CN106003876A - 一种防拉铆撕裂的复合材料及敷设方法 - Google Patents
一种防拉铆撕裂的复合材料及敷设方法 Download PDFInfo
- Publication number
- CN106003876A CN106003876A CN201610329777.1A CN201610329777A CN106003876A CN 106003876 A CN106003876 A CN 106003876A CN 201610329777 A CN201610329777 A CN 201610329777A CN 106003876 A CN106003876 A CN 106003876A
- Authority
- CN
- China
- Prior art keywords
- prepreg
- unidirectional
- fabric
- composite
- fiber
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 42
- 238000000034 method Methods 0.000 title claims abstract description 29
- 239000000835 fiber Substances 0.000 claims abstract description 63
- 239000004744 fabric Substances 0.000 claims abstract description 49
- 239000000463 material Substances 0.000 claims abstract description 6
- 239000003365 glass fiber Substances 0.000 claims description 8
- 229920006231 aramid fiber Polymers 0.000 claims description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims 4
- 229910052799 carbon Inorganic materials 0.000 claims 4
- 239000004760 aramid Substances 0.000 claims 2
- 229920003235 aromatic polyamide Polymers 0.000 claims 2
- 239000002184 metal Substances 0.000 abstract description 22
- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 238000009434 installation Methods 0.000 abstract description 5
- 238000003780 insertion Methods 0.000 abstract description 4
- 230000037431 insertion Effects 0.000 abstract description 4
- 229920000049 Carbon (fiber) Polymers 0.000 description 22
- 239000004917 carbon fiber Substances 0.000 description 22
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 22
- 238000012360 testing method Methods 0.000 description 15
- 238000010586 diagram Methods 0.000 description 4
- 238000007585 pull-off test Methods 0.000 description 4
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
Classifications
-
- 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
- B32B5/02—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 structural features of a fibrous or filamentary layer
- B32B5/12—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 structural features of a fibrous or filamentary layer characterised by the relative arrangement of fibres or filaments of different layers, e.g. the fibres or filaments being parallel or perpendicular to each other
-
- 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
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/02—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by a sequence of laminating steps, e.g. by adding new layers at consecutive laminating stations
-
- 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
