WO2018161696A1 - Cabin frame and vehicle having same - Google Patents

Cabin frame and vehicle having same Download PDF

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Publication number
WO2018161696A1
WO2018161696A1 PCT/CN2017/119059 CN2017119059W WO2018161696A1 WO 2018161696 A1 WO2018161696 A1 WO 2018161696A1 CN 2017119059 W CN2017119059 W CN 2017119059W WO 2018161696 A1 WO2018161696 A1 WO 2018161696A1
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WO
WIPO (PCT)
Prior art keywords
cockpit
frame
cross member
floor
top cover
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PCT/CN2017/119059
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French (fr)
Chinese (zh)
Inventor
孙彦明
段兴中
唐殿菊
李云端
罗杰
Original Assignee
北京新能源汽车股份有限公司
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Priority to CN201720217872.2 priority Critical
Priority to CN201720217872.2U priority patent/CN206579721U/en
Application filed by 北京新能源汽车股份有限公司 filed Critical 北京新能源汽车股份有限公司
Publication of WO2018161696A1 publication Critical patent/WO2018161696A1/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D25/00Superstructure or monocoque structure sub-units; Parts or details thereof not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D25/00Superstructure or monocoque structure sub-units; Parts or details thereof not otherwise provided for
    • B62D25/08Front or rear portions
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D25/00Superstructure or monocoque structure sub-units; Parts or details thereof not otherwise provided for
    • B62D25/20Floors or bottom sub-units
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D33/00Superstructures for load-carrying vehicles
    • B62D33/06Drivers' cabs

Abstract

A cabin frame and a vehicle having same. The cabin frame (200) comprises a left side roof rail (2011), a right side roof rail (2012), a front roof crossbeam (2013), a rear roof crossbeam (2014), a lower cabin frame (202), a dash panel (203), a floor panel (205), and a back panel (204). The left side roof rail (2011), the right side roof rail (2012), the front roof crossbeam (2013), and the rear roof crossbeam (2014) together form a roof frame assembly (201); the lower cabin frame (202) is fixed below the roof frame assembly (201); the dash panel (203) is fixed to the front of the lower cabin frame (202); the floor panel (205) is fixed at the bottom of the lower cabin frame (202); the back panel (204) is fixed to the back of the lower cabin frame (202). In this way, the structure of the cabin frame is modularized, the number of parts required during assembling of the cabin frame is reduced, and the assembling of the cabin frame is facilitated.

Description

驾驶舱框架和具有其的车辆Cockpit frame and vehicle with it
相关申请的交叉引用Cross-reference to related applications
本申请要求北京新能源汽车股份有限公司于2017年3月7日提交的、实用新型名称为“驾驶舱框架和具有其的车辆”的、中国专利申请号为“201720217872.2”的优先权。This application claims the priority of the Chinese patent application No. "201720217872.2" submitted by Beijing New Energy Automobile Co., Ltd. on March 7, 2017, the utility model name is "cockpit frame and vehicle with it".
技术领域Technical field
本发明涉及车辆制造领域,具体而言,涉及一种驾驶舱框架和具有该驾驶舱框架的车辆。The present invention relates to the field of vehicle manufacturing, and in particular to a cockpit frame and a vehicle having the cockpit frame.
背景技术Background technique
相关技术中,车辆的驾驶舱框架是由多个冲压成型的钣金件拼焊而成,驾驶舱框架需要制造的零件众多,进而增加了驾驶舱框架的装配难度,延长了驾驶舱框架的开发周期,且驾驶舱框架的制造成本较高。另外,该技术方案下的驾驶舱框架的重量较大,不利于车辆的轻量化布置,且钣金件耐腐蚀性差,易发生锈蚀。In the related art, the cockpit frame of the vehicle is welded by a plurality of stamped and formed sheet metal parts, and the cockpit frame needs to be manufactured with numerous parts, thereby increasing the assembly difficulty of the cockpit frame and extending the development of the cockpit frame. Cycles and the cost of manufacturing the cockpit frame is high. In addition, the weight of the cockpit frame under the technical solution is large, which is not conducive to the lightweight arrangement of the vehicle, and the sheet metal parts have poor corrosion resistance and are prone to rust.
发明内容Summary of the invention
本发明旨在至少在一定程度上解决相关技术中的技术问题之一。为此,本发明的第一方面在于提出一种至少在一定程度上能降低装配难度的驾驶舱框架。The present invention aims to solve at least one of the technical problems in the related art to some extent. To this end, a first aspect of the invention consists in proposing a cockpit frame that at least to some extent reduces the difficulty of assembly.
本发明的第二方面在于提出一种具有上述驾驶舱框架的车辆。A second aspect of the invention resides in a vehicle having the above described cockpit frame.
根据本发明第一方面所述的驾驶舱框架,包括左侧围上边梁、右侧围上边梁、顶盖前横梁、顶盖后横梁、驾驶舱下部框架、前围板、地板面板和后围板,所述顶盖前横梁连接在所述左侧围上边梁与所述右侧围上边梁的前部之间,所述顶盖后横梁连接在所述左侧围上边梁与所述右侧围上边梁的后部之间以使所述左侧围上边梁、所述右侧围上边梁、所述顶盖前横梁和所述顶盖后横梁共同形成顶盖框架总成,所述驾驶舱下部框架固定在所述顶盖框架总成的下方,所述前围板固定在所述驾驶舱下部框架的前部,所述地板面板固定在所述驾驶舱下部框架的底部,所述后围板固定在所述驾驶舱下部框架的后部。A cockpit frame according to the first aspect of the present invention includes a left side roof side rail, a right side roof side rail, a top cover front cross member, a top cover rear cross member, a cockpit lower frame, a dash panel, a floor panel, and a rear wall a top cover front beam connected between the left side roof side rail and a front side of the right side roof side rail, the top cover rear beam connected to the left side roof side rail and the right side Forming a top cover frame assembly between the rear side rails of the side rails such that the left side roof side rails, the right side roof side rails, the top cover front cross members, and the top cover rear beams together a cockpit lower frame is secured below the roof frame assembly, the dash panel is secured to a front portion of the cockpit lower frame, and the floor panel is secured to a bottom of the cockpit lower frame, A rear panel is fixed to the rear of the lower frame of the cockpit.
根据本发明第一方面所述的驾驶舱框架,使驾驶舱框架的结构模块化,减少了驾驶舱框架装配时所需的零件数量,驾驶舱框架的装配更容易。According to the cockpit frame of the first aspect of the invention, the structure of the cockpit frame is modularized, the number of parts required for assembly of the cockpit frame is reduced, and the assembly of the cockpit frame is easier.
