CN110561841A - 一种可承受集中载荷的蜂窝板及其加工方法 - Google Patents

一种可承受集中载荷的蜂窝板及其加工方法 Download PDF

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CN110561841A
CN110561841A CN201910878539.XA CN201910878539A CN110561841A CN 110561841 A CN110561841 A CN 110561841A CN 201910878539 A CN201910878539 A CN 201910878539A CN 110561841 A CN110561841 A CN 110561841A
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thin plate
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李耀宗
王宏兵
王志明
李亚林
胡志明
王帆
邓时成
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KUNCHUAN ELECTRONIC EQUIPMENT CO Ltd YUNNAN
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    • B32B1/00—Layered products having a non-planar shape
    • 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 shape; Layered products comprising a layer having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • 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 shape; Layered products comprising a layer having particular features of form
    • B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
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    • 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
    • B32B33/00—Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class
    • 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
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    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
    • E04C2/36—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels
    • E04C2/365—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels by honeycomb structures
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04F—FINISHING WORK ON BUILDINGS, e.g. STAIRS, FLOORS
    • E04F13/00—Coverings or linings, e.g. for walls or ceilings
    • E04F13/07—Coverings or linings, e.g. for walls or ceilings composed of covering or lining elements; Sub-structures therefor; Fastening means therefor
    • E04F13/08—Coverings or linings, e.g. for walls or ceilings composed of covering or lining elements; Sub-structures therefor; Fastening means therefor composed of a plurality of similar covering or lining elements
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04F—FINISHING WORK ON BUILDINGS, e.g. STAIRS, FLOORS
    • E04F13/00—Coverings or linings, e.g. for walls or ceilings
    • E04F13/07—Coverings or linings, e.g. for walls or ceilings composed of covering or lining elements; Sub-structures therefor; Fastening means therefor
    • E04F13/08—Coverings or linings, e.g. for walls or ceilings composed of covering or lining elements; Sub-structures therefor; Fastening means therefor composed of a plurality of similar covering or lining elements
    • E04F13/0866—Coverings or linings, e.g. for walls or ceilings composed of covering or lining elements; Sub-structures therefor; Fastening means therefor composed of a plurality of similar covering or lining elements composed of several layers, e.g. sandwich panels or layered panels

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Abstract

本发明公开了一种可承受集中载荷的蜂窝板及其加工方法，包括覆盖于蜂窝板的上表面的上薄板、覆盖于蜂窝板的下表面的下薄板以及位于上薄板和下薄板之间的蜂窝芯，在蜂窝芯上设置有多个通孔，在通孔内设置有垫块。其加工方法包括先粗略加工出上薄板和下薄板的外形轮廓、将下薄板放在工作平台上，并在下薄板的上表面均匀涂上粘接剂、然后将垫块和蜂窝芯依次放在下薄板的上表面所需位置、再然后在上薄板的下表面均匀涂上粘接剂并放在蜂窝芯上、在上薄板上施加压力、根据需要在垫块的位置加工出连接孔，用于连接固定所述上薄板与下薄板。本发明的具有普通蜂窝板的优点，又具有可承受集中载荷的优点，可应用于电动汽车、建筑装饰、工业装备等领域。