- B32B5/22—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/582—Tearability
- B32B2307/5825—Tear resistant
Landscapes
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
本发明涉及材料领域,特别涉及一种防拉铆撕裂的复合材料及敷设方法,本发明提供防拉铆撕裂的复合材料,由下到上依次为一层或多层纤维织物以及多层单向纤维预浸料,所述每层纤维织物的经度方向和单向纤维预浸料的纤维方向与预设水平面成不同角度敷设,借助于本发明的技术方案,解决了现有技术中由于盲插安装金属垫片导致的生产进度和质量受到严重影响的问题,能够不用加装金属片,直接采用抽芯铆钉连接两层或多层板,同时不会产生由于抽芯铆钉的膨胀而撕裂复合材料孔口、从而造成连接强度降低、甚至连接失效。
Description
技术领域
本发明涉及材料领域,特别涉及一种防拉铆撕裂的复合材料及敷设方法。
背景技术
复合材料板构件采用抽芯铆钉连接两层或多层板时通常需要在抽芯铆钉的膨胀端加装金属垫片,以保护抽芯铆钉膨胀端的复合材料板孔口不被撕裂。
一组件由大长径比碳纤维方管和金属U形件组成,需将两个构件采用铆接的方式连接在一起,由于碳纤维方管是大长径比的封闭构件,无法采用压铆工艺连接成型,只能采用拉铆工艺,即抽芯铆钉铆接连接成型,在开放的空间进行这种装配工艺是较为成熟的技术,然而在狭小或封闭的空间,由于无法或不便安装金属垫片,这种装配工艺便不能使用或效率很低。
按照传统的碳纤维板的铆接要求,需要在碳纤维背部加装金属垫片,但是由于操作空间狭小,采用专用夹具在铆钉孔位置预先用胶粘接金属垫片的方法加装,由于粘接金属垫片的数量很多,工作量非常大,生产效率低,而且由于盲插安装,在胶固化后,仍容易出现金属垫片掉落现象,生产进度和质量受到严重影响。
发明内容
为了解决现有技术中盲插安装时金属垫片掉落现象,生产进度和质量受到严重影响的问题,本发明提供了一种防拉铆撕裂的复合材料及敷设方法。
本发明提供一种防拉铆撕裂的复合材料,由下到上依次为一层或多层纤维织物以及多层单向纤维预浸料,所述每层纤维织物的经度方向和单向纤维预浸料的纤维方向与预设水平面成不同角度敷设。
本发明还提供了一种防拉铆撕裂的复合材料的敷设方法,包括以下步骤:
分别确定一层或多层纤维织物预浸料以及多层单向纤维预浸料的敷设层数和方向,其中,所述每层纤维织物的经度方向和单向纤维预浸料的纤维方向与预设水平面成不同角度;
按照所述层数和方向将一层或多层纤维织物预浸料以及多层单向纤维预浸料在模具上进行敷设,并进行压实。
本发明有益效果如下:
本发明提供的复合材料中每层纤维织物和单向纤维预浸料织物均具有各自的方向,解决了现有技术中由于盲插安装时金属垫片掉落导致的生产进度和质量受到严重影响的问题,能够不用加装金属片,直接采用抽芯铆钉连接两层或多层板(复合材料板/复合材料板,或复合材料板/金属板),同时不会产生由于抽芯铆钉的膨胀而撕裂复合材料孔口、从而造成连接强度降低、甚至连接失效。
附图说明
图1为本发明产品实施例的防拉铆撕裂的复合材料的结构示意图;
图2为本发明方法实施例的防拉铆撕裂的复合材料和金属U形件的连接结构示意图;
图3为本发明方法实施例的防拉铆撕裂的复合材料的敷设方法流程图;
图4为本发明试验例中拉脱试验用碳纤维板的结构示意图;
图5为本发明试验例中拉剪试验用碳纤维板的结构示意图;
图6为本发明试验例中拉脱试样的俯视图;
图7为本发明试验例中拉剪试样的剖视图。
具体实施方式
为了解决现有技术中盲插安装时金属垫片掉落现象,生产进度和质量受到严重影响的问题,本发明提供了一种防拉铆撕裂的复合材料及敷设方法,以下结合附图以及实施例,对本发明进行进一步详细说明。应当理解,此处所描述的具体实施例仅仅用以解释本发明,并不限定本发明。
产品实施例
根据本发明的实施例,提供了一种防拉铆撕裂的复合材料,图2是本发明产品实施例的防拉铆撕裂的复合材料的结构示意图,如图2所示,根据本发明产品实施例的防拉铆撕裂的复合材料,包括由下到上依次为一层或多层纤维织物以及多层单向纤维预浸料,所述每层纤维织物的经度方向和单向纤维预浸料的纤维方向与预设水平面成不同角度敷设,以下对本发明实施例的各个模块进行详细的说明。
具体地,本发明产品实施例的防拉铆撕裂的复合材料包括包括由下到上的1层纤维织物以及16层单向纤维预浸料,壁厚为2.75mm(2.45mm~2.75mm),图2中的第i层表示第一层与第n层之间的任意一层,n=17。铺层顺序为[0°/+45°/-45°/0°/0°/90°/0°/-45°/0°/+45°/0°/0°/90°/0°/0°/-45°/+45°],0°方向为管件长度方向。
所述纤维织物包括碳纤维织物、玻璃纤维织物、芳纶纤维织物;所述单向纤维预浸料包括单向碳纤维预浸料、单向玻璃纤维预浸料、单向芳纶纤维预浸料等。
优选地,所述单向碳纤维为碳纤维T700,表1为碳纤维T700的基本性能。
表1
本发明产品实施例的防拉铆撕裂的复合材料(也可称为碳纤维方管)可以与金属U形件拼装,用抽芯铆钉铆接成型,而不需要加装金属垫片,同时不会产生由于抽芯铆钉的膨胀而撕裂复合材料孔口、从而造成连接强度降低、甚至连接失效,图2为本发明方法实施例的防拉铆撕裂的复合材料和金属U形件的连接结构示意图。
方法实施例
根据本发明的实施例,提供了一种防拉铆撕裂的复合材料的敷设方法,图3为本发明方法实施例的防拉铆撕裂的复合材料的敷设方法流程图,如图3所示,根据本发明方法实施例的防拉铆撕裂的复合材料的敷设方法包括如下处理:
步骤302,分别确定一层或多层纤维织物预浸料以及多层单向纤维预浸料的敷设层数和方向,其中,所述每层纤维织物的经度方向和单向纤维的纤维方向与预设水平面成不同角度。
具体地,分别确定一层或多层纤维织物预浸料以及多层单向纤维预浸料的敷设层数和方向包括以下步骤:按照防拉铆撕裂的复合材料的强度和刚度要求分别确定一层或多层纤维织物预浸料以及多层单向纤维预浸料的敷设层数和方向。
优选地,确定纤维织物预浸料以及多层单向纤维预浸料的敷设层数包括以下步骤:所述复合材料包括由下到上的1层纤维织物预浸料以及16层单向纤维预浸料。