另外,根据本发明上述的驾驶舱框架还可以具有如下附加的技术特征:Furthermore, the above described cockpit frame according to the invention may also have the following additional technical features:
优选地,所述驾驶舱下部框架包括左右间隔设置的两个A柱、左右间隔设置的两个B柱、驾驶舱左下边梁、驾驶舱右下边梁和多个驾驶舱连接横梁,所述B柱位于所述A柱的后方,所述驾驶舱左下边梁分别与左侧的所述A柱的下端与左侧的所述B柱的下端连接,所述驾驶舱右下边梁分别与右侧的所述A柱的下端与右侧的所述B柱的下端连接,所述多个驾驶舱连接横梁连接在所述驾驶舱左下边梁和所述驾驶舱右下边梁之间。Preferably, the cockpit lower frame comprises two A-pillars arranged at right and left intervals, two B-pillars arranged at right and left, a lower left side sill of the cockpit, a right lower side sill of the cockpit and a plurality of cockpit connecting beams, the B a column is located behind the A-pillar, and the left lower side sill of the cockpit is respectively connected to a lower end of the A-pillar on the left side and a lower end of the B-pillar on the left side, and the right lower side beam of the cockpit is respectively opposite to the right side The lower end of the A-pillar is connected to the lower end of the B-pillar on the right side, and the plurality of cockpit connecting beams are connected between the left lower side sill of the cockpit and the right lower side sill of the cockpit.
进一步地,所述驾驶舱连接横梁包括驾驶舱前横梁、驾驶舱后横梁和驾驶舱中间横梁,所述驾驶舱前横梁分别与所述驾驶舱左下边梁的前端以及所述驾驶舱右下边梁的前端连接,所述驾驶舱后横梁分别与所述驾驶舱左下边梁的后端以及所述驾驶舱右下边梁的后端连接,所述驾驶舱中间横梁位于所述驾驶舱前横梁和所述驾驶舱后横梁之间。Further, the cockpit connecting beam comprises a cockpit front cross beam, a cockpit rear cross beam and a cockpit middle cross beam, respectively, the front cockpit cross beam and the front left side sill of the cockpit and the right lower side sill of the cockpit a front end connection, the cockpit rear cross member being respectively connected to a rear end of the cockpit left side sill and a rear end of the cockpit right side sill, the cockpit middle cross member being located at the front cockpit of the cockpit Between the cockpit rear beams.
更进一步地,所述驾驶舱下部框架还包括驾驶舱连接纵梁,所述驾驶舱连接纵梁沿前后方向延伸且连接在所述驾驶舱前横梁和所述驾驶舱中间横梁之间,所述驾驶舱连接纵梁位于所述驾驶舱左下边梁和所述驾驶舱右下边梁之间。Further, the cockpit lower frame further includes a cockpit connecting stringer, the cockpit connecting stringer extending in a front-rear direction and connected between the cockpit front cross member and the cockpit intermediate beam, A cockpit connection stringer is located between the left lower side sill of the cockpit and the lower right side sill of the cockpit.
更进一步地,所述驾驶舱下部框架还包括:两个加强件,两个所述加强件分别位于所述驾驶舱后横梁与所述驾驶舱左下边梁的连接处以及所述驾驶舱后横梁与所述驾驶舱右下边梁的连接处。Further, the cockpit lower frame further includes: two reinforcing members, the two reinforcing members are respectively located at a joint of the cockpit rear cross member and the left lower side sill of the cockpit, and the cockpit rear cross member The connection to the right lower side sill of the cockpit.
更进一步地,所述地板面板包括左前地板、右前地板和后地板,所述左前地板安装在所述驾驶舱下部框架的底部的左前部,所述右前地板安装在所述驾驶舱下部框架的底部的右前部,所述后地板安装在所述驾驶舱下部框架的底部的后部。Further, the floor panel includes a left front floor, a right front floor, and a rear floor, the left front floor is mounted at a left front portion of a bottom of the cockpit lower frame, and the right front floor is installed at a bottom of the cockpit lower frame On the right front portion, the rear floor is mounted at the rear of the bottom of the lower frame of the cockpit.
更进一步地,所述左前地板安装在所述驾驶舱连接纵梁、所述驾驶舱前横梁、所述驾驶舱左下边梁和所述驾驶舱中间横梁限制的区域内,所述右前地板安装在所述驾驶舱连接纵梁、所述驾驶舱前横梁、所述驾驶舱右下边梁和所述驾驶舱中间横梁限制的区域内,所述后地板安装在所述驾驶舱右下边梁、所述驾驶舱后横梁、所述驾驶舱左下边梁和所述驾驶舱中间横梁限制的区域内。Further, the left front floor is installed in an area of the cockpit connecting stringer, the cockpit front cross member, the cockpit left lower side rail and the cockpit intermediate cross member, and the right front floor is installed at The cockpit connection stringer, the cockpit front cross member, the cockpit right lower side rail, and the cockpit intermediate cross member are constrained, the rear floor is mounted to the cockpit right lower side rail, the The cockpit rear cross member, the left underside of the cockpit, and the area of the cockpit intermediate beam are restricted.
可选地,所述驾驶舱框架为轻质合金框架。Optionally, the cockpit frame is a lightweight alloy frame.
进一步地,所述驾驶舱框架为铝合金框架。Further, the cockpit frame is an aluminum alloy frame.
根据本发明第二方面所述的车辆,设有如本发明第一方面所述的驾驶舱框架。A vehicle according to a second aspect of the invention is provided with a cockpit frame according to the first aspect of the invention.
根据本发明第二方面所述的车辆,降低了整车的装配难度,提高了车辆的装配节拍。According to the vehicle of the second aspect of the present invention, the assembly difficulty of the entire vehicle is reduced, and the assembly tempo of the vehicle is improved.
附图说明DRAWINGS
图1是本发明实施例的驾驶舱框架的结构示意图;1 is a schematic structural view of a cockpit frame according to an embodiment of the present invention;
图2是本发明实施例的驾驶舱下部框架的结构示意图;2 is a schematic structural view of a lower frame of a cockpit according to an embodiment of the present invention;
图3是本发明实施例的前围板的结构示意图;3 is a schematic structural view of a dash panel according to an embodiment of the present invention;
图4是本发明实施例的后围板的结构示意图;4 is a schematic structural view of a rear panel according to an embodiment of the present invention;
图5是本发明实施例的地板面板的结构示意图;Figure 5 is a schematic structural view of a floor panel according to an embodiment of the present invention;
图6是本发明实施例的左侧围上边梁的结构示意图;6 is a schematic structural view of a left side side edge beam according to an embodiment of the present invention;
图7是本发明实施例的顶盖前横梁的结构示意图;7 is a schematic structural view of a front cover cross member according to an embodiment of the present invention;
图8是本发明实施例的顶盖后横梁的结构示意图。Fig. 8 is a structural schematic view of a rear cover cross member according to an embodiment of the present invention.
