CN111016301A - 纤维复合材料连接孔周边的增强及其制备方案 - Google Patents
纤维复合材料连接孔周边的增强及其制备方案 Download PDFInfo
- Publication number
- CN111016301A CN111016301A CN202010025434.2A CN202010025434A CN111016301A CN 111016301 A CN111016301 A CN 111016301A CN 202010025434 A CN202010025434 A CN 202010025434A CN 111016301 A CN111016301 A CN 111016301A
- Authority
- CN
- China
- Prior art keywords
- connecting hole
- composite material
- periphery
- conical head
- plate
- 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.)
- Granted
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 32
- 239000000835 fiber Substances 0.000 title claims abstract description 27
- 238000002360 preparation method Methods 0.000 title claims abstract description 10
- 238000000034 method Methods 0.000 title claims description 17
- 230000003014 reinforcing effect Effects 0.000 title claims description 12
- 239000000463 material Substances 0.000 claims abstract description 14
- 230000002787 reinforcement Effects 0.000 claims abstract description 11
- 238000003825 pressing Methods 0.000 claims description 22
- 238000005520 cutting process Methods 0.000 claims description 6
- 239000006260 foam Substances 0.000 claims description 3
- 239000002184 metal Substances 0.000 claims description 3
- 230000002093 peripheral effect Effects 0.000 claims description 3
- 239000012783 reinforcing fiber Substances 0.000 claims description 3
- 239000004033 plastic Substances 0.000 claims description 2
- 229920003023 plastic Polymers 0.000 claims description 2
- 238000010008 shearing Methods 0.000 claims 2
- 238000010438 heat treatment Methods 0.000 abstract description 4
- 238000005553 drilling Methods 0.000 description 9
- 239000003733 fiber-reinforced composite Substances 0.000 description 4
- 239000011347 resin Substances 0.000 description 3
- 229920005989 resin Polymers 0.000 description 3
- 229920000049 Carbon (fiber) Polymers 0.000 description 2
- 239000004917 carbon fiber Substances 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 238000004080 punching Methods 0.000 description 2
- 229920002430 Fibre-reinforced plastic Polymers 0.000 description 1