Description

一种可承受集中载荷的蜂窝板及其加工方法
技术领域
本发明涉及一种蜂窝板及其加工方法，尤其是一种可承受集中载荷的蜂窝板及其加工方法。
背景技术
蜂窝板属轻量化结构，具有成本低、质量轻、易运输施工和节能环保等特点，在建筑、装饰、包装等行业被广泛应用。
但是，现有的普通蜂窝板内部为纯蜂窝芯，易导致其不能承受较大的集中载荷的缺点，使得其应用受到一定的限制。
针对目前的现状，有必要设计一种可承受集中载荷的蜂窝板，使其在具备普通蜂窝板轻量化的优点的基础上，能够承受较大集中载荷，解决其应用受限的问题。
发明内容
为了解决普通蜂窝板能够承受较大集中载荷的问题，本发明提出一种有效的改进结构，即在普通蜂窝板上需要承受较大集中载荷的位置，增加实心垫块。
本发明技术方案为：
一种可承受集中载荷的蜂窝板，包括覆盖于所述蜂窝板的上表面的上薄板、覆盖于所述蜂窝板的下表面的下薄板以及位于所述上薄板和下薄板之间的蜂窝芯，其特征在于：在所述蜂窝芯上设置有多个通孔，在所述通孔内设置有垫块，该垫块的厚度与所述蜂窝芯的厚度相同。进一步，在所述下薄板的上表面和上薄板的下表面均匀涂覆的粘接剂，用于将所述上薄板、下薄板、蜂窝芯以及垫块粘接成为可承受集中载荷的蜂窝板。
一种可承受集中载荷的蜂窝板的加工方法：
先根据实际需要粗略加工出上薄板和下薄板的外形轮廓；将下薄板放在工作平台上，并在下薄板的上表面均匀涂上粘接剂；然后将垫块和蜂窝芯依次放在下薄板的上表面所需位置，所述垫块的放置位置与通孔相对应；然后在上薄板的下表面均匀涂上粘接剂，并放在蜂窝芯上；接着在上薄板上施加压力，保证各零件与粘接剂充分接触，等待粘接完成；粘接完成后，将整块蜂窝板放在一定的夹具上，利用数控切割的方式加工出精确轮廓，并根据实际需要在垫块的位置加工出连接孔，用于连接固定所述上薄板与下薄板。
本发明的有益效果是：
通过在普通蜂窝板之间需要承受较大集中载荷的位置，增加实心垫块用于连接或承重，解决了普通蜂窝板不能承受集中载荷的缺点，同时具备普通蜂窝板轻量化的优点。由于具有普通蜂窝板的优点，又具有可承受集中载荷的优点，可应用于电动汽车、建筑装饰、工业装备等领域。
附图说明
图1是本发明的可承受集中载荷的蜂窝板的拆解图；
图2是本发明的可承受集中载荷的蜂窝板的方形通孔内设置实心垫块的示意图；
图3是本发明的可承受集中载荷的蜂窝板的圆形通孔内设置实心垫块的示意图；
图4是本发明的可承受集中载荷的蜂窝板的蜂窝芯和实心垫块放置在下薄板上的示意图；
图5是本发明的可承受集中载荷的蜂窝板粘接完成后的示意图；
图6是本发明的可承受集中载荷的蜂窝板完成连接孔加工的示意图；
图7是本发明的可承受集中载荷的蜂窝板完整结构的局部剖视图；
图8是本发明的可承受集中载荷的蜂窝板加工工艺流程图。
具体实施方式
下面通过具体实施例对本发明作进一步的详述。
一种可承受集中载荷的蜂窝板，包括覆盖于所述蜂窝板的上表面的上薄板1、覆盖于所述蜂窝板的下表面的下薄板2以及位于所述上薄板1和下薄板2之间的蜂窝芯3，其特征在于：在所述蜂窝芯3上设置有多个通孔5，在所述通孔5内设置有垫块4，该垫块4的厚度与所述蜂窝芯3的厚度相同。
进一步地，在所述每个通孔5内设置一个垫块4。
优选地，所述通孔5呈方孔或者圆孔形状。
优选地，所述垫块4呈方形或者圆形。
优选地，还包括在所述下薄板2的上表面和上薄板1的下表面均匀涂覆的粘接剂6，用于将所述上薄板1、下薄板2、蜂窝芯3以及垫块4粘接成为可承受集中载荷的蜂窝板。
优选地，所述垫块4选用轻量化可负荷材料的实心垫块。
优选地，所述实心垫块选用金属材料的垫块。
具体加工时的工艺流程可以是：
先根据实际需要粗略加工出上薄板1和下薄板2的外形轮廓。将下薄板2放在工作平台上，并在下薄板2的上表面均匀涂上粘接剂6；然后将垫块4和蜂窝芯3依次放在下薄板2的上表面所需位置，所述垫块4的放置位置与通孔5相对应；然后在上薄板1的下表面均匀涂上粘接剂6，并放在蜂窝芯3上；接着在上薄板1上施加压力，保证各零件与粘接剂6充分接触，等待粘接完成；粘接完成后，将整块蜂窝板放在一定的夹具上，利用数控切割的方式加工出精确轮廓，并根据实际需要在垫块4的位置加工出连接孔，用于连接固定所述上薄板1与下薄板2。
本发明工作原理是，在需要连接或集中承重的位置，在蜂窝芯3设置通孔5，在所述通孔5内设置有垫块4，并按照上述的制作工艺流程，完成本发明一种可承受集中载荷的蜂窝板的制作。该可承受集中载荷的蜂窝板不仅具备普通蜂窝板轻量化的优点，还具备在需要的位置承受较大集中载荷的优点。