附图标记:Reference mark:
驾驶舱框架200,顶盖框架总成201,左侧围上边梁2011,左侧围上边梁本体20111,左后立梁20112,A柱连接板20113,左连接板20114,右侧围上边梁2012,顶盖前横梁2013,顶盖前横梁本体20131,前横梁连接板20132,顶盖后横梁2014,顶盖后横梁本体20141,后横梁连接板20142,驾驶舱下部框架202,A柱2021,B柱2022,驾驶舱左下边梁2023,驾驶舱右下边梁2024,驾驶舱前横梁2025,驾驶舱中间横梁2026,驾驶舱后横梁2027,驾驶舱连接纵梁2028,加强件2029,前围板203,前围板本体2031,前围板上横梁2032,前围板安装支架2033,后围板204,后围板本体2041,后围上板2042,地板面板205,右前地板2051,左前地板2052,后地板2053。Cockpit frame 200, roof frame assembly 201, left side rails 2011, left side rail side body 20111, left rear beam 20112, A-pillar connection panel 20113, left connecting panel 20114, right side railings 2012 Top cover front beam 2013, top cover front beam body 20131, front beam connection plate 20132, top cover rear beam 2014, top cover rear beam body 20141, rear beam connection plate 20142, cockpit lower frame 202, A-pillar 2021, B Column 2022, cockpit lower left side rail 2023, cockpit right lower side rail 2024, cockpit front cross member 2025, cockpit middle cross member 2026, cockpit rear cross member 2027, cockpit connection stringer 2028, reinforcement member 2029, dash panel 203 The front panel body 2031, the front panel cross member 2032, the dash panel mounting bracket 2033, the rear panel 204, the rear panel body 2041, the rear panel upper panel 2042, the floor panel 205, the right front floor 2051, and the left front floor 2052, Rear floor 2053.
具体实施方式detailed description
下面详细描述本发明的实施例,所述实施例的示例在附图中示出,其中自 始至终相同或类似的标号表示相同或类似的元件或具有相同或类似功能的元件。下面通过参考附图描述的实施例是示例性的,旨在用于解释本发明,而不能理解为对本发明的限制。The embodiments of the present invention are described in detail below, and the examples of the embodiments are illustrated in the drawings, wherein the same or similar reference numerals are used to refer to the same or similar elements or elements having the same or similar functions. The embodiments described below with reference to the drawings are intended to be illustrative of the invention and are not to be construed as limiting.
在本发明的描述中,需要理解的是,术语“上”、“下”、“前”、“后”、“左”、“右”、“顶”、“底”、“内”、“外”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本发明和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本发明的限制。In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "back", "left", "right", "top", "bottom", "inner", " The orientation or positional relationship of the indications is based on the orientation or positional relationship shown in the drawings, and is merely for the convenience of describing the present invention and the simplified description, and does not indicate or imply that the device or component referred to has a specific orientation. The specific orientation and operation are not to be construed as limiting the invention.
此外,术语“第一”、“第二”仅用于描述目的,而不能理解为指示或暗示相对重要性或者隐含指明所指示的技术特征的数量。由此,限定有“第一”、“第二”的特征可以明示或者隐含地包括一个或者更多个该特征。在本发明的描述中,“多个”的含义是至少两个,例如两个,三个等,除非另有明确具体的限定。Moreover, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, features defining "first" and "second" may include one or more of the features either explicitly or implicitly. In the description of the present invention, the meaning of "a plurality" is at least two, such as two, three, etc., unless specifically defined otherwise.
在本发明中,除非另有明确的规定和限定,术语“安装”、“相连”、“连接”、“固定”等术语应做广义理解,例如,可以是固定连接,也可以是可拆卸连接,或成一体;可以是机械连接,也可以是电连接或可以互相通讯;可以是直接相连,也可以通过中间媒介间接相连,可以是两个元件内部的连通或两个元件的相互作用关系。对于本领域的普通技术人员而言,可以根据具体情况理解上述术语在本发明中的具体含义。In the present invention, the terms "installation", "connected", "connected", "fixed" and the like shall be understood broadly, and may be either a fixed connection or a detachable connection, unless explicitly stated and defined otherwise. , or integrated; can be mechanical connection, can also be electrically connected or can communicate with each other; can be directly connected, or can be indirectly connected through an intermediate medium, can be the internal communication of two elements or the interaction of two elements. For those skilled in the art, the specific meanings of the above terms in the present invention can be understood on a case-by-case basis.
在本发明中,除非另有明确的规定和限定,第一特征在第二特征之“上”或之“下”可以包括第一和第二特征直接接触,也可以包括第一和第二特征不是直接接触而是通过它们之间的另外的特征接触。而且,第一特征在第二特征“之上”、“上方”和“上面”包括第一特征在第二特征正上方和斜上方,或仅 仅表示第一特征水平高度高于第二特征。第一特征在第二特征“之下”、“下方”和“下面”包括第一特征在第二特征正下方和斜下方,或仅仅表示第一特征水平高度小于第二特征。In the present invention, the first feature "on" or "under" the second feature may include direct contact of the first and second features, and may also include first and second features, unless otherwise specifically defined and defined. It is not in direct contact but through additional features between them. Moreover, the first feature "above", "above" and "above" the second feature includes the first feature directly above and above the second feature, or only the first feature level is higher than the second feature. The first feature "below", "below" and "below" the second feature includes the first feature directly below and below the second feature, or merely the first feature level being less than the second feature.
下面结合附图并参考具体实施例描述本发明。The invention is described below in conjunction with the specific embodiments in conjunction with the drawings.
首先结合图1-图8描述本发明实施例的驾驶舱框架200。A cockpit frame 200 of an embodiment of the present invention will first be described with reference to Figs.
如图1-图8所示,本发明实施例的驾驶舱框架200可以包括左侧围上边梁2011、右侧围上边梁2012、顶盖前横梁2013、顶盖后横梁2014、驾驶舱下部框架202、前围板203、地板面板205和后围板204。As shown in FIGS. 1-8, the cockpit frame 200 of the embodiment of the present invention may include a left side roof side rail 2011, a right side roof side rail 2012, a top cover front beam 2013, a top cover rear beam 2014, and a cockpit lower frame. 202, a dash panel 203, a floor panel 205, and a back panel 204.
如图1所示,顶盖前横梁2013可以连接在左侧围上边梁2011与右侧围上边梁2012的前部之间,顶盖后横梁2014可以连接在左侧围上边梁2011与右侧围上边梁2012的后部之间,由此左侧围上边梁2011、右侧围上边梁2012、顶盖前横梁2013和顶盖后横梁2014可以共同形成顶盖框架总成201,车辆的顶盖可以安装在左侧围上边梁2011、右侧围上边梁2012、顶盖前横梁2013和顶盖后横梁2014围成的框架内。As shown in Fig. 1, the top cover front cross member 2013 can be connected between the left side top side beam 2011 and the right side top side beam 2012, and the top cover rear cross member 2014 can be connected to the left side top side beam 2011 and the right side. Between the rear portions of the side beams 2012, the left side rails 2011, the right side rails 2012, the roof front beams 2013 and the roof rear beams 2014 may collectively form the roof frame assembly 201, the roof of the vehicle The cover may be mounted in a frame surrounded by the left side rails 2011, the right side rails 2012, the top front rails 2013, and the top back beams 2014.
