CN203175322U - Aluminum alloy side cabin door of passenger car - Google Patents
Aluminum alloy side cabin door of passenger car Download PDFInfo
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- CN203175322U CN203175322U CN 201320048336 CN201320048336U CN203175322U CN 203175322 U CN203175322 U CN 203175322U CN 201320048336 CN201320048336 CN 201320048336 CN 201320048336 U CN201320048336 U CN 201320048336U CN 203175322 U CN203175322 U CN 203175322U
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 43
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 52
- 238000007689 inspection Methods 0.000 claims description 66
- 230000002787 reinforcement Effects 0.000 claims description 42
- 230000007704 transition Effects 0.000 claims description 9
- 239000003351 stiffener Substances 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 4
- 239000013585 weight reducing agent Substances 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 15
- 238000006748 scratching Methods 0.000 description 9
- 230000002393 scratching effect Effects 0.000 description 9
- 238000003754 machining Methods 0.000 description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000001125 extrusion Methods 0.000 description 3
- 238000003466 welding Methods 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 230000000903 blocking effect Effects 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 102220480540 Glycogen synthase kinase-3 beta_R96A_mutation Human genes 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 210000002435 tendon Anatomy 0.000 description 1
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Abstract
Description
技术领域 technical field
本实用新型涉及客车侧舱门结构,更具体的说涉及一种客车铝合金侧舱门,属于客车车身技术领域。 The utility model relates to a passenger car side cabin door structure, in particular to an aluminum alloy side cabin door of a passenger car, which belongs to the technical field of passenger car bodies.
背景技术 Background technique
目前国内客车多是钢结构车身,但很多零部件已经广泛采用铝合金材料,用的最多的是铝合金侧舱门。目前,现有的国内客车厂生产的铝合金侧舱门结构类似于原来的钢骨架侧舱门结构,如泰州市第一铝材厂生产的东风汽车有限公司R96A车型所用的铝合金侧舱门,参见图1、图2,侧舱门分为侧检修门和行李舱门,侧舱门包括舱门外板1和舱门骨架,舱门外板1是利用单块铝合金平板弯曲后形成,舱门外板1上端与舱门铰链26相连接固定,其中舱门骨架由两根竖梁25、上横梁27和下横梁焊接而成,两根竖梁25分别固定在舱门外板1内侧的两边,竖梁25的上部固定有气撑支架4;当侧舱门为行李舱门时,行李舱门由于其舱门锁较大,舱门外板1内侧的下部设置有行李舱门锁封板23来固定舱门锁,现有的铝合金行李舱门中是由下横梁焊接在舱门外板1上作为行李舱门锁封板23,行李舱门锁封板23为U形,其与舱门外板1形成一个行李舱门锁封腔24;行李舱门锁封板23中部开有行李舱门锁中间检修口12,行李舱门锁封板23两边开有行李舱门锁侧边检修口11,用于对舱门锁进行安装或检修;在舱门外板1外侧相对于行李舱门锁中间检修口12的位置设置有外侧锁孔13;行李舱门锁封板23的两端焊有行李舱门锁堵板8,行李舱门锁堵板8上设有行李舱门边锁孔10,用于固定锁舌。这种侧舱门是由铝合金舱门外板1贴合在舱门骨架上焊接而成,舱门骨架是侧舱门的主体结构,相对较软、易变形,因此往往通过增加舱门外板1的厚度来提高其刚度,通常该种铝合金侧舱门的舱门外板1为3.0mm厚,这种结构导致侧舱门整体减重效果不明显,没有充分体现出铝合金材料的性能优势。
At present, most domestic passenger cars have steel structure bodies, but aluminum alloy materials have been widely used for many parts, and the aluminum alloy side hatches are the most used. At present, the structure of the aluminum alloy side hatch produced by the existing domestic passenger car factory is similar to the original steel skeleton side hatch structure, such as the aluminum alloy side hatch used in the R96A model of Dongfeng Motor Co., Ltd. produced by Taizhou No. 1 Aluminum Material Factory , see Figure 1 and Figure 2, the side hatch is divided into a side inspection door and a luggage compartment door, the side hatch includes the hatch
发明内容 Contents of the invention
本实用新型的目的在于克服现有的铝合金侧舱门刚度低、重量大等问题,提供一种客车铝合金侧舱门。 The purpose of the utility model is to overcome the problems of low rigidity and heavy weight of the existing aluminum alloy side hatch, and provide an aluminum alloy side hatch for passenger cars.