更加优选地,确定纤维织物预浸料以及多层单向纤维预浸料的铺层顺序为[0°/+45°/-45°/0°/0°/90°/0°/-45°/0°/+45°/0°/0°/90°/0°/0°/-45°/+45°]。
所述纤维织物预浸料包括碳纤维织物预浸料、玻璃纤维织物预浸料、芳纶纤维织物预浸料,优选为厚度为0.3mm的碳纤维织物预浸料(成型后厚度);所述单向纤维预浸料包括单向碳纤维预浸料、单向玻璃纤维预浸料、单向芳纶纤维预浸料,优选为0.15mm的单向碳纤维预浸料(成型后厚度)。
本发明方法实施例中的纤维织物预浸料经固化成型后为产品实施例中的纤维织物,方法实施例中的单向纤维预浸料经固化成型后为产品实施例中的单向纤维。
步骤304,按照所述层数和方向将一层或多层纤维织物预浸料以及多层单向纤维预浸料预浸料在模具上进行敷设,并进行压实。
为了更好的说明方法实施例,给出实例1。
实例1为图2所示防拉铆撕裂的复合材料的制备方法,具备包括以下步骤:
将裁剪好的碳纤维织物预浸料和单向碳纤维预浸料在芯模上进行敷设,在敷设过程中需要随时压实,并且按照以下顺序进行敷设:
[0°/+45°/-45°/0°/0°/90°/0°/-45°/0°/+45°/0°/0°/90°/0°/0°/-45°/+45°]。
试验例
按照本发明方法实施例的方法制备两种碳纤维复合材料板,图4为本发明试验例中拉脱试验用碳纤维板的结构示意图,尺寸为20×30mm,厚度为2.75mm;图5为本发明试验例中拉剪试验用碳纤维板的结构示意图,尺寸为36mm×135mm,厚度为2.75mm。
图6本发明试验例中拉脱试样的结构示意图,图7本发明试验例中拉剪试样的结构示意图,用φ4不锈钢抽芯铆钉按图6和图7装配成拉脱试样和拉剪试样。拉脱试样共做10件,其中5件在抽芯铆钉的膨胀端安装φ4金属垫片铆接,另5件不安装金属垫片直接铆接;拉剪试样共做10件,其中5件在抽芯铆钉的膨胀端安装φ4金属垫片铆接,另5件不安装金属垫片直接铆接;
将20组试样分别进行拉脱试验和拉剪试验,测试铆钉破坏所需的拉脱力和拉剪力,表2为拉脱试验和拉剪试验的原始试验数据。
表2
由表2数据看到:碳纤维复合材料板背部有、无金属垫片的拉剪力均值差为0.016KN;背部有、无金属垫片的拉脱力均值差为0.018KN;它们的差值很小,在通常情况下,二者结构形式可以互换,其拉脱力和拉剪力均满足使用性能要求。
显然,本领域的技术人员可以对本发明进行各种改动和变型而不脱离本发明的精神和范围。这样,倘若本发明的这些修改和变型属于本发明权利要求及其等同技术的范围之内,则本发明也意图包含这些改动和变型在内。
Claims (10)
1.一种防拉铆撕裂的复合材料,其特征在于,由下到上依次为一层或多层纤维织物以及多层单向纤维预浸料,所述每层纤维织物的经度方向和单向纤维预浸料的纤维方向与预设水平面成不同角度敷设。
2.根据权利要求1所述的防拉铆撕裂的复合材料,其特征在于,包括由下到上的1层纤维织物以及16层单向纤维预浸料。
3.根据权利要求2所述的防拉铆撕裂的复合材料,铺层顺序为[0°/+45°/-45°/0°/0°/90°/0°/-45°/0°/+45°/0°/0°/90°/0°/0°/-45°/+45°]。
4.根据权利要求1所述的防拉铆撕裂的复合材料,其特征在于,所述纤维织物包括碳纤维织物、玻璃纤维织物、芳纶纤维织物。
5.根据权利要求1所述的防拉铆撕裂的复合材料,其特征在于,所述单向纤维预浸料包括单向碳纤维预浸料、单向玻璃纤维预浸料、单向芳纶纤维预浸料。
6.一种防拉铆撕裂的复合材料的敷设方法,其特征在于,
分别确定一层或多层纤维织物预浸料以及多层单向纤维预浸料的敷设层数和方向,其中,所述每层纤维织物的经度方向和单向纤维预浸料的纤维方向与预设水平面成不同角度;
按照所述层数和方向将一层或多层纤维织物预浸料以及多层单向纤维预浸料在模具上进行敷设,并进行压实。
7.如权利要求6所述的敷设方法,其特征在于,分别确定一层或多层纤维织物预浸料以及多层单向纤维预浸料的铺设层数和方向具体包括以下步骤:
按照防拉铆撕裂的复合材料的强度和刚度要求分别确定一层或多层纤维织物预浸料以及多层单向纤维预浸料的敷设层数和方向。
8.如权利要求7所述的敷设方法,其特征在于,确定纤维织物预浸料以及多层单向纤维预浸料的敷设层数包括以下步骤:
所述复合材料包括由下到上的1层纤维织物预浸料以及16层单向纤维预浸料。
9.如权利要求7或8所述的敷设方法,其特征在于,确定纤维织物预浸料以及多层单向纤维预浸料的铺层顺序为[0°/+45°/-45°/0°/0°/90°/0°/-45°/0°/+45°/0°/0°/90°/0°/0°/-45°/+45°]。
10.如权利要求6所述的敷设方法,其特征在于,所述纤维织物预浸料包括碳纤维织物预浸料、玻璃纤维织物预浸料、芳纶纤维织物预浸料;所述单向纤维预浸料包括单向碳纤维预浸料、单向玻璃纤维预浸料、单向芳纶纤维预浸料。
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610329777.1A CN106003876A (zh) | 2016-05-18 | 2016-05-18 | 一种防拉铆撕裂的复合材料及敷设方法 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610329777.1A CN106003876A (zh) | 2016-05-18 | 2016-05-18 | 一种防拉铆撕裂的复合材料及敷设方法 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106003876A true CN106003876A (zh) | 2016-10-12 |
Family
ID=57097872
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610329777.1A Pending CN106003876A (zh) | 2016-05-18 | 2016-05-18 | 一种防拉铆撕裂的复合材料及敷设方法 |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106003876A (zh) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108297458A (zh) * | 2018-04-04 | 2018-07-20 | 吉林大学 | 碳纤维复合材料成型及与金属板件粘铆一体化的装置及方法 |