如图1所示,驾驶舱下部框架202可以固定在顶盖框架总成201的下方,前围板203可以固定在驾驶舱下部框架202的前部,前围板203可以遮住驾驶舱下部框架202的前部,地板面板205可以固定在驾驶舱下部框架202的底部,地板面板205可以遮住驾驶舱下部框架202的底部,后围板204可以遮住驾驶舱下部框架202的后部。As shown in Figure 1, the cockpit lower frame 202 can be secured below the roof frame assembly 201, the dash panel 203 can be secured to the front of the cockpit lower frame 202, and the dash panel 203 can cover the cockpit lower frame At the front of the 202, the floor panel 205 can be secured to the bottom of the cockpit lower frame 202, the floor panel 205 can cover the bottom of the cockpit lower frame 202, and the back panel 204 can cover the rear of the cockpit lower frame 202.
由此,驾驶舱框架200可以包括左侧围上边梁2011、右侧围上边梁2012、顶盖前横梁2013、顶盖后横梁2014、驾驶舱下部框架202、前围板203、地板面板205和后围板204八个模块,人员在装配驾驶舱框架200前,可以预先将不同截面的型材通过焊接或铆接制成左侧围上边梁2011、右侧围上边梁2012、 顶盖前横梁2013、顶盖后横梁2014、驾驶舱下部框架202、前围板203、地板面板205和后围板204。Thus, the cockpit frame 200 may include a left side rail side beam 2011, a right side roof side rail 2012, a top cover front cross member 2013, a top cover rear cross member 2014, a cockpit lower frame 202, a dash panel 203, a floor panel 205, and The rear panel 204 has eight modules. Before assembling the cockpit frame 200, the profiles of different sections can be pre-formed by welding or riveting into the left side rails 2011, the right side rails 2012, the top front beams 2013, The top cover rear cross member 2014, the cockpit lower frame 202, the dash panel 203, the floor panel 205, and the rear panel 204.
人员在装配驾驶舱框架200时,可以直接将左侧围上边梁2011、右侧围上边梁2012、顶盖前横梁2013、顶盖后横梁2014、驾驶舱下部框架202、前围板203、地板面板205和后围板204焊接或铆接在一起,进而完成驾驶舱框架200的装配。相对于传统的驾驶舱框架,减少了驾驶舱框架200装配时所需的零件数量,节约了驾驶舱框架200的装配时间,驾驶舱框架200的装配更容易。When assembling the cockpit frame 200, the personnel can directly place the left side rail side beam 2011, the right side roof side rail 2012, the top cover front beam 2013, the top cover rear beam 2014, the cockpit lower frame 202, the dash panel 203, and the floor. The panel 205 and the back panel 204 are welded or riveted together to complete the assembly of the cockpit frame 200. Compared to the conventional cockpit frame, the number of parts required for assembly of the cockpit frame 200 is reduced, saving the assembly time of the cockpit frame 200, and the assembly of the cockpit frame 200 is easier.
根据本发明实施例的驾驶舱框架200,通过设置左侧围上边梁2011、右侧围上边梁2012、顶盖前横梁2013、顶盖后横梁2014、驾驶舱下部框架202、前围板203、地板面板205和后围板204,使驾驶舱结构模块化,在装配形成车身驾驶舱框架200时只需将上述的八个结构模块进行装配,减少了装配工序和装配时所需的零件数量,节约了驾驶舱框架200的装配时间,降低驾驶舱框架200的开发成本,驾驶舱框架200的装配更容易。According to the cockpit frame 200 of the embodiment of the present invention, the left side roof side rail 2011, the right side roof side rail 2012, the top cover front cross member 2013, the top cover rear cross member 2014, the cockpit lower frame 202, the dash panel 203, The floor panel 205 and the rear panel 204 modularize the cockpit structure, and only need to assemble the above eight structural modules when assembling the body cockpit frame 200, thereby reducing the number of parts required for the assembly process and assembly. The assembly time of the cockpit frame 200 is saved, the development cost of the cockpit frame 200 is reduced, and the assembly of the cockpit frame 200 is easier.
优选地,如图2所示,驾驶舱下部框架202可以包括左右间隔设置的两个A柱2021、左右间隔设置的两个B柱2022、驾驶舱左下边梁2023、驾驶舱右下边梁2024和多个驾驶舱连接横梁,驾驶舱下部框架202可以由两个A柱2021、两个B柱2022、驾驶舱左下边梁2023、驾驶舱右下边梁2024和多个驾驶舱连接横梁彼此拼焊或铆接制成。Preferably, as shown in FIG. 2, the cockpit lower frame 202 may include two A-pillars 2021 spaced apart from left and right, two B-pillars 2022 spaced apart from left and right, a cockpit lower left side rail 2023, a cockpit right lower side rail 2024, and a plurality of cockpit connecting beams, the cockpit lower frame 202 may be welded to each other by two A-pillars 2021, two B-pillars 2022, a cockpit lower left side rail 2023, a cockpit right side sill 2024, and a plurality of cockpit connecting beams Riveted.
如图2所示,左侧的B柱2022可以位于左侧A柱2021的后方,右侧的B柱2022可以位于右侧A柱2021的后方,驾驶舱左下边梁2023可以分别与左侧的A柱2021的下端与左侧的B柱2022的下端连接,驾驶舱右下边梁2024可以分别与右侧的A柱2021的下端与右侧的B柱2022的下端连接,多个驾驶 舱连接横梁可以连接在驾驶舱左下边梁2023和驾驶舱右下边梁2024之间,从而驾驶舱下部框架202整体结构更加牢固。As shown in FIG. 2, the left B-pillar 2022 may be located behind the left A-pillar 2021, and the right B-pillar 2022 may be located behind the right A-pillar 2021, and the cockpit lower left side rail 2023 may be respectively associated with the left side. The lower end of the A-pillar 2021 is connected to the lower end of the left B-pillar 2022, and the cockpit right lower side rail 2024 can be respectively connected to the lower end of the right A-pillar 2021 and the lower end of the right B-pillar 2022, and the plurality of cockpit connecting beams It can be connected between the cockpit lower left side rail 2023 and the cockpit right lower side rail 2024, so that the overall structure of the cockpit lower frame 202 is more secure.