为实现上述目的,本实用新型的技术解决方案是:一种客车铝合金侧舱门,侧舱门分为侧检修门和行李舱门,包括舱门外板和固定在舱门外板内侧两边的竖梁,所述的舱门外板上端与舱门铰链相连接,所述两边的竖梁上部固定有气撑支架,当侧舱门为行李舱门时,舱门外板内侧的下部设置有行李舱门锁封板,所述的舱门外板由挤压式铝合金型材制成,所述舱门外板内侧两边的竖梁之间设置有一根或多根I形的普通加强筋,所述的普通加强筋垂直于舱门外板板面。 In order to achieve the above object, the technical solution of the utility model is: a passenger car aluminum alloy side cabin door, the side cabin door is divided into a side inspection door and a luggage cabin door, including the door outer panel and the two sides fixed on the inner side of the cabin door outer panel The upper part of the outer panel of the cabin door is connected to the hinge of the cabin door, and the upper part of the vertical beam on both sides is fixed with an air support bracket. When the side cabin door is a luggage compartment door, the lower part of the inner side of the outer panel of the cabin door There is a lock and seal plate for the luggage compartment door, and the outer panel of the cabin door is made of extruded aluminum alloy profiles, and one or more I-shaped ordinary reinforcing ribs are arranged between the vertical beams on both sides of the inner side of the outer panel of the cabin door , the common stiffener is perpendicular to the outer panel of the hatch door.
所述舱门外板内侧的中部均匀设置有一根或多根竖梁,所述普通加强筋设置在相邻的竖梁之间。 One or more vertical beams are uniformly arranged in the middle of the inner side of the outer panel of the cabin door, and the common reinforcing ribs are arranged between adjacent vertical beams.
所述舱门外板内侧上端设置有铰链固定筋,所述铰链固定筋为L形边,方向朝下,舱门外板通过铰链固定筋与舱门铰链相连接,铰链固定筋与竖梁连接固定。 The upper end of the inner side of the door outer panel is provided with a hinge fixing rib, the hinge fixing rib is an L-shaped side, and the direction is downward, the hatch door outer panel is connected with the hatch hinge through the hinge fixing rib, and the hinge fixing rib is connected with the vertical beam fixed.
所述舱门外板内侧、两边的竖梁之间设置有气撑支架固定加强筋,所述气撑支架固定加强筋为L形边,方向朝上,分布在铰链固定筋的下方,气撑支架固定加强筋与竖梁连接固定,所述气撑支架与气撑支架固定加强筋和两边的竖梁同时连接固定。 The inner side of the outer panel of the hatch door and between the vertical beams on both sides are provided with air support bracket fixing reinforcement ribs, and the air support bracket fixing reinforcement ribs are L-shaped sides with an upward direction and are distributed below the hinge fixing ribs. The bracket fixing reinforcing rib is connected and fixed with the vertical beam, and the air support bracket is connected and fixed with the gas supporting bracket fixing reinforcing rib and the vertical beams on both sides at the same time.