| CN113167217A (zh) * | 2018-12-19 | 2021-07-23 | 通用电气公司 | 具有带有用于销增强的不同的纤维取向的内部支承结构的连结式转子叶片 |
| CN114953514A (zh) * | 2021-02-19 | 2022-08-30 | 河北雷萨重型工程机械有限责任公司 | 起重机及其副起重臂、副起重臂的臂筒及其制作方法 |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4622254A (en) * | 1981-08-31 | 1986-11-11 | Toray Industries, Inc. | Fiber material for reinforcing plastics |
| WO2004078442A1 (en) * | 2003-03-06 | 2004-09-16 | Vestas Wind Systems A/S | Pre-consolidated pre-form and method of pre-consolidating pre-forms |
| WO2005033393A1 (en) * | 2003-09-30 | 2005-04-14 | Fabrics Technologies Llc | Fiber-reinforced thermoplastic composite materials and method of manufacturing the same |
| EP1342544B1 (en) * | 2002-03-08 | 2008-03-12 | Gurit (UK) Limited | Moulding material |
| WO2009031657A1 (ja) * | 2007-09-07 | 2009-03-12 | Toyota Jidosha Kabushiki Kaisha | プリプレグの積層構造 |
| CN104169077A (zh) * | 2012-02-08 | 2014-11-26 | 奎德兰特塑料合成股份公司 | 平面复合材料 |
| CN104228087A (zh) * | 2014-09-01 | 2014-12-24 | 机械科学研究总院先进制造技术研究中心 | 一种复合材料预浸料制备方法 |
-
2016
- 2016-05-18 CN CN201610329777.1A patent/CN106003876A/zh active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4622254A (en) * | 1981-08-31 | 1986-11-11 | Toray Industries, Inc. | Fiber material for reinforcing plastics |
| EP1342544B1 (en) * | 2002-03-08 | 2008-03-12 | Gurit (UK) Limited | Moulding material |
| WO2004078442A1 (en) * | 2003-03-06 | 2004-09-16 | Vestas Wind Systems A/S | Pre-consolidated pre-form and method of pre-consolidating pre-forms |
| WO2005033393A1 (en) * | 2003-09-30 | 2005-04-14 | Fabrics Technologies Llc | Fiber-reinforced thermoplastic composite materials and method of manufacturing the same |
| WO2009031657A1 (ja) * | 2007-09-07 | 2009-03-12 | Toyota Jidosha Kabushiki Kaisha | プリプレグの積層構造 |
| CN104169077A (zh) * | 2012-02-08 | 2014-11-26 | 奎德兰特塑料合成股份公司 | 平面复合材料 |
| CN104228087A (zh) * | 2014-09-01 | 2014-12-24 | 机械科学研究总院先进制造技术研究中心 | 一种复合材料预浸料制备方法 |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108297458A (zh) * | 2018-04-04 | 2018-07-20 | 吉林大学 | 碳纤维复合材料成型及与金属板件粘铆一体化的装置及方法 |
| CN108297458B (zh) * | 2018-04-04 | 2023-05-02 | 吉林大学 | 碳纤维复合材料成型及与金属板件粘铆方法 |
| CN113167217A (zh) * | 2018-12-19 | 2021-07-23 | 通用电气公司 | 具有带有用于销增强的不同的纤维取向的内部支承结构的连结式转子叶片 |
| CN113167217B (zh) * | 2018-12-19 | 2024-06-07 | Lm风力发电公司 | 具有带有用于销增强的不同的纤维取向的内部支承结构的连结式转子叶片 |
| CN114953514A (zh) * | 2021-02-19 | 2022-08-30 | 河北雷萨重型工程机械有限责任公司 | 起重机及其副起重臂、副起重臂的臂筒及其制作方法 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP3166787B1 (en) | Thinwall composites for electronic enclosures and other devices | |