- 239000011324 bead Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000011151 fibre-reinforced plastic Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Images
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
- B32B1/00—Layered products having a non-planar shape
-
- 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
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
-
- 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
-
- 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
- B29C70/545—Perforating, cutting or machining during or after moulding
-
- 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
- B32B3/266—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 characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12
-
- 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
-
- 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
- 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
- B32B7/08—Interconnection of layers by mechanical means
-
- 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
- B32B2250/00—Layers arrangement
- B32B2250/20—All layers being fibrous or filamentary
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Moulding By Coating Moulds (AREA)
- Laminated Bodies (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
Abstract
本发明公开了一种纤维复合材料连接孔周边的增强及其制备方案,包括叠加铺层中连接孔是采用锥头轴杆穿孔,连接孔沿复合材料板材边沿方向部分的丝束剪断后再补强,锥头轴杆穿孔过程中采用左右转动和压板振动相结合的方案,锥头轴杆穿孔完成后在其中放置套筒,之后加温固化的技术方案,锥头轴杆穿孔使纤维丝束向连接孔周边两侧分开并加强在两侧,连接孔周边的丝束向开口处延伸,使受力分散,而丝束开口处受上下丝层的不同方向的丝层和基材固定,减少了产生疲劳及裂缝的可能性,还可减少连接孔数量,也减少了耗材,延长了部件的使用寿命,省去了维修、更换部件耗费的时间及费用,使安全得到保障。
Description
技术领域
本发明涉及一种以纤维增强的复合材料连接孔的制造,尤其是一种以纤维增强,塑料或金属为基材的复合材料板材连接孔周边増强及制备技术。
背景技术
现有以纤维增强的复合材料板材的机械连接方式,主要是采用钻孔,通过孔洞进行铆接或螺栓连接。例如,公告号为CN205086002U 的中国实用新型专利,公开了“一种蜂窝碳纤维复合材料连接件”,解决现有工业机器人末端连接件重量大,增加了额外负载,有效载荷利用率低,应用成本高的问题,进而提出一种蜂窝碳纤维复合材料连接件。其通过上碳纤维层、蜂窝层、下碳纤维层、两组铆接衬环之间通过多个空心铆钉铆接。 此种通过铆接方式或其它的螺栓连接方式,都不能解决孔洞周边容易产生疲劳及出现裂缝的问题,因钻孔方式将孔洞部分的纤维丝除去、经过孔洞部分的丝束全部断掉,增加了钻孔周边丝束的受力,导致孔洞周边容易产生疲劳及容易出现裂缝的问题,上述问题造成维修、更换部件而耗费时间,增加费用及造成安全隐患。
发明内容
为了克服现有技术中以纤维增强的复合材料板材,包括平面板材、曲面板材,板材中连接孔的钻孔方式使孔洞周边容易产生疲劳及裂缝问题,本发明提供一种采用锥头轴杆穿孔方案,使纤维丝在穿孔过程中向孔洞两侧分开并加强在两侧,纤维丝的丝束由孔洞两侧形成开口并向开口处延伸,受力也从孔洞边向开口处延伸分散,开口处受上下丝层不同方向的丝层和基材的固定,减少了产生疲劳及裂缝的可能性。连接孔周边产生了叠层凸缘,通过在复合材料板材一面采用模具设置凹槽,控制叠层凸缘直径与厚度,有凸缘的一面与主体结构或框架相连接,另一面是平面,对产品几乎无影响。本发明解决了钻孔的孔洞周边容易产生疲劳及裂缝的缺陷问题,增强了连接孔周边的承受力,延长了部件的使用寿命,省去了维修、更换部件需耗费时间及增加的费用,使安全得到保障。