所述的舱门外板由上侧舱门外板和下侧舱门外板组成,所述的竖梁包括上竖梁和下竖梁,所述的上侧舱门外板内侧固定有上竖梁,所述的下侧舱门外板内侧固定有下竖梁,所述气撑支架固定在两边的上竖梁上,所述上侧舱门外板内侧、相邻的上竖梁之间设置有普通加强筋,所述的下侧舱门外板内侧、相邻的下竖梁之间设置有普通加强筋,所述上侧舱门外板内侧的下端、两边的上竖梁之间设置有上连接加强筋,所述的上连接加强筋为L形边,方向朝上,上连接加强筋与上竖梁连接固定,当侧舱门为侧检修门时,所述的下侧舱门外板为侧检修门外板,所述的下竖梁为侧检修门下竖梁,上竖梁与侧检修门下竖梁上下对齐固定,所述侧检修门外板内侧的上端、两边的侧检修门下竖梁之间设置有侧检修门连接加强筋,所述的侧检修门连接加强筋为L形边,方向朝下,侧检修门连接加强筋与侧检修门下竖梁连接固定,上连接加强筋和侧检修门连接加强筋对接固定;当侧舱门为行李舱门时,所述的下侧舱门外板为行李舱门外板,所述的下竖梁为行李舱门下竖梁,上竖梁与行李舱门下竖梁上下对齐固定,所述行李舱门外板内侧的上端、两边的行李舱门下竖梁之间设置有行李舱门连接加强筋,所述行李舱门连接加强筋为L形,方向朝下,行李舱门连接加强筋与行李舱门下竖梁连接固定,上连接加强筋和行李舱门连接加强筋对接固定。 The hatch door outer plate is composed of an upper hatch door outer plate and a lower side hatch door outer plate, and the vertical beam includes an upper vertical beam and a lower vertical beam, and the inner side of the upper hatch door outer plate is fixed with an upper Vertical beams, the lower vertical beams are fixed on the inner side of the outer panel of the lower hatch door, the air support brackets are fixed on the upper vertical beams on both sides, and the inner side of the outer panel of the upper hatch door and the adjacent upper vertical beams Ordinary reinforcing ribs are arranged between the inner side of the outer panel of the lower hatch door and between the adjacent lower vertical beams, and the lower end of the inner side of the outer panel of the upper hatch door and the upper vertical beams on both sides An upper connection reinforcing rib is arranged between them, the upper connecting reinforcing rib is an L-shaped side, and the direction is upward, and the upper connecting reinforcing rib is connected and fixed with the upper vertical beam. When the side cabin door is a side inspection door, the lower side The outer panel of the hatch door is the outer panel of the side inspection door, the lower vertical beam is the lower vertical beam of the side inspection door, the upper vertical beam is aligned and fixed up and down with the lower vertical beam of the side inspection door, the upper end of the inner side of the outer panel of the side inspection door, the The side inspection door connecting stiffener is arranged between the lower vertical beams of the side inspection door, and the side inspection door connecting reinforcing rib is an L-shaped side, the direction is downward, and the side inspection door connecting reinforcing rib is connected and fixed with the side inspection door lower vertical beam. The connecting reinforcing rib and the connecting reinforcing rib of the side inspection door are docked and fixed; when the side hatch is a luggage compartment door, the outer panel of the lower side compartment door is the outer panel of the luggage compartment door, and the lower vertical beam is the lower vertical panel of the luggage compartment door. Beam, the upper vertical beam and the lower vertical beam of the luggage compartment door are aligned and fixed up and down, the upper end of the inner side of the outer panel of the luggage compartment door, and the luggage compartment door lower vertical beams on both sides are provided with reinforcement ribs for connecting the luggage compartment door, and the luggage compartment door is connected The reinforcing rib is L-shaped, and the direction is downward. The connecting reinforcing rib of the luggage compartment door is connected and fixed with the lower vertical beam of the luggage compartment door, and the upper connecting reinforcing rib is connected and fixed with the connecting reinforcing rib of the luggage compartment door.
所述的上连接加强筋和上侧舱门外板的过渡段开有倒角,当侧舱门为侧检修门时,侧检修门连接加强筋和侧检修门外板的过渡段开有倒角,当侧舱门为行李舱门时,行李舱门连接加强筋和行李舱门外板的过渡段开有倒角。 The transition section between the upper connecting rib and the outer panel of the upper side hatch is chamfered. If the side hatch is a luggage compartment door, the transition section connecting the reinforcement rib of the luggage compartment door and the outer panel of the luggage compartment door is chamfered.
所述下侧舱门外板内侧的最下端设置有裙边加强筋,所述的裙边加强筋为J形边,方向朝上。 The lowermost end of the inner side of the outer panel of the lower hatch door is provided with a skirt reinforcement rib, and the skirt reinforcement rib is a J-shaped edge with an upward direction.
当下侧舱门外板为侧检修门外板时,所述的裙边加强筋上方、两边的侧检修门下竖梁之间设置有门锁固定加强筋,所述的门锁固定加强筋为L形边,方向朝上,门锁固定加强筋与侧检修门下竖梁连接固定。 When the outer panel of the lower hatch door is the outer panel of the side access door, a door lock fixing rib is arranged above the skirt rib and between the lower vertical beams of the side access door on both sides, and the door lock fixing rib is L Shaped side, the direction is upward, and the door lock fixing reinforcement is connected and fixed with the lower vertical beam of the side inspection door.
