CN203805331U - 组合件 - Google Patents

组合件 Download PDF

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Publication number
CN203805331U
CN203805331U CN201420053786.9U CN201420053786U CN203805331U CN 203805331 U CN203805331 U CN 203805331U CN 201420053786 U CN201420053786 U CN 201420053786U CN 203805331 U CN203805331 U CN 203805331U
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China
Prior art keywords
assembly
sub
fiber
resin matrix
securing member
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Expired - Fee Related
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CN201420053786.9U
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English (en)
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艾因卓·麦凯尔维·坎贝尔
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Ford Global Technologies LLC
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Ford Global Technologies LLC
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/72—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by combined operations or combined techniques, e.g. welding and stitching
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during moulding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P11/00—Connecting or disconnecting metal parts or objects by metal-working techniques not otherwise provided for 
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/84—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks by moulding material on preformed parts to be joined
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form
    • B32B3/02—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by features of form at particular places, e.g. in edge regions
    • B32B3/06—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by features of form at particular places, e.g. in edge regions for securing layers together; for attaching the product to another member, e.g. to a support, or to another product, e.g. groove/tongue, interlocking
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/14—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by a layer differing constitutionally or physically in different parts, e.g. denser near its faces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
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    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/05—Interconnection of layers the layers not being connected over the whole surface, e.g. discontinuous connection or patterned connection
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    • B62D—MOTOR VEHICLES; TRAILERS
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/04—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of riveting
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    • B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
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    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
    • B29C65/562—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits using extra joining elements, i.e. which are not integral with the parts to be joined
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/112—Single lapped joints
    • B29C66/1122—Single lap to lap joints, i.e. overlap joints
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
    • B29C66/21—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being formed by a single dot or dash or by several dots or dashes, i.e. spot joining or spot welding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
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    • B29C66/7212—Fibre-reinforced materials characterised by the composition of the fibres
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    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
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    • B29C66/742—Joining plastics material to non-plastics material to metals or their alloys
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    • B29L2031/727—Fastening elements
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    • Y10T29/49835—Punching, piercing or reaming part by surface of second part with shaping
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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
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    • Y10T428/24994—Fiber embedded in or on the surface of a polymeric matrix

Abstract

本实用新型提供了一种组合件，其包括：树脂基体，具有用于容纳紧固件的预定位置；以及位于树脂基体的第一部分中的强化树脂基体的纤维，树脂基体的位于所述预定位置的第二部分基本上不含纤维。本实用新型提供的组合件经过强化并且在与其它零件连接时不会产生裂缝。