本发明纤维复合材料连接孔周边的增强及其制备方案,包括纤维增强,塑料或金属为基材的复合材料板材,板材包括平面板材、曲面板材,其特征在于所述的复合材料板材的连接孔(1)周边的加强方案,加强方案是板材的纤维丝层铺层过程中开始进行,是纤维丝层预浸或涂抹基材后进行叠加铺层,铺层至板材边沿(5)附近设置连接孔(1)的位置,将沿板材边沿(5)方向相临两个连接孔(1)中间距离位置,按连接孔(1)的直径宽度丝束剪断,再在剪断位置(15)补强,在设置的各个连接孔(1)位置通过锥头轴杆(12)进行穿孔,穿孔完成后,在孔中放置套筒(6),在后续的固化中,套筒(6)使连接孔(1)不变形。
上述的剪断位置(15)补强,补强丝层条(11)采用宽度与剪断宽度相同,长度是两个相临的连接孔(1)的丝束开口处(3)的中间距离长度。
上述的锥头轴杆(12)穿孔,包括单个穿孔,多个一组穿孔,多组穿孔。
上述的锥头轴杆(12)穿孔,锥头轴杆(12)可左右转动,还包括附加压板(13),压板(13)中有压板孔(14),通过压板(13)振动和锥头轴杆(12)左右转动增加穿孔周边丝束蠕变移动。
上述的锥头轴杆(12)穿孔,在穿孔过程中,孔洞周边的丝束产生挤压凸起,采用在模具上设置圆型凹槽,圆型凹槽的直径宽度等于连接孔两端丝束(2)的丝束开口处(3)之间的距离,凹槽的直径宽度和厚度根据产品情况自由设定。
上述的复合材料板材不但边沿设置连接孔(1),中部也可以设置连接孔(1),中部的连接孔(1)采用将锥头轴杆(12)设置在模具上,在铺层中进行穿孔,并且用高弹性泡沫块施压周围,逐渐至板材边沿(5)附近,使穿孔涉及的丝束蠕变和滑动,保持板面中部平整。
上述的复合材料板材的叠加铺层,还包括采用绕丝机,铺带机进行铺层。
本发明的有益效果是,本发明纤维增强的复合材料板材连接孔采用锥头轴杆穿孔,使纤维丝向孔洞两侧分开并加强在两侧,开口由连接孔周边向外延伸至初始开口处,受力也从连接孔周边向外延伸至初始开口处逐渐分散,而开口部分受不同方向的上下丝层和基材固定,减少了产生疲劳及裂缝的可能性。本发明解决了钻孔式连接孔容易产生疲劳及裂缝的缺陷问题,增强了穿孔式连接孔周边的承受力,而且可将原钻孔方式的双排连接孔改为穿孔式单排连接孔,减少了铆钉或螺栓,也减轻了该金属材料连接件的的重量,本发明延长了部件的使用寿命,不容易产生疲劳及裂缝,省去了复合材料板材钻孔式连接孔的维修、更换部件耗费的时间及费用,安全得到保障,钻孔式的板材因连接孔周边的疲劳问题而采取的增加铺层补强,本发明的铺层还可减少,铺层减少也就减少了材料和减轻了重量。
附图说明
下面结合附图和实施例对本发明进一步说明。
图1为本发明示意图;
图2为多轴向连接孔周边平面示意图;
图3为锥头轴杆侧面示意图;
图4为板材边沿方向两连接孔间剪断丝束位置示意图;
图5为板材边沿方向两连接孔间剪断处补强示意图;
图6为穿孔压条示意图。
图中1. 连接孔,2. 丝束,3. 开口处,4.开口的最大宽度,5. 板材的边沿,6. 套筒,7. 边沿方向0°丝束,8.+45°丝束,9. 90°丝束,10. -45°丝束,11. 补强丝束条,12. 锥头轴杆, 13. 压板,14.压板孔,15. 剪断位置。
具体实施方式
【实施例1】
纤维复合材料连接孔周边的增强及其制备方案,包括平面板材和曲面板材,板材包括叠加铺层中连接孔1是采用锥头轴杆12穿孔,连接孔1周边沿复合材料板材边沿5方向部分丝束2剪断及补强,锥头轴杆12穿孔过程中采用左右转动和压板13振动,锥头轴杆12穿孔完成后在其中放置套筒,之后加温固化成复合材料。制备过程首先是铺层,铺层逐层叠加,包括采用各丝层涂抹基材树脂或预浸丝层或预浸布进行铺层,在铺层中,在板材的边沿5方向设置为边沿方向0°丝束7, 每两个边沿方向的连接孔1的中间位置,按连接孔1直径宽度的部分丝束2剪断,在剪断位置15处补强,补强的丝层条11宽度与剪断宽度相同,长度是两个连接孔1的中间位置除去连接孔1两端开口处3位置的长度。完成铺层后采用锥头轴杆12进行穿孔,在穿孔的过程中锥头轴杆12可以左右转动,锥头轴杆12还套装在压板13的压板孔14中,压板13的压板孔14是按连接孔1的位置设置的,压板13可以振动,通过锥头轴杆12左右转动和压板13振动产生丝束2蠕变移动,将各方向丝层,包括设置为边沿方向0°丝束7的轴向、设置为90°丝束9的轴向、设置为+45°丝束8的轴向、设置为- 45°丝束10的轴向的丝束2从中分开至两侧,形成周边增强丝束2的连接孔1,丝束2开口的最大宽度4一侧的宽度小于开口处3一侧的宽度,连接孔1的周边增强丝束2产生叠加凸起,采用在模具上设置凹槽控制凸缘的宽度与厚度,凹槽设置为圆型,圆型凹槽的直径宽度等于连接孔两端丝束2的丝束开口处3之间的距离,圆型凹槽的厚度由內向外逐渐减薄,圆型凹槽中芯部位留有锥头穿孔的孔洞,有凸缘的一面与主体结构或框架相连接,连接几乎对产品无连接影响,另一面表面平整,不影响产品表面外观平整。