.
第三、结构更紧凑,更稳定,提升了小偏置碰撞性能,同时提升了车身整体刚度性能。Third, the structure is more compact and stable, which improves the small offset collision performance and improves the overall rigidity of the vehicle body.
Claims (10)
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