Description

组合件
技术领域
本实用新型涉及强化组合件以及制造紧固性能提升的强化组合件组件的方法。
背景技术
随着汽车工业持续关注于减轻车辆重量以满足客户对于燃油经济性的期望和CAFE（Corporate Average Fuel Economy，公司平均燃油经济性）标准，汽车工业对包括碳纤维复合材料在内的替代材料的应用兴趣已经上升。在白车身结构中，连接方法传统上依赖于电阻点焊（例如，在钢结构中）。
在铝密集型车辆以及其他混合金属连接应用的情况下，自冲铆接（SPR）工艺盛行。SPR工艺的优势在于其为高产量装配工艺。此外，该工艺与粘合剂兼容，即这两种方法可结合使用。然而，SPR工艺通常面临的挑战是基底材料必须具有足够的延展性以形成“扣形物”，即凸起，该“扣形物”是创建连接的结果和提供机械互锁的必要形变。当组合件不具备足够的延展性以在正面形成扣形物时，纤维会通过该表面上的裂缝暴露。不期望出现表面裂缝和纤维移位，因为它们会降低连接的耐久度并导致过早失效。
其他可用于连接金属零件和纤维强化组合件的连接工艺包括热熔钻螺钉、冲铆连接以及热熔钻工艺。对于每一种工艺，紧固件插入区域或接头形成区域中的纤维都有可能导致表面裂缝或纤维移位。
由于将零件连接在一起的挑战，诸如碳素纤维、玻璃纤维或者天然纤维的复合材料在应用上受到限制。通常，这些复合材料具有有限的延展性，且不能很好地适应将零件连接在一起所需的大的位移和形变。
粘合剂被广泛用于将组合件连接在一起。粘接在其单独使用时是一种低产量的生产方法，而且粘接在胶粘物固化前易于产生位移（即，被连接零件之间的移动）。
其他方法（比如盲孔铆钉）可被用于将零件固定到组合件上，但是必须首先贯穿零件钻孔或预成形孔以便插入盲孔铆钉。钻孔、对齐孔、插入盲孔铆钉然后固定铆钉的装配操作增加了装配成本和加工成本。因此，需要一种既能满足高产量生产需求又能连接低延展性材料的连接方案。
本实用新型旨在克服以上问题，以及在其它零件连接于组合件的应用中与组合件的使用相关的其它问题。
实用新型内容
本实用新型的目的在于提供一种组合件，该组合件经过强化并且在与其它零件连接时不会产生裂缝。
根据本实用新型的一个方面，公开了一种组合件，其包括具有用于容纳紧固件的预定位置的树脂基体以及在树脂基体的第一部分中对树脂基体进行强化的纤维。树脂基体的位于预定位置的第二部分基本上不含纤维。
根据涉及组合件的本实用新型的另一个方面，强化树脂基体的纤维还包括编织垫，该编织垫于预定位置在编织垫中形成有孔口。可选地，强化树脂基体的纤维可为松散纤维，这些纤维分散在树脂基体的第一部分，但未分散在树脂基体的第二部分。
组合件可与装配件结合并一并提供，该装配件通过穿透组合件的第一侧和装配件的紧固件装配至组合件。该结合还可包括于预定位置、在组合件的与第一侧上的插入点相对的第二侧上形成的凸起。
根据本实用新型的再一个方面，公开了一种制造纤维强化组合件的方法，该方法包括提供形成有孔口的纤维垫。将纤维垫插入模具中，同时使孔口位于模具中的预定位置。液态的树脂被供应至模具并将纤维垫封装。然后，对模具中的树脂进行硬化或固化。树脂填充孔口，以于预定位置、在纤维强化组合件上提供基本不含纤维的紧固件容纳区域。
根据本实用新型的其他方面，该方法还可包括将第二零件装配至纤维强化组合件。将纤维强化组合件和第二零件在预定位置连接到一起。连接纤维强化组合件和第二零件的步骤还可包括在第二零件和纤维强化组合件的紧固件容纳区域中形成冲铆连接。可选地，连接纤维强化组合件和第二零件的步骤还可包括穿透第二零件并深入纤维强化组合件的紧固件容纳区域插入紧固件。紧固件可为铆钉、自冲铆钉、自攻螺钉或者热熔钻螺钉。