与现有技术相比较,本实用新型的有益效果是: Compared with the prior art, the beneficial effects of the utility model are:
提升了侧舱门的整体刚度,减重效果好。本实用新型的舱门外板是由单块或两块挤压式铝合金型材制成,舱门外板构成侧舱门主体,减轻了侧舱门的重量;舱门外板内侧设置有竖梁,竖梁作为辅助加强结构对侧舱门进行加固,舱门外板的内侧设置有多种加强筋,提高了侧舱门的整体刚度。 The overall rigidity of the side hatch is improved, and the weight reduction effect is good. The outer panel of the hatch door of the utility model is made of a single or two extruded aluminum alloy profiles, and the outer panel of the hatch door constitutes the main body of the side hatch door, which reduces the weight of the side hatch; the inner side of the outer panel of the hatch door is provided with a vertical Beams and vertical beams are used as auxiliary reinforcement structures to reinforce the side hatch, and various reinforcing ribs are arranged on the inner side of the hatch outer panel, which improves the overall rigidity of the side hatch.
附图说明 Description of drawings
图1为现有的铝合金侧检修门结构。 Fig. 1 is the structure of the existing aluminum alloy side inspection door.
图2为现有的铝合金行李舱门结构。 Fig. 2 is the structure of the existing aluminum alloy luggage compartment door.
图3是本实用新型侧检修门的轴测图。 Fig. 3 is an axonometric view of the side inspection door of the present invention.
图4是本实用新型侧检修门的左视图。 Fig. 4 is a left view of the utility model side inspection door.
图5是本实用新型侧检修门的主视图。 Fig. 5 is a front view of the utility model side inspection door.
图6是本实用新型行李舱门的轴测图。 Fig. 6 is an axonometric view of the luggage compartment door of the present invention.
图7是本实用新型行李舱门的左视图。 Fig. 7 is a left view of the luggage compartment door of the present invention.
图8是本实用新型行李舱门的主视图。 Fig. 8 is a front view of the luggage compartment door of the present invention.
图9是本实用新型行李舱门的后视图。 Fig. 9 is a rear view of the luggage compartment door of the present invention.
图10是本实用新型上侧舱门外板的截面图。 Fig. 10 is a cross-sectional view of the outer panel of the upper hatch door of the present invention.
图11是本实用新型侧检修门外板的截面图。 Fig. 11 is a cross-sectional view of the outer panel of the side maintenance door of the present invention.
图12是本实用新型行李舱门外板的截面图。 Fig. 12 is a sectional view of the outer panel of the luggage compartment door of the present invention.
图13是本实用新型中上竖梁和气撑支架连接示意图。 Fig. 13 is a schematic diagram of the connection between the upper vertical beam and the air support bracket in the utility model.
图14是本实用新型中上竖梁和上连接加强筋连接示意图。 Fig. 14 is a schematic diagram of the connection between the upper vertical beam and the upper connecting rib in the utility model.
图15是本实用新型中铰链固定筋和舱门铰链连接示意图。 Fig. 15 is a schematic diagram of the connection between the hinge fixing rib and the door hinge in the present invention.
图16是本实用新型A-A剖视图。 Fig. 16 is an A-A sectional view of the utility model.
图17是本实用新型B-B剖视图。 Fig. 17 is a B-B sectional view of the utility model.
图中,舱门外板1,上侧舱门外板2,侧检修门外板3,气撑支架4,上竖梁5,侧检修门下竖梁6,行李舱门外板7,行李舱门锁堵板8,行李舱门下竖梁9,行李舱门边锁孔10,行李舱门锁侧边检修口11,行李舱门锁中间检修口12,外侧锁孔13,铰链固定筋14,普通加强筋15,气撑支架固定加强筋16,上连接加强筋17,倒角18,侧检修门连接加强筋19,门锁固定加强筋20,裙边加强筋21,行李舱门连接加强筋22,行李舱门锁封板23,行李舱门锁封腔24,竖梁25,舱门铰链26,上横梁27,侧围腰梁28,焊缝29,铆钉30。
In the figure, door
具体实施方式 Detailed ways
以下结合附图说明和具体实施方式对本实用新型作进一步的详细描述。 The utility model will be described in further detail below in conjunction with the accompanying drawings and specific embodiments.