| US11247383B2 (en) | Composite filler | |
| CN103502326A (zh) | 由纤维增强复合材料构成的成形制品 | |
| Nguyen et al. | Experimental and numerical study on the tensile failure behavior of toughened-interlayer composite laminates with automated fiber placement (AFP) induced gap and overlap defects | |
| Růžek et al. | Effect of fatigue loading rate on lifespan and temperature of tailored blank C/PPS thermoplastic composite | |
| CN104302463A (zh) | 用于飞行器发动机的承载结构及其工艺 | |
| CN106003876A (zh) | 一种防拉铆撕裂的复合材料及敷设方法 | |
| US7722944B2 (en) | Piece made of composite material with areas of different thickness | |
| JP2010507530A (ja) | 翼パネル構造 | |
| CN102991031A (zh) | 一种frp板及其生产方法 | |
| Wu et al. | Bending properties and failure behavior of 3D printed fiber reinforced resin T‐beam | |
| WO2008118649A1 (en) | Method for bonding a facing skin to a freeform-fabricated composite core | |
| Asi | Effect of different woven linear densities on the bearing strength behaviour of glass fiber reinforced epoxy composites pinned joints | |
| US8871126B2 (en) | Manufacturing method for trumpet spar and other curved objects | |
| Lin et al. | Transverse tensile properties of laminar unidirectional carbon fiber‐reinforced polymers enhanced with multiscale fiber‐interleaving: experiments and modeling | |
| Attar et al. | Failure analysis of unidirectional polymeric matrix composites with two serial pin loaded-holes | |
| Zhang et al. | Assessment of 3D woven near‐net‐shaped I‐sections for aeronautical applications: Weave design, manufacture, and mechanical properties under multiple loading conditions | |
| Xiaoquan et al. | Effects of hygrothermal environmental conditions on compressive strength of CFRP stitched laminates | |
| CN102416716A (zh) | 带有泡沫夹芯梁的金字塔型点阵芯材及其制备工艺 | |
| Sevkat et al. | The bearing strength of pin loaded woven composites manufactured by vacuum assisted resin transfer moulding and hand lay-up techniques | |
| CN111896352A (zh) | 用于测试泡沫芯材剪切性能的试样、制作方法及测试方法 | |
| Kumar et al. | Modeling and experimental evaluation of geometrically graded multi-material single-lap joints | |
| Lundsgaard-Larsen et al. | Tailoring sandwich face/core interfaces for improved damage tolerance—part II: experiments | |
| Sharma et al. | Effect of core-shell micro-fillers on impact performance and damage progression in bi-directional carbon thermoplastic composites | |
| CN108799267B (zh) | 经由内部叶片将复合板联结的叶槽式接头 |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161012 |
|
| RJ01 | Rejection of invention patent application after publication |