根据本实用新型的又一个方面，公开了一种使用松散纤维材料制造纤维强化组合件的替代方法。该替代方法包括：防护模具的预定部分，同时向模具中沉积松散纤维材料，以使松散纤维材料不在模具的预定部分沉积。向模具供应液态的树脂，该树脂封装松散纤维强化材料并填充模具的预定部分。然后使树脂硬化以在纤维强化组合件中形成紧固件容纳区域，该紧固件容纳区域基本不含纤维。
根据本实用新型的其他方面，该方法还包括：装配第二零件至纤维强化组合件；以及将纤维强化组合件和第二零件在紧固件容纳区域连接在一起。
根据本实用新型的一个实施例，连接纤维强化组合件和第二零件的步骤还包括：在第二零件和纤维强化组合件的紧固件容纳区域中形成冲铆连接。
根据本实用新型的一个实施例，连接纤维强化组合件和第二零件的步骤还包括：插入紧固件使其穿透所述第二零件并深入所述纤维强化组合件的紧固件容纳区域之中。
根据本实用新型的一个实施例，在插入的步骤中，紧固件选自由铆钉、自冲铆钉、自攻螺钉和热熔钻螺钉组成的组。
本实用新型旨在解决上述问题，以及将在下文中参照所述实施例的附图更加详细描述的其它问题。
本实用新型的有益效果在于，通过提供局部区域未受到纤维强化的组合件，使得该组合件在得到强化的同时，在与其它零件装配形成组件时不会产生裂缝。
附图说明
图1是即将通过紧固件固定至纤维强化组合件的零件的分解立体图，该纤维强化组合件具有未利用纤维强化的紧固件容纳区域；
图2是模具的部分横断面视图，该模具具有形成有孔口并设置在模具中的纤维垫；
图3是填充有树脂基体材料和纤维垫的模具的部分横断面视图；
图4是包括销的模具的部分横断面视图，该销可在延长位置与回缩位置间移动，该销在延长位置可防止松散纤维沉积到模具的预定区域，此预定区域随后在销回缩时用树脂回填；
图5是包括销的模具的部分横断面视图，该销可在延长位置和回缩位置间移动，图中示出了销在回缩位置时松散纤维沉积在预定区域的周围；
图6是填充树脂基体材料且其中包括销的模具的部分横断面视图，该销可在延长位置和回缩位置间移动，图中示出了销在回缩位置时松散纤维沉积在预定区域的周围；
图7是将零件装配到纤维强化组合件的横断面视图，图中自冲铆钉位于将要插入上述零件的位置；
图8是零件装配到纤维强化组合件的横断面视图，图中自冲铆钉将上述零件紧固在一起；
图9是将零件装配到纤维强化组合件的横断面视图，图中热熔钻螺钉位于将要插入该零件的位置；
图10是零件装配到纤维强化组合件的横断面视图，图中热熔钻螺钉将上述零件紧固在一起；
图11是将零件装配到纤维强化组合件的横断面视图，图中冲铆连接成型工具位于将要连接该零件的位置；
图12是零件装配到纤维强化组合件的横断面视图，图中冲铆连接将上述零件紧固在一起。
具体实施方式
下面提供本实用新型所示实施例的详细描述。所公开的实施例是本实用新型的示例，本实用新型可由各种替代的形式实施。附图不一定按比例绘制。某些特征可能被放大或者缩小来展示特定部件的细节。本应用中所公开的特定构造和功能细节不应认作限定，而仅仅作为教导本领域技术人员如何实践本实用新型的代表性基础。
参照图1，组合件组件10被示出包括铝质零件12，其安置成即将通过自冲铆钉16连接到纤维强化组合件14。自冲铆钉16被示出与纤维强化组合件14中的紧固件容纳区域18对齐。这些零件利用自冲铆钉16进行装配的过程会在下文中参照图7和图8进行描述。
参照图2，所示模具20包括模具型腔22。编织纤维垫26在预定区域形成有孔口28，该预定区域对应于紧固件容纳区域18（见图1）的期望位置。编织纤维垫26被装入模具型腔22，此时孔口28位于预定区域中。
参照图3，所示模具20的模具型腔22被编织纤维垫26和倾注、注入或以其它方式供应至模具型腔22中的树脂基体30所填充。树脂基体填充编织纤维垫26之间的间隙，而且还填充纤维垫26内的孔口28。孔口28中的树脂基体30构成紧固件容纳区域18（见图1）。