参见图3-图17,一种客车铝合金侧舱门,侧舱门分为侧检修门和行李舱门,包括舱门外板1和固定在舱门外板1内侧两边的竖梁25,竖梁25为U形或L形的铝型材,所述的舱门外板1上端与舱门铰链26相连接。所述两边的竖梁25上部固定有气撑支架4,气撑支架4由L形铝合金型材加工而成,L形铝合金型材的两边进行倒角或倒圆处理,以排除尖角伤人隐患,气撑支架4上设有圆孔,用以固定连接气撑。当侧舱门为行李舱门时,行李舱门由于其舱门锁较大,舱门外板1内侧的下部设置有行李舱门锁封板23来固定舱门锁,行李舱门锁封板23为U形,其与舱门外板1形成一个行李舱门锁封腔24;行李舱门锁封板23中部开有行李舱门锁中间检修口12,行李舱门锁封板23两边开有行李舱门锁侧边检修口11,用于对舱门锁进行安装或检修;在舱门外板1外侧相对于行李舱门锁中间检修口12的位置设置有外侧锁孔13;行李舱门锁封板23的两端焊接有行李舱门锁堵板8,行李舱门锁堵板8上设有行李舱门边锁孔10,用于固定锁舌。所述的舱门外板1由挤压式铝合金型材制成,所述舱门外板1内侧设置有一根或多根I形的普通加强筋15,所述的普通加强筋15垂直于舱门外板1板面以提高舱门外板1的整体刚度,并改善挤压式铝型材舱门外板1的挤压工艺;普通加强筋15设置于两边的竖梁25之间,一般是普通加强筋15在两边的竖梁25外侧通过机加工切割掉,以避免开启过程中出现刮伤人的隐患。本实用新型中舱门外板1构成了侧舱门的主体,而内部的竖梁25只作为侧舱门的辅助加强结构。根据侧舱门的长短需要,可以在舱门外板1内侧的中部均匀设置有一根或多根竖梁25,普通加强筋15设置在相邻的竖梁25之间。所述舱门外板1内侧上端设置有铰链固定筋14,所述铰链固定筋14为L形边,方向朝下,舱门外板1通过铰链固定筋14与舱门铰链26相连接,铰链固定筋14与竖梁25通过铆钉30进行连接固定。所述舱门外板内侧1设置有气撑支架固定加强筋16,所述气撑支架固定加强筋16为L形边,方向朝上,分布在铰链固定筋14的下方,气撑支架固定加强筋16位于气撑支架4附近,用于对此处竖梁25进行刚度加强,气撑支架固定加强筋16设置于两边的竖梁25之间,一般是气撑支架固定加强筋16在两边的竖梁25外侧通过机加工切割掉,以避免开启过程中出现刮伤人的隐患;气撑支架固定加强筋16与竖梁25通过铆钉30连接固定,气撑支架4的下方可以和气撑支架固定加强筋16以及两边的竖梁25同时利用一个铆钉30同时连接固定。
Referring to Fig. 3-Fig. 17, an aluminum alloy side hatch of a passenger car, the side hatch is divided into a side inspection door and a luggage compartment door, including a hatch
参见图3-图5、图10-图11、13-图16,根据侧舱门高度和铝合金型材挤压工艺,该挤压式铝合金型材舱门外板1可以采用单块铝合金型材外板或者由两块铝合金型材外板组成,本实施例中的舱门外板1由上侧舱门外板2和下侧舱门外板组成,所述的竖梁25包括上竖梁5和下竖梁,所述的上侧舱门外板2内侧固定有上竖梁5,所述的下侧舱门外板内侧固定有下竖梁,所述气撑支架4固定在两边的上竖梁5上,所述上侧舱门外板2内侧、相邻的上竖梁5之间设置有普通加强筋15,所述的下侧舱门外板内侧、相邻的下竖梁之间设置有普通加强筋15;所述上侧舱门外板2内侧的下端设置有上连接加强筋17,所述的上连接加强筋17为L形边,方向朝上,上连接加强筋17设置在两边的上竖梁5之间,一般是上连接加强筋17在两边的上竖梁5外侧通过机加工切割掉,以避免开启过程中出现刮伤人的隐患;上连接加强筋17与上竖梁5通过铆钉30连接固定。当侧舱门为侧检修门时,所述的下侧舱门外板为侧检修门外板3,所述的下竖梁为侧检修门下竖梁6,上竖梁5与侧检修门下竖梁6上下对齐固定,所述侧检修门外板3内侧的上端设置有侧检修门连接加强筋19,所述的侧检修门连接加强筋19为L形边,方向朝下,侧检修门连接加强筋19设置在两边的侧检修门下竖梁6之间,一般是侧检修门连接加强筋19在两边的侧检修门下竖梁6外侧通过机加工切割掉,以避免开启过程中出现刮伤人的隐患;侧检修门连接加强筋19与侧检修门下竖梁6通过铆钉30连接固定。