锥头轴杆12可设置为单个或多个一组或多组操作,根据产品情况设定,还包括在连接孔1中放置套筒6,套筒6的型状根据将采用的连接部件型状设定,采用套筒6的方案是保证复合材料板材在后续加温固化中连接孔1不变形。锥头轴杆12在穿孔过程中,丝束2向两侧分开,在分开过程中,丝束2距离板材边沿5的距离比较短,这部分穿孔位置的丝束2容易向连接孔1处退缩、板材中部在距离连接孔较远的部分还可放置部分压重物,锥头轴杆12在穿孔过程中,控制适当速度及力度,达到不影响板材中部丝层过快退缩,在丝束2向两侧分开的开口处3至孔边沿形成了开口间隙,在铺层和穿孔过程中,放置套筒6之前补充基材树脂,套筒6中可以设置溢流孔洞,便于多余的树脂流出,后续加温固化后,将板材边沿剪齐,剪除因丝束2退缩产生的不平整边沿部分。
【实施例2】
复合材料板材除了边沿有连接孔1,中部还有连接孔1的情况下,采用在模具上设置锥头轴杆12,再在模具上铺层和设置连接孔1, 在板材边沿5距离连接孔1较远的部分放置部分压重物,让板材边5距离连接孔1较近的部分容易回缩,采用边穿孔边施压的方式,施压采用高弹性泡沫块,施压使丝束2产生蠕变、滑动、回缩。边沿部分的连接孔1可以参照上述实施例1方案原理进行。
【实施例3】
复合材料板材铺层采用绕丝机、铺带机进行铺层,连接孔1周边增强的技术方案的设置参照上述实施例1、上述实施例2的技术方案原理进行。
Claims (7)
1.纤维复合材料连接孔周边的增强及其制备方案,包括纤维增强,塑料或金属为基材的复合材料板材,板材包括平面板材、曲面板材,其特征在于所述的复合材料板材的连接孔(1)周边的加强方案,加强方案是板材的纤维丝层铺层过程中开始进行,是纤维丝层预浸或涂抹基材后进行叠加铺层,铺层至板材边沿(5)附近设置连接孔(1)的位置,将沿板材边沿(5)方向相临两个连接孔(1)中间距离位置,按连接孔(1)的直径宽度丝束剪断,再在剪断位置(15)补强,在设置的各个连接孔(1)位置通过锥头轴杆(12)进行穿孔,穿孔完成后,在孔中放置套筒(6),在后续的固化中,套筒(6)使连接孔(1)不变形。
2.根据权利要求1所述的纤维复合材料连接孔周边的增强及其制备方案,其特征在于,所述剪断位置(15)补强,补强丝层条(11)采用宽度与剪断宽度相同,长度是两个相临的连接孔(1)的丝束开口处(3)的中间距离长度。
3.根据权利要求1所述的纤维复合材料连接孔周边的增强及其制备方案,其特征在于,所述锥头轴杆(12)穿孔,包括单个穿孔,多个一组穿孔,多组穿孔。
4.根据权利要求1所述的纤维复合材料连接孔周边的增强及其制备方案,其特征在于,所述锥头轴杆(12)穿孔,锥头轴杆(12)可左右转动,还包括附加压板(13),压板(13)中有压板孔(14),通过压板(13)振动和锥头轴杆(12)左右转动增加穿孔周边丝束蠕变移动。
5.根据权利要求1所述的纤维复合材料连接孔周边的增强及其制备方案,其特征在于,所述锥头轴杆(12)穿孔,在穿孔过程中,孔洞周边的丝束产生挤压凸起,采用在模具上设置圆型凹槽,圆型凹槽的直径宽度等于连接孔两端丝束(2)的丝束开口处(3)之间的距离,凹槽的直径宽度和厚度根据产品情况自由设定。
6.根据权利要求1所述的纤维复合材料连接孔周边的增强及其制备方案,其特征在于,所述复合材料板材不但边沿设置连接孔(1),中部也可以设置连接孔(1),中部的连接孔(1)采用将锥头轴杆(12)设置在模具上,在铺层中进行穿孔,并且用高弹性泡沫块施压周围,逐渐至板材边沿(5)附近,使穿孔涉及的丝束蠕变和滑动,保持板面中部平整。
7.根据权利要求1所述的纤维复合材料连接孔周边的增强及其制备方案,其特征在于,所述复合材料板材的叠加铺层,还包括采用绕丝机,铺带机进行铺层。
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010025434.2A CN111016301B (zh) | 2020-01-10 | 2020-01-10 | 纤维复合材料连接孔周边的增强及其制备方案 |
PCT/CN2020/000302 WO2021138751A1 (zh) | 2020-01-10 | 2020-12-15 | 纤维复合材料连接孔周边的增强及其制备方案 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010025434.2A CN111016301B (zh) | 2020-01-10 | 2020-01-10 | 纤维复合材料连接孔周边的增强及其制备方案 |
Publications (2)
Publication Number | Publication Date |
---|---|
CN111016301A true CN111016301A (zh) | 2020-04-17 |
CN111016301B CN111016301B (zh) | 2023-11-17 |