参照图4，示出了模具32的替代实施例，其包括模具型腔34，该模具型腔中设置有销36。图4中所示的销36处于其延长位置。在销36处于其延长位置的同时，松散纤维38被供应至模具型腔34。处于延长位置的销36防止松散纤维38沉积到处于延长位置的销36在模具型腔34之内所占据的空间。处于延长位置的销36使模具型腔34的一部分免于被纤维38的沉积所占据。
参照图5，所示替代模具32的销36位于其回缩位置。除了在松散纤维38之内所形成的且位于销36上方的空间40之外，模具型腔34均包括松散纤维。应该理解，因为没有隔离物来阻止纤维38无意中沉积到空间40内，该空间40可能包括有限数量的松散纤维38。
参照图6，所示替代模具32的模具型腔34中所填充的松散纤维38现在被封装在树脂基体42中。树脂基体42填充松散纤维38之间的间隙区域，同时还填充空间40（见图5）。空间40中的树脂42构成紧固件容纳区域18（见图1）。树脂42和空间40可包括一些无意间沉积的纤维38。然而，该纤维38的密度应该明显地小于空间区域40的密度，空间区域40的纤维密度不足树脂基体42的其他部分中的纤维密度的10%。
应当理解，树脂42可按照具有两步固化的两步树脂注入工艺来注入。例如，可在销延伸时在模具中填充松散纤维。树脂可被注入模具32中并部分固化。
参照图7，铝质零件12和纤维强化组合件14被示出处于即将通过自冲铆钉16的插入而装配在一起的位置。自冲铆钉16与纤维强化组合件14内的紧固件容纳区域18相对齐。
参照图8，自冲铆钉16被铆钉冲头44驱动穿过面板12和14。支撑模46在紧固件容纳区域18处支撑纤维强化组合件14。自冲铆钉16的插入使得在纤维强化组合件14的正面形成扣形凸起48。
参照图9，热熔钻螺钉50对准铝质零件12和纤维强化组合件14。所示热熔钻螺钉50正准备插入到铝质零件12中并且与纤维强化组合件14所提供的紧固件容纳区域18相对齐。热熔钻螺钉50受力穿入铝质零件12要通过首先快速旋转热熔钻螺钉50并同时施加压力以驱动热熔钻螺钉50穿过铝质零件12来实现。在铝质零件12开始被热熔钻螺钉50穿透后，热熔钻螺钉50的旋转速度下降，而且热熔钻螺钉50上的螺纹在铝质零件12和纤维强化组合件14中形成螺纹孔。
虽然如图1所示的铝质零件12不具备排屑孔，应当理解，可提供穿过铝质零件12的排屑孔。若如此，那么排屑孔（未示出）应该与纤维强化组合件14中的紧固件容纳区域18对齐。铝质零件12的厚度和材料属性是确定是否必须为热熔钻螺钉50在铝质零件12中提供孔所必须考虑的因素。
参照图10，所示热熔钻螺钉50将铝质零件12固定至纤维强化组合件14。热熔钻螺钉50在纤维强化组合件14上整体形成衬套区域52。热熔钻螺钉50插入基本上没有纤维的紧固件容纳区域。衬套52中基本上没有纤维渗入、没有裂缝或开裂，通常，热熔钻螺钉50插入不具有紧固件容纳区域18的纤维强化组合件14时会形成裂缝或开裂。
参照图11，所示冲铆连接冲头56与冲铆连接支撑模58相对齐。纤维强化组合件14的紧固件容纳区域18设置在冲铆连接冲头56与冲铆连接支撑模58之间并且与它们两个对齐。
参照图12，示出了组合件组件10，铝质零件12通过冲铆连接60组装至纤维强化组合件14。冲铆连接60在基本上没有强化纤维的紧固件容纳区域18中形成。纤维强化组合件14的强化纤维强化了零件14，而紧固件容纳区域18中不存在纤维允许形成冲铆连接60而不会因纤维强行穿过纤维强化组合件14的紧固件容纳区域18的正面而造成裂缝或开裂。
尽管上面描述了示例性实施例，但并不意味着这些实施例描述了本实用新型的所有可能形式。相反，此说明书里的措辞仅仅是描述性措辞而非限制性措辞，并且应当理解，可进行各种改变而不偏离本实用新型所主张的主旨和范围。多种执行的实施例的特征可结合起来形成本实用新型的其它实施例。