上连接加强筋17和侧检修门连接加强筋19对接固定,实现侧检修门的拼接,从而完成侧检修门的拼装,即由上侧舱门外板2和侧检修门外板3拼接成一个侧检修门的舱门外板1。所述的上连接加强筋17和上侧舱门外板2的过渡段开有倒角18,侧检修门连接加强筋19和侧检修门外板3的过渡段开有倒角18,倒角18用以进行焊接处理,保证舱门外板连接1牢靠。所述的侧检修门外板3内侧的最下端设置有裙边加强筋21,所述的裙边加强筋21为J形边,方向朝上,对侧检修门外板3下边缘起到加强作用,裙边加强筋21在侧检修门外板3的两边一般通过机加工切割掉60mm长,以避免开启过程中出现刮伤人的隐患。所述的裙边加强筋21上方设置有门锁固定加强筋20,所述的门锁固定加强筋20为L形边,方向朝上,门锁固定加强筋20设置在两边的侧检修门下竖梁6之间,一般是门锁固定加强筋20在两边的侧检修门下竖梁6外侧通过机加工切割掉,以避免开启过程中出现刮伤人的隐患;门锁固定加强筋20并与侧检修门下竖梁6通过铆钉30连接固定,主要用于固定侧检修门锁。本实施例的实际组装过程如下:将上连接加强筋17和侧检修门连接加强筋19对齐后利用铆钉30进行铆接固定连接,然后在倒角18处进行焊接处理,焊缝29经打磨后保证表面平顺;在上侧舱门外板2的内侧通过铆接固定三根上竖梁5,并在两边的上竖梁5的车内侧上部固定气撑支架4,使气撑支架4的下端与气撑支架固定加强筋16和上竖梁5同时铆接固定;在侧检修门外板3的内侧通过铆接固定三根侧检修门下竖梁6,使侧检修门下竖梁6与上竖梁5能够上下对齐;将橡胶舱门铰链26的橡胶铰链下型材通过粘接固定在上侧舱门外板2的铰链固定筋14上,并利用铆钉30进行铆接固定,至此,完成了整个侧检修门的组装;最后将橡胶舱门铰链26的橡胶铰链上型材固定在侧围骨架的侧围腰梁28上即可。
Referring to Figure 3-Figure 5, Figure 10-Figure 11, 13-Figure 16, according to the height of the side hatch and the extrusion process of the aluminum alloy profile, the
参见图6-图10、图12-图15、图17,根据侧舱门高度和铝合金型材挤压工艺,该挤压式铝合金型材舱门外板1可以采用单块铝合金型材外板或者由两块铝合金型材外板组成,本实施例中的舱门外板1由上侧舱门外板2和下侧舱门外板组成,所述的竖梁25包括上竖梁5和下竖梁,所述的上侧舱门外板2内侧固定有上竖梁5,所述的下侧舱门外板内侧固定有下竖梁,所述气撑支架4固定在两边的上竖梁5上,所述上侧舱门外板2内侧、相邻的上竖梁5之间设置有普通加强筋15,所述的下侧舱门外板内侧、相邻的下竖梁之间设置有普通加强筋15;所述上侧舱门外板2内侧的下端设置有上连接加强筋17,所述的上连接加强筋17为L形边,方向朝上,上连接加强筋17设置在两边的上竖梁5之间,一般是上连接加强筋17在两边的上竖梁5外侧通过机加工切割掉,以避免开启过程中出现刮伤人的隐患;上连接加强筋17与上竖梁5通过铆钉30连接固定。当侧舱门为行李舱门时,所述的下侧舱门外板为行李舱门外板7,所述的下竖梁为行李舱门下竖梁9,上竖梁5与行李舱门下竖梁9上下对齐固定;所述行李舱门外板7内侧的上端设置有行李舱门连接加强筋22,所述行李舱门连接加强筋22为L形,方向朝下,行李舱门连接加强筋22设置在两边的行李舱门下竖梁9之间,一般是行李舱门连接加强筋22在行李舱门下竖梁9外侧通过机加工切割掉,以避免开启过程中出现刮伤人的隐患;行李舱门连接加强筋22与行李舱门下竖梁9通过铆钉30连接固定。上连接加强筋17和行李舱门连接加强筋22对接固定,实现行李舱门的拼接,从而完成行李舱门的拼装,即由上侧舱门外板2和行李舱门外板7拼接成一个行李舱门的舱门外板1。上连接加强筋17和上侧舱门外板2的过渡段开有倒角18,行李舱门连接加强筋22和行李舱门外板7的过渡段开有倒角18,倒角18用以进行焊接处理,保证舱门外板连接1牢靠。所述的下行李舱门外板7内侧的最下端设置有裙边加强筋21,所述的裙边加强筋21为J形边,方向朝上,对行李舱门外板7下边缘起到加强作用;裙边加强筋21在行李舱门外板7的两边一般通过机加工切割掉60mm长,以避免开启过程中出现刮伤人的隐患。