在一些具体的实施例中,如图2所示,驾驶舱连接横梁可以包括驾驶舱前横梁2025、驾驶舱后横梁2027和驾驶舱中间横梁2026,驾驶舱前横梁2025可以分别与驾驶舱左下边梁2023的前端以及驾驶舱右下边梁2024的前端连接,驾驶舱后横梁2027可以分别与驾驶舱左下边梁2023的后端以及驾驶舱右下边梁2024的后端连接。驾驶舱前横梁2025和驾驶舱后横梁2027可以互相平行。In some specific embodiments, as shown in FIG. 2, the cockpit connecting beam may include a cockpit front cross member 2025, a cockpit rear cross member 2027, and a cockpit middle cross member 2026, and the cockpit front cross member 2025 may be respectively associated with the lower left side of the cockpit. The front end of the beam 2023 and the front end of the cockpit right side rail 2024 are connected, and the cockpit rear cross member 2027 can be coupled to the rear end of the cockpit lower left side rail 2023 and the rear end of the cockpit right side rail 2024, respectively. The cockpit front cross member 2025 and the cockpit rear cross member 2027 can be parallel to each other.
可以理解的是,驾驶舱下部框架202的前端可以由两个A柱2021和驾驶舱前横梁2025构成,驾驶舱下部框架202的后端可以由两个B柱2022和驾驶舱后横梁2027构成,驾驶舱中间横梁2026可以位于驾驶舱前横梁2025和驾驶舱后横梁2027之间,驾驶舱中间横梁2026可以使驾驶舱下部框架202整体结构更加牢固。It can be understood that the front end of the cockpit lower frame 202 can be composed of two A-pillars 2021 and a cockpit front cross member 2025, and the rear end of the cockpit lower frame 202 can be composed of two B-pillars 2022 and a cockpit rear cross member 2027. The cockpit intermediate cross member 2026 can be located between the cockpit front cross member 2025 and the cockpit rear cross member 2027, and the cockpit intermediate cross member 2026 can provide a more robust overall structure of the cockpit lower frame 202.
在一些更加具体的实施例中,如图2所示,驾驶舱下部框架202还可以包括驾驶舱连接纵梁2028,驾驶舱连接纵梁2028可以沿前后方向延伸,且驾驶舱连接纵梁2028可以连接在驾驶舱前横梁2025和驾驶舱中间横梁2026之间。In some more specific embodiments, as shown in FIG. 2, the cockpit lower frame 202 can also include a cockpit connection stringer 2028 that can extend in the fore-and-aft direction and that the cockpit connection stringer 2028 can It is connected between the cockpit front cross member 2025 and the cockpit intermediate cross member 2026.
如图2所示,在左右方向上,驾驶舱连接纵梁2028可以位于驾驶舱左下边梁2023和驾驶舱右下边梁2024之间并优选处在中间位置,驾驶舱连接纵梁2028可以与驾驶舱前横梁2025以及驾驶舱后横梁2027互相平行,由此驾驶舱连接纵梁2028可以进一步增强驾驶舱下部框架202整体的结构强度。As shown in FIG. 2, in the left-right direction, the cockpit connecting stringer 2028 can be located between the cockpit lower left side rail 2023 and the cockpit right lower side rail 2024 and preferably in an intermediate position, and the cockpit connecting stringer 2028 can be driven The cabin front cross member 2025 and the cockpit rear cross member 2027 are parallel to each other, whereby the cockpit connection stringer 2028 can further enhance the structural strength of the overall cockpit lower frame 202.
在一些更加具体的实施例中,如图2所示,驾驶舱下部框架202还可以包括两个加强件2029,两个加强件2029可以分别位于驾驶舱后横梁2027与驾驶舱左下边梁2023的连接处以及驾驶舱后横梁2027与驾驶舱右下边梁2024 的连接处,两个加强件2029均可以焊接或铆接在驾驶舱下部框架202的内侧。In some more specific embodiments, as shown in FIG. 2, the cockpit lower frame 202 can also include two stiffeners 2029, which can be located in the cockpit rear cross member 2027 and the cockpit lower left side rail 2023, respectively. At the junction and the junction of the cockpit rear cross member 2027 and the cockpit right lower side rail 2024, both stiffeners 2029 can be welded or riveted to the inside of the cockpit lower frame 202.
由此,位于左侧的加强件2029可以增强驾驶舱后横梁2027与驾驶舱左下边梁2023的连接强度,位于右侧的加强件2029可以增强驾驶舱后横梁2027与驾驶舱右下边梁2024的连接强度,进而增强了驾驶舱下部框架202整体的结构强度。Thus, the reinforcement member 2029 on the left side can enhance the strength of the connection between the cockpit rear cross member 2027 and the cockpit lower left side rail 2023, and the reinforcement member 2029 on the right side can reinforce the cockpit rear cross member 2027 and the cockpit right lower side rail 2024. The strength of the connection, in turn, enhances the structural strength of the overall cockpit lower frame 202.
在一些更加具体的实施例中,如图5所示,地板面板205可以包括左前地板2052、右前地板2051和后地板2053,左前地板2052可以安装在驾驶舱下部框架202的底部的左前部,右前地板2051可以安装在驾驶舱下部框架202的底部的右前部,后地板2053可以安装在驾驶舱下部框架202的底部的后部。In some more specific embodiments, as shown in FIG. 5, the floor panel 205 can include a left front floor 2052, a right front floor 2051, and a rear floor 2053, and the left front floor 2052 can be mounted to the left front of the bottom of the cockpit lower frame 202, right front The floor 2051 can be mounted to the right front of the bottom of the cockpit lower frame 202, and the rear floor 2053 can be mounted to the rear of the bottom of the cockpit lower frame 202.
更加具体地,如图1、图2和图5所示,左前地板2052可以安装在驾驶舱连接纵梁2028、驾驶舱前横梁2025、驾驶舱左下边梁2023和驾驶舱中间横梁2026限制的区域内,右前地板2051可以安装在驾驶舱连接纵梁2028、驾驶舱前横梁2025、驾驶舱右下边梁2024和驾驶舱中间横梁2026限制的区域内,后地板2053可以安装在驾驶舱右下边梁2024、驾驶舱后横梁2027、驾驶舱左下边梁2023和驾驶舱中间横梁2026限制的区域内。More specifically, as shown in FIGS. 1, 2, and 5, the left front floor 2052 can be mounted to the cockpit connecting stringer 2028, the cockpit front cross member 2025, the cockpit lower left side rail 2023, and the cockpit intermediate cross member 2026. Inside, the right front floor 2051 can be mounted in the area bounded by the cockpit connection stringer 2028, the cockpit front cross member 2025, the cockpit right lower side rail 2024, and the cockpit middle cross member 2026, and the rear floor 2053 can be mounted to the cockpit right lower side rail 2024. The cockpit rear cross member 2027, the cockpit lower left side rail 2023, and the cockpit intermediate cross member 2026 are constrained.
由此,地板面板205可以避让驾驶舱连接纵梁2028和驾驶舱中间横梁2026,方便地板面板205安装在驾驶舱下部框架202底部。Thus, the floor panel 205 can avoid the cockpit connection stringer 2028 and the cockpit intermediate cross member 2026, allowing the floor panel 205 to be mounted to the bottom of the cockpit lower frame 202.