Claims (4)

1.一种组合件，其特征在于，包括：
树脂基体，具有用于容纳紧固件的预定位置；以及
位于所述树脂基体的第一部分中的强化所述树脂基体的纤维，所述树脂基体的位于所述预定位置的第二部分不含纤维。
2.根据权利要求1所述的组合件，其特征在于，强化所述树脂基体的所述纤维还包括编织垫，所述编织垫于所述预定位置在所述编织垫中形成有孔口。
3.根据权利要求1所述的组合件，其特征在于，强化所述树脂基体的所述纤维是松散纤维，所述松散纤维分散在所述树脂基体的第一部分，而并未分散在所述树脂基体的第二部分。
4.根据权利要求1所述的组合件，其特征在于，所述组合件与装配件结合，所述装配件通过穿透所述组合件的第一侧和所述装配件的紧固件而装配至所述组合件，所述结合还包括：
于所述预定位置、在所述组合件的与所述第一侧相对的第二侧上形成的凸起。
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105538695A (zh) * 2014-10-24 2016-05-04 丰田自动车株式会社 连接元件的方法
CN110248798A (zh) * 2017-02-09 2019-09-17 中车青岛四方机车车辆股份有限公司 用于将部件连接至纤维复合结构的连接元件
CN110481061A (zh) * 2019-09-17 2019-11-22 中国航发沈阳发动机研究所 一种纤维增强复合材料的穿孔方法、消音板及其声衬

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2785859C (en) * 2010-02-26 2016-10-04 Mitsubishi Heavy Industries, Ltd. Repairing method for composite material and composite material using the same
US9023455B2 (en) * 2013-01-30 2015-05-05 Ford Global Technologies, Llc Method of making reinforced composite articles with reduced fiber content in local areas and articles made by the method
US20150001885A1 (en) * 2013-06-28 2015-01-01 GM Global Technology Operations LLC Mixed material underbody for noise controlled occupant compartment
US9346241B2 (en) * 2014-01-15 2016-05-24 Ford Global Technologies, Llc Composite panel for joining with a clinch joint and method of forming a clinch joint
US9718157B2 (en) * 2014-02-21 2017-08-01 Ford Global Technologies, Llc Expanding die for clinching and riveting operations
DE102014017810B4 (de) 2014-12-03 2018-05-03 Audi Ag Verfahren zum automatisierten, vorlochfreien Fügen von Faserverbundbauteilen mit einseitiger Zugänglichkeit
GB2533429A (en) * 2014-12-19 2016-06-22 Airbus Operations Ltd A metallic-composite joint
GB2535193A (en) * 2015-02-12 2016-08-17 Zodiac Seats Uk Ltd Tool for curing a composite component
DE102015106563B4 (de) * 2015-04-28 2024-03-21 Airbus Operations Gmbh Verfahren zum Verbinden von faserverstärkten Strukturbauteilen
DE102015110791A1 (de) * 2015-07-03 2017-01-05 Elringklinger Ag Verfahren zum Herstellen eines Abschirmteils aufweisend zumindest eine metallische Abschirmlage und eine textile Dämmlage sowie ein Abschirmteil
US10864682B2 (en) * 2018-03-05 2020-12-15 GM Global Technology Operations LLC Method of joining of polymeric composites