本实施例的实际组装过程如下:将上连接加强筋17和行李舱门连接加强筋22对齐后利用铆钉30进行铆接固定连接,然后在倒角18处进行焊接处理,焊缝29经打磨后保证表面平顺;在上侧舱门外板2的内侧通过铆接固定三根上竖梁5,并在两边的上竖梁5的车内侧固定气撑支架4,使气撑支架4的下端与气撑支架固定加强筋16和上竖梁5同时铆接固定;在行李舱门外板7的内侧通过铆接固定三根行李舱门下竖梁9,使行李舱门下竖梁9与上竖梁5能够上下对齐;将橡胶舱门铰链26的橡胶铰链下型材通过粘接固定在上侧舱门外板2的铰链固定筋14上,并利用铆钉30进行铆接固定,至此,完成了整个行李舱门的组装;最后将橡胶舱门铰链26的橡胶铰链上型材固定在侧围骨架的侧围腰梁28上即可。
Referring to Figure 6-Figure 10, Figure 12-Figure 15, and Figure 17, according to the height of the side hatch and the extrusion process of the aluminum alloy profile, the
以上内容是结合具体的优选实施方式对本实用新型所作的进一步详细说明,不能认定本实用新型的具体实施只局限于这些说明。对于本实用新型所属技术领域的普通技术人员来说,在不脱离本实用新型构思的前提下,还可以做出若干简单推演或替换,上述结构都应当视为属于本实用新型的保护范围。 The above content is a further detailed description of the utility model in combination with specific preferred embodiments, and it cannot be assumed that the specific implementation of the utility model is only limited to these descriptions. For those of ordinary skill in the technical field to which the utility model belongs, some simple deduction or replacement can also be made without departing from the concept of the utility model, and the above structures should be regarded as belonging to the protection scope of the utility model. the
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103206150A (en) * | 2013-01-29 | 2013-07-17 | 东风汽车有限公司 | A passenger car aluminum alloy side cabin door |
| CN107336590A (en) * | 2016-12-28 | 2017-11-10 | 浙江中车电车有限公司 | A kind of side hatch door and the vehicle body with side hatch door |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103206150A (en) * | 2013-01-29 | 2013-07-17 | 东风汽车有限公司 | A passenger car aluminum alloy side cabin door |
| CN107336590A (en) * | 2016-12-28 | 2017-11-10 | 浙江中车电车有限公司 | A kind of side hatch door and the vehicle body with side hatch door |
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