在一些具体的实施例中,如图3所示,前围板203可以包括前围板本体2031,前围板本体2031的上端可以设有前围板上横梁2032,前围板上横梁2032的左右两端可以分别与左右两侧的B柱2022连接,从而增强前围板203的结构强度,前围板本体2031上还可以设有前围板安装支架2033,前围板安装支架2033可以安装车辆的仪表板以及转向系统。In some specific embodiments, as shown in FIG. 3, the dash panel 203 may include a dash panel body 2031. The upper end of the dash panel body 2031 may be provided with a front panel cross member 2032 and a front panel cross member 2032. The left and right ends can be respectively connected with the B pillars 2022 on the left and right sides to enhance the structural strength of the dash panel 203. The dash panel mounting bracket 2033 can also be provided on the dash panel body 2031, and the dash panel mounting bracket 2033 can be installed. The dashboard of the vehicle and the steering system.
在一些具体的实施例中,如图4所示,后围板204可以包括后围板本体 2041,后围板本体2041的上端可以设有向后延伸的后围上板2042,后围上板2042可以为车辆的后挡风玻璃提供安装点。在一些其他的实施例中,后围上板2042还也可以设有安装支架以安装车辆的座椅靠背等部件。In some specific embodiments, as shown in FIG. 4, the rear panel 204 may include a rear panel body 2041. The upper end of the rear panel body 2041 may be provided with a rearward extending upper panel 2042 extending rearward. The 2042 provides a mounting point for the rear windshield of the vehicle. In some other embodiments, the rear upper panel 2042 may also be provided with mounting brackets to mount components such as the seat back of the vehicle.
在一些具体的实施例中,如图6所示,左侧围上边梁2011可以包括向下弯曲的左侧围上边梁本体20111,左侧围上边梁本体20111的后端可以设有左后立梁20112,左后立梁20112可以支撑左侧围上边梁本体20111,左后立梁20112的底部可以与左侧B柱2022的上端面相连,左侧围上边梁本体20111的前端可以设有A柱连接板20113,左侧围上边梁本体20111的A柱连接板20113可以与左侧A柱2021的顶部相连,左侧围上边梁本体20111上可以向右设有用于连接顶盖前横梁2013的左连接板20114。In some specific embodiments, as shown in FIG. 6, the left side roof side beam 2011 may include a downwardly curved left side roof side body 20111, and the left side of the left side beam body 20111 may be provided with a left rear side. The beam 20112, the left rear standing beam 20112 can support the left side roof side beam body 20111, the bottom of the left rear side beam 20112 can be connected with the upper end surface of the left side B column 2022, and the front end of the left side side beam body 20111 can be provided with A The column connecting plate 20113, the A-pillar connecting plate 20113 of the left side roof beam body 20111 may be connected to the top of the left A-pillar 2021, and the left side surrounding-side beam body 20111 may be provided to the right for connecting the top cover front beam 2013. Left connection plate 20114.
左侧围上边梁2011与右侧围上边梁2012的结构可以沿车辆的纵向对称线轴对称。The structure of the left side rails 2011 and the right side rails 2012 may be axisymmetric along the longitudinal symmetry of the vehicle.
换言之,右侧围上边梁2012可以包括向下弯曲的右侧围上边梁本体,右侧围上边梁本体的后端可以设有右后立梁,右后立梁可以支撑右侧围上边梁本体,右后立梁的底部可以与右侧B柱2022的上端面相连,右侧围上边梁本体的前端可以设有A柱连接板,右侧围上边梁本体的A柱连接板可以与右侧A柱2021的顶部相连,右侧围上边梁本体上可以向左设有用于连接顶盖前横梁2013的右连接板。In other words, the right side top side beam 2012 may include a right side surrounding side beam body that is curved downward, the right rear side beam body may have a right rear side beam at the rear end, and the right rear side beam may support the right side top side beam body. The bottom of the right rear standing beam may be connected to the upper end surface of the right B-pillar 2022, and the front end of the right side rail beam body may be provided with an A-pillar connecting plate, and the A-pillar connecting plate of the right side surrounding side beam body may be connected to the right side. The tops of the A-pillars 2021 are connected, and the right side of the side rails can be provided with a right connecting plate for connecting the top front beams 2013 to the left.
在一些具体的实施例中,如图7所示,顶盖前横梁2013可以包括左右延伸的顶盖前横梁本体20131,顶盖前横梁本体20131的左右两端可以分别设有前横梁连接板20132,顶盖前横梁2013可以通过前横梁连接板20132分别与左侧围上边梁2011以及右侧围上边梁2012连接。可以理解的是,在一些具体的实施例中,顶盖前横梁本体20131的左端的前横梁连接板20132可以与左连 接板20114连接,顶盖前横梁本体20131的右端的前横梁连接板20132可以与右连接板连接。In some specific embodiments, as shown in FIG. 7 , the top cover front beam 2013 may include a top cover front beam body 20131 extending left and right, and the left and right ends of the top cover front beam body 20131 may be respectively provided with a front beam connection plate 20132 The top cover front beam 2013 can be connected to the left side roof side rails 2011 and the right side roof side rails 2012 through the front beam connecting plates 20132, respectively. It can be understood that, in some specific embodiments, the front beam connecting plate 20132 of the left end of the top front beam body 20131 can be connected with the left connecting plate 20114, and the front beam connecting plate 20132 of the right end of the front cover front beam body 20131 can be Connect to the right connection plate.
在一些具体的实施例中,如图8所示,顶盖后横梁2014可以包括左右延伸的顶盖后横梁本体20141,顶盖后横梁本体20141的左部和右部分别可以设有向后延伸的后横梁连接板20142,后横梁连接板20142可以安装车辆的后挡风玻璃。In some specific embodiments, as shown in FIG. 8, the top cover rear cross member 2014 may include a top cover rear cross member body 20141 extending left and right, and the left and right portions of the top cover rear cross member body 20141 may be respectively extended rearward. The rear cross member connection plate 20142, the rear cross member connection plate 20142 can be installed with the rear windshield of the vehicle.
在一些可选的实施例中,驾驶舱框架200均可以为轻质合金框架,即左侧围上边梁2011、右侧围上边梁2012、顶盖前横梁2013、顶盖后横梁2014、驾驶舱下部框架202、前围板203、地板面板205和后围板204均可以为轻质合金件,由此可以在车辆保持较强的刚度和防撞性能下减轻驾驶舱框架200的重量,进而减轻了整车重量。In some alternative embodiments, the cockpit frame 200 may each be a lightweight alloy frame, ie, the left side rails 2011, the right side rails 2012, the roof front beams 2013, the roof back beams 2014, the cockpit The lower frame 202, the dash panel 203, the floor panel 205, and the back panel 204 may each be a lightweight alloy member, thereby reducing the weight of the cockpit frame 200 while the vehicle maintains strong rigidity and crashworthiness, thereby reducing The weight of the whole vehicle.