Claims (7)

1.一种可承受集中载荷的蜂窝板，包括覆盖于所述蜂窝板的上表面的上薄板(1)、覆盖于所述蜂窝板的下表面的下薄板(2)以及位于所述上薄板(1)和下薄板(2)之间的蜂窝芯(3)。其特征在于：在所述蜂窝芯(3)上设置有多个通孔(5)，在所述通孔(5)内设置有垫块(4)，该垫块(4)的厚度与所述蜂窝芯(3)的厚度相同。
2.根据权利要求1所述的可承受集中载荷的蜂窝板，其特征在于：在所述每个通孔(5)内设置一个垫块(4)。
3.根据权利要求1至2任一项所述的可承受集中载荷的蜂窝板，其特征在于：所述通孔(5)呈方孔或者圆孔形状；所述垫块(4)为方形或者圆形。
4.根据权利要求3所述的可承受集中载荷的蜂窝板，其特征在于：还包括在所述下薄板(2)的上表面和上薄板(1)的下表面均匀涂覆的粘接剂(6)，用于将所述上薄板(1)、下薄板(2)、蜂窝芯(3)以及垫块(4)粘接成为可承受集中载荷的蜂窝板。
5.根据权利要求3所述的可承受集中载荷的蜂窝板，其特征在于：所述垫块(4)选用轻量化可负荷材料的实心垫块。
6.根据权利要求5所述的可承受集中载荷的蜂窝板，其特征在于：所述的实心垫块选用金属材料的垫块。
7.一种可承受集中载荷的蜂窝板的加工方法，其特征在于：
先根据实际需要粗略加工出上薄板(1)和下薄板(2)的外形轮廓；
将下薄板(2)放在工作平台上，并在下薄板(2)的上表面均匀涂上粘接剂(6)；
然后将垫块(4)和蜂窝芯(3)依次放在下薄板(2)的上表面所需位置，所述垫块(4)的放置位置与通孔(5)相对应；
然后在上薄板(1)的下表面均匀涂上粘接剂(6)，并放在蜂窝芯(3)上；
接着在上薄板(1)上施加压力，保证各零件与粘接剂(6)充分接触，等待粘接完成；
粘接完成后，将整块蜂窝板放在一定的夹具上，利用数控切割的方式加工出精确轮廓，并根据实际需要在垫块(4)的位置加工连接孔，用于连接固定所述上薄板(1)与下薄板(2)。
CN201910878539.XA 2019-09-17 2019-09-17 一种可承受集中载荷的蜂窝板及其加工方法 Withdrawn CN110561841A (zh)

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CN1378504A (zh) * 1999-10-08 2002-11-06 密尔沃基合成物公司 使用预固化的强化芯层的嵌板及其制造方法
WO2005032304A1 (fr) * 2003-10-08 2005-04-14 Luhao Leng Panneau avec noyaux a nid d'abeille en papier utilisable comme dessus de table
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CN202106602U (zh) * 2011-05-12 2012-01-11 都江堰金祥装饰工程有限公司 高抗剥离强度的蜂窝板
WO2012090518A1 (ja) * 2010-12-29 2012-07-05 ジェイ・バス株式会社 組合せハニカムピース構造によるハニカムパネル
CN210706305U (zh) * 2019-09-17 2020-06-09 云南昆船电子设备有限公司 一种可承受集中载荷的蜂窝板

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1378504A (zh) * 1999-10-08 2002-11-06 密尔沃基合成物公司 使用预固化的强化芯层的嵌板及其制造方法
WO2005032304A1 (fr) * 2003-10-08 2005-04-14 Luhao Leng Panneau avec noyaux a nid d'abeille en papier utilisable comme dessus de table
CN101468533A (zh) * 2007-12-25 2009-07-01 上海卫星工程研究所 航天器镁合金镶嵌件板
WO2012090518A1 (ja) * 2010-12-29 2012-07-05 ジェイ・バス株式会社 組合せハニカムピース構造によるハニカムパネル
CN202106602U (zh) * 2011-05-12 2012-01-11 都江堰金祥装饰工程有限公司 高抗剥离强度的蜂窝板
CN210706305U (zh) * 2019-09-17 2020-06-09 云南昆船电子设备有限公司 一种可承受集中载荷的蜂窝板

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