Family Cites Families (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3125974A (en) 1964-03-24 figure
US2845699A (en) 1955-12-13 1958-08-05 Lee L Woodard Sons Method of making contoured dished articles
US3053713A (en) 1958-01-13 1962-09-11 Union Carbide Corp Plastic articles reinforced with preformed precompressed metal fiber elements
US3429766A (en) 1965-10-21 1969-02-25 Raybestos Manhattan Inc Clutch facing
US4327536A (en) 1980-03-07 1982-05-04 Linx Building Systems Corp. Composite building panel
US4894102A (en) 1985-03-04 1990-01-16 Kenneth F. Halls Method for refinishing building panels
US4863771A (en) 1985-08-22 1989-09-05 The Budd Company Hollow fiber reinforced structure and method of making same
US5192330A (en) 1987-01-20 1993-03-09 Smith & Nephew Richards, Inc. Orthopedic device of biocompatible polymer with oriented fiber reinforcement
US5121537A (en) 1987-07-01 1992-06-16 Kawasaki Jukogyo Kabushiki Kaisha Method of production of anchor-bonded composite structures
US5139405A (en) 1988-05-31 1992-08-18 Phillips Petroleum Company Composite with integrally molded rib and manufacture thereof
JP2507565B2 (ja) 1988-11-24 1996-06-12 東レ株式会社 熱可塑性樹脂と補強繊維との複合板
JP2528024B2 (ja) * 1990-06-14 1996-08-28 豊田合成株式会社 自動車用スポイラ―
US5884386A (en) 1991-11-27 1999-03-23 Henrob Ltd. Panel clinching methods and apparatus
US5984055A (en) 1997-11-21 1999-11-16 Northrop Grumman Corporation Integrated fiber reinforced ceramic matrix composite brake pad and back plate
CA2287104A1 (en) * 1999-07-19 2001-01-19 Karl Hermann Werner Gregori Decking assembly and decking kit with hold-down clip
US6609286B2 (en) 2000-05-10 2003-08-26 Honda Giken Kogyo Kabushiki Kaisha Process for manufacturing a part of a metal matrix composite material
US7284319B2 (en) 2002-02-08 2007-10-23 Newfrey Llc Self-piercing rivet setting die and apparatus
US6921444B2 (en) 2003-01-13 2005-07-26 Ford Global Technologies, Llc Method of locally heating a part to reduce strength and increase ductility for subsequent manufacturing operation
US20050022362A1 (en) 2003-08-01 2005-02-03 San Shing Fastech Corp. Method for making a composite tool
US7410687B2 (en) * 2004-06-08 2008-08-12 Trex Co Inc Variegated composites and related methods of manufacture
DE112007001331B4 (de) 2006-05-31 2023-11-02 Atlas Copco IAS UK Ltd. Verfahren und Vorrichtung zum Verbinden
US20080072527A1 (en) 2006-08-01 2008-03-27 Honda Motor Co., Ltd. Fiber-reinforced composite member and method for producing structure using same
JP5276817B2 (ja) 2007-09-12 2013-08-28 矢崎総業株式会社 金属接合体、金属接合方法、及び、金属接合装置
US7810875B2 (en) 2007-10-05 2010-10-12 Mark Von Edward Genaddi Gerisch Structural pan-chassis stabilization system
GB0813883D0 (en) 2008-07-30 2008-09-03 Henrob Ltd Joining apparatus and method
US20100083481A1 (en) 2008-10-08 2010-04-08 Gm Global Technology Operations, Inc. Method for attaching magnesium panels using self-piercing rivet
US20110170983A1 (en) * 2010-01-14 2011-07-14 Backyard Leisure Holdings, Inc. Playset fastener
US8474158B2 (en) 2010-01-21 2013-07-02 K-2 Corporation Molded snowshoe with compound deck
CA2803949C (en) * 2010-06-25 2015-10-20 Omg, Inc. Hidden fastener formed in situ during attachment of sheathing onto a support member
US9023455B2 (en) * 2013-01-30 2015-05-05 Ford Global Technologies, Llc Method of making reinforced composite articles with reduced fiber content in local areas and articles made by the method
US8826510B1 (en) * 2013-02-15 2014-09-09 Ford Global Technologies, Llc Method of making assemblies including reinforced composite parts with pre-formed rivet receiving buttons and articles made by the method

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105538695A (zh) * 2014-10-24 2016-05-04 丰田自动车株式会社 连接元件的方法
CN105538695B (zh) * 2014-10-24 2017-09-22 丰田自动车株式会社 连接元件的方法
CN110248798A (zh) * 2017-02-09 2019-09-17 中车青岛四方机车车辆股份有限公司 用于将部件连接至纤维复合结构的连接元件
CN110481061A (zh) * 2019-09-17 2019-11-22 中国航发沈阳发动机研究所 一种纤维增强复合材料的穿孔方法、消音板及其声衬

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