在一些具体的实施例中,驾驶舱框架200可以为铝合金框架,即左侧围上边梁2011、右侧围上边梁2012、顶盖前横梁2013、顶盖后横梁2014、驾驶舱下部框架202、前围板203、地板面板205和后围板204均可以为铝合金件,从而左侧围上边梁2011、右侧围上边梁2012、顶盖前横梁2013、顶盖后横梁2014、驾驶舱下部框架202、前围板203、地板面板205和后围板204均可以经不同截面的铝合金型材挤压成型后,再通过焊接或铆接制成。由此驾驶舱框架200造价便宜,成型简单,且具有良好的防腐性能。In some specific embodiments, the cockpit frame 200 can be an aluminum alloy frame, ie, a left side roof rail 2011, a right side roof rail 2012, a roof front beam 2013, a roof rear beam 2014, a cockpit lower frame 202, The dash panel 203, the floor panel 205 and the rear panel 204 may each be an aluminum alloy member, so that the left side rails 2011, the right side rails 2012, the roof front beams 2013, the roof rear beams 2014, the cockpit The lower frame 202, the dash panel 203, the floor panel 205, and the back panel 204 may be extruded through aluminum alloy profiles of different cross sections, and then formed by welding or riveting. The cockpit frame 200 thus is inexpensive to manufacture, simple to mold, and has good corrosion resistance.
下面描述本发明实施例的车辆。The vehicle of the embodiment of the present invention will be described below.
本发明实施例的车辆设有如本发明上述任一种实施例的驾驶舱框架200。A vehicle according to an embodiment of the present invention is provided with a cockpit frame 200 according to any of the above embodiments of the present invention.
根据本发明实施例的车辆,通过设置驾驶舱框架200,降低了整车的装配难度,提高了车辆的装配节拍。According to the vehicle of the embodiment of the present invention, by providing the cockpit frame 200, the assembly difficulty of the entire vehicle is reduced, and the assembly tempo of the vehicle is improved.
在本说明书的描述中,参考术语“一个实施例”、“一些实施例”、“示例”、 “具体示例”、或“一些示例”等的描述意指结合该实施例或示例描述的具体特征、结构、材料或者特点包含于本发明的至少一个实施例或示例中。在本说明书中,对上述术语的示意性表述不必须针对的是相同的实施例或示例。而且,描述的具体特征、结构、材料或者特点可以在任何的一个或多个实施例或示例中以合适的方式结合。此外,本领域的技术人员可以将本说明书中描述的不同实施例或示例进行接合和组合。In the description of the present specification, the description with reference to the terms "one embodiment", "some embodiments", "example", "specific example", or "some examples" and the like means a specific feature described in connection with the embodiment or example. A structure, material or feature is included in at least one embodiment or example of the invention. In the present specification, the schematic representation of the above terms is not necessarily directed to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in a suitable manner in any one or more embodiments or examples. Further, various embodiments or examples described in this specification can be joined and combined by those skilled in the art.
尽管上面已经示出和描述了本发明的实施例,可以理解的是,上述实施例是示例性的,不能理解为对本发明的限制,本领域的普通技术人员在本发明的范围内可以对上述实施例进行变化、修改、替换和变型。Although the embodiments of the present invention have been shown and described, it is understood that the above-described embodiments are illustrative and are not to be construed as limiting the scope of the invention. The embodiments are subject to variations, modifications, substitutions and variations.

Claims (10)

  1. 一种驾驶舱框架,其特征在于,所述驾驶舱框架包括:A cockpit frame, characterized in that the cockpit frame comprises:
    左侧围上边梁、右侧围上边梁、顶盖前横梁、顶盖后横梁,所述顶盖前横梁连接在所述左侧围上边梁与所述右侧围上边梁的前部之间,所述顶盖后横梁连接在所述左侧围上边梁与所述右侧围上边梁的后部之间以使所述左侧围上边梁、所述右侧围上边梁、所述顶盖前横梁和所述顶盖后横梁共同形成顶盖框架总成;a left side side rail, a right side roof side rail, a top cover front beam, a top cover rear beam, and the top cover front beam is connected between the left side roof side rail and the right side top side rail The top cover rear beam is connected between the left side roof side rail and the right side roof side rail to make the left side roof side rail, the right side roof side rail, the top The front cover beam and the top cover rear beam together form a top cover frame assembly;
    驾驶舱下部框架,所述驾驶舱下部框架固定在所述顶盖框架总成的下方;a cockpit lower frame, the cockpit lower frame being fixed below the top cover frame assembly;
    前围板,所述前围板固定在所述驾驶舱下部框架的前部;a dash panel fixed to a front portion of the lower frame of the cockpit;
    地板面板,所述地板面板固定在所述驾驶舱下部框架的底部;以及a floor panel fixed to a bottom of the lower frame of the cockpit;
    后围板,所述后围板固定在所述驾驶舱下部框架的后部。a rear panel that is fixed to a rear portion of the lower frame of the cockpit.
  2. 根据权利要求1所述的驾驶舱框架,其特征在于,所述驾驶舱下部框架包括:The cockpit frame of claim 1 wherein said cockpit lower frame comprises:
    左右间隔设置的两个A柱;Two A-pillars spaced apart from each other;
    左右间隔设置的两个B柱,所述B柱位于所述A柱的后方;Two B pillars arranged at right and left intervals, the B pillars being located behind the A pillars;
    驾驶舱左下边梁,所述驾驶舱左下边梁分别与左侧的所述A柱的下端与左侧的所述B柱的下端连接;a left lower side sill of the cockpit, wherein the left lower side sill of the cockpit is connected to a lower end of the A-pillar on the left side and a lower end of the B-pillar on the left side, respectively;
    驾驶舱右下边梁,所述驾驶舱右下边梁分别与右侧的所述A柱的下端与右侧的所述B柱的下端连接;a right lower side sill of the cockpit, wherein the right lower side sill of the cockpit is respectively connected to a lower end of the A-pillar on the right side and a lower end of the B-pillar on the right side;
    多个驾驶舱连接横梁,所述多个驾驶舱连接横梁连接在所述驾驶舱左下边梁和所述驾驶舱右下边梁之间。A plurality of cockpit connecting beams, the plurality of cockpit connecting beams being coupled between the lower left side sill of the cockpit and the right lower side sill of the cockpit.
  3. 根据权利要求2所述的驾驶舱框架,其特征在于,所述驾驶舱连接横梁包括:The cockpit frame of claim 2 wherein said cockpit connecting beam comprises:
    驾驶舱前横梁,所述驾驶舱前横梁分别与所述驾驶舱左下边梁的前端以及所述驾驶舱右下边梁的前端连接;a cockpit front cross member, the front cockpit cross beam being respectively connected to a front end of the left underside of the cockpit and a front end of the right lower side sill of the cockpit;
    驾驶舱后横梁,所述驾驶舱后横梁分别与所述驾驶舱左下边梁的后端以及所述驾驶舱右下边梁的后端连接;a cockpit rear cross member, the cockpit rear cross member being respectively connected to a rear end of the left lower side sill of the cockpit and a rear end of the right lower side sill of the cockpit;
    驾驶舱中间横梁,所述驾驶舱中间横梁位于所述驾驶舱前横梁和所述驾驶舱后横梁之间。a cockpit intermediate beam, the cockpit intermediate beam being located between the cockpit front cross member and the cockpit rear cross member.
  4. 根据权利要求3所述的驾驶舱框架,其特征在于,所述驾驶舱下部框架还包括:The cockpit frame of claim 3 wherein said cockpit lower frame further comprises:
    驾驶舱连接纵梁,所述驾驶舱连接纵梁沿前后方向延伸且连接在所述驾驶舱前横梁和所述驾驶舱中间横梁之间,所述驾驶舱连接纵梁位于所述驾驶舱左下边梁和所述驾驶舱右下边梁之间。a cockpit connecting a longitudinal beam, the cockpit connecting stringer extending in a front-rear direction and being connected between the cockpit front cross member and the cockpit intermediate cross member, the cockpit connecting stringer being located at a lower left side of the cockpit Between the beam and the right lower side of the cockpit.
  5. 根据权利要求3所述的驾驶舱框架,其特征在于,所述驾驶舱下部框架还包括:两个加强件,两个所述加强件分别位于所述驾驶舱后横梁与所述驾驶舱左下边梁的连接处以及所述驾驶舱后横梁与所述驾驶舱右下边梁的连接处。A cockpit frame according to claim 3, wherein said cockpit lower frame further comprises: two reinforcing members, said two reinforcing members being respectively located at said cockpit rear cross member and said lower left side of said cockpit a joint of the beam and a junction of the cockpit rear cross member and the right lower side sill of the cockpit.
  6. 根据权利要求3所述的驾驶舱框架,其特征在于,所述地板面板包括:The cockpit frame of claim 3 wherein said floor panel comprises:
    左前地板,所述左前地板安装在所述驾驶舱下部框架的底部的左前部;a left front floor, the left front floor being mounted at a left front portion of a bottom of the lower frame of the cockpit;
    右前地板,所述右前地板安装在所述驾驶舱下部框架的底部的右前部;以及a right front floor, the right front floor being mounted to the right front of the bottom of the lower frame of the cockpit;
    后地板,所述后地板安装在所述驾驶舱下部框架的底部的后部。A rear floor, the rear floor being mounted at the rear of the bottom of the lower frame of the cockpit.
  7. 根据权利要求6所述的驾驶舱框架,其特征在于,所述左前地板安装 在所述驾驶舱连接纵梁、所述驾驶舱前横梁、所述驾驶舱左下边梁和所述驾驶舱中间横梁限制的区域内,所述右前地板安装在所述驾驶舱连接纵梁、所述驾驶舱前横梁、所述驾驶舱右下边梁和所述驾驶舱中间横梁限制的区域内,所述后地板安装在所述驾驶舱右下边梁、所述驾驶舱后横梁、所述驾驶舱左下边梁和所述驾驶舱中间横梁限制的区域内。A cockpit frame according to claim 6 wherein said left front floor is mounted to said cockpit connecting stringer, said cockpit front cross member, said cockpit lower left side rail and said cockpit intermediate beam In the restricted area, the right front floor is installed in the cockpit connecting stringer, the cockpit front cross member, the cockpit right side sill and the cockpit intermediate beam restricted area, the rear floor installation In the area of the cockpit right lower side rail, the cockpit rear cross member, the cockpit left lower side rail, and the cockpit intermediate cross member.
  8. 根据权利要求1-7中任一项所述的驾驶舱框架,其特征在于,所述驾驶舱框架为轻质合金框架。The cockpit frame according to any one of claims 1 to 7, wherein the cockpit frame is a lightweight alloy frame.
  9. 根据权利要求8所述的驾驶舱框架,其特征在于,所述驾驶舱框架为铝合金框架。The cockpit frame of claim 8 wherein said cockpit frame is an aluminum alloy frame.
  10. 一种车辆,其特征在于,包括根据权利要求1-9中任一项所述的驾驶舱框架。A vehicle characterized by comprising a cockpit frame according to any one of claims 1-9.
PCT/CN2017/119059 2017-03-07 2017-12-27 Cabin frame and vehicle having same WO2018161696A1 (en)

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Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN206579721U (en) * 2017-03-07 2017-10-24 北京新能源汽车股份有限公司 Cabin frame and the vehicle with it
CN110316254A (en) * 2018-03-30 2019-10-11 蔚来汽车有限公司 Squab panel component and vehicle
CN108857127B (en) * 2018-08-09 2021-01-22 北京长城华冠汽车科技股份有限公司 Welding method of frame type aluminum alloy car body top cover
CN111572649B (en) * 2020-05-25 2022-03-22 安徽江淮汽车集团股份有限公司 Body-in-white structure

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007069799A (en) * 2005-09-08 2007-03-22 Komatsu Ltd Construction vehicle
CN201842151U (en) * 2010-04-06 2011-05-25 厦门厦工机械股份有限公司 Novel cab capsule
CN203698445U (en) * 2013-12-31 2014-07-09 中铁十一局集团汉江重工有限公司 Mining dump truck cab framework
CN204399304U (en) * 2015-01-06 2015-06-17 烟台嘉华车辆部件有限公司 A kind of cab framework
CN106143652A (en) * 2016-06-30 2016-11-23 徐州徐工矿山机械有限公司 A kind of radial type cab of mine dump truck
CN206579721U (en) * 2017-03-07 2017-10-24 北京新能源汽车股份有限公司 Cabin frame and the vehicle with it
CN206634069U (en) * 2017-03-07 2017-11-14 北京新能源汽车股份有限公司 Body shell assembly and there is its vehicle
CN206954318U (en) * 2017-03-07 2018-02-02 北京新能源汽车股份有限公司 the vehicle body of automobile

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007069799A (en) * 2005-09-08 2007-03-22 Komatsu Ltd Construction vehicle
CN201842151U (en) * 2010-04-06 2011-05-25 厦门厦工机械股份有限公司 Novel cab capsule
CN203698445U (en) * 2013-12-31 2014-07-09 中铁十一局集团汉江重工有限公司 Mining dump truck cab framework
CN204399304U (en) * 2015-01-06 2015-06-17 烟台嘉华车辆部件有限公司 A kind of cab framework
CN106143652A (en) * 2016-06-30 2016-11-23 徐州徐工矿山机械有限公司 A kind of radial type cab of mine dump truck
CN206579721U (en) * 2017-03-07 2017-10-24 北京新能源汽车股份有限公司 Cabin frame and the vehicle with it
CN206634069U (en) * 2017-03-07 2017-11-14 北京新能源汽车股份有限公司 Body shell assembly and there is its vehicle
CN206954318U (en) * 2017-03-07 2018-02-02 北京新能源汽车股份有限公司 the vehicle body of automobile

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