Family
ID=70198790
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202010025434.2A Active CN111016301B (zh) | 2020-01-10 | 2020-01-10 | 纤维复合材料连接孔周边的增强及其制备方案 |
Country Status (2)
Country | Link |
---|---|
CN (1) | CN111016301B (zh) |
WO (1) | WO2021138751A1 (zh) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2021138751A1 (zh) * | 2020-01-10 | 2021-07-15 | 杭州友凯船艇有限公司 | 纤维复合材料连接孔周边的增强及其制备方案 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH1052191A (ja) * | 1996-08-09 | 1998-02-24 | Sekisui Plastics Co Ltd | 浮沈式フロート |
WO2007068847A1 (fr) * | 2005-12-15 | 2007-06-21 | Chomarat Composites | Complexe textile destine a etre utilise comme couche de renfort pour la fabrication de pieces composites, et procede de fabrication d'un tel complexe |
CN105431286A (zh) * | 2013-07-29 | 2016-03-23 | 波音公司 | 具有通过受控纤维铺放生产的孔图案的复合材料层压板 |
US20170291253A1 (en) * | 2016-04-06 | 2017-10-12 | Honda Motor Co., Ltd. | Hybrid structures for joining of metals and continuous fiber materials |
CN110549638A (zh) * | 2019-09-06 | 2019-12-10 | 杭州友凯船艇有限公司 | 纤维增强塑料基材的复合材料防脆断的技术方案 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2763881B1 (fr) * | 1997-05-30 | 2000-09-29 | Peguform France | Procede et dispositif pour realiser in-situ une ouverture traversante dans un panneau a structure composite de type sandwich a ame alveolaire |
CN102935721B (zh) * | 2012-11-13 | 2015-08-19 | 中国科学院宁波材料技术与工程研究所 | 一种纤维复合材料开孔制件的补强片设计及补强方法 |
CN102922834B (zh) * | 2012-11-13 | 2015-10-28 | 中国科学院宁波材料技术与工程研究所 | 一种热塑性纤维复合材料开孔制件的补强片设计及补强方法 |
CN103042698B (zh) * | 2012-11-13 | 2015-02-18 | 中国科学院宁波材料技术与工程研究所 | 一种复合材料连接结构 |
CN103925267B (zh) * | 2014-03-19 | 2016-09-07 | 刘龙权 | 一种复合材料与金属连接结构及形成所述连接结构的方法 |
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 |
CN111016301B (zh) * | 2020-01-10 | 2023-11-17 | 杭州友凯船艇有限公司 | 纤维复合材料连接孔周边的增强及其制备方案 |
-
2020
- 2020-01-10 CN CN202010025434.2A patent/CN111016301B/zh active Active
- 2020-12-15 WO PCT/CN2020/000302 patent/WO2021138751A1/zh active Application Filing
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH1052191A (ja) * | 1996-08-09 | 1998-02-24 | Sekisui Plastics Co Ltd | 浮沈式フロート |
WO2007068847A1 (fr) * | 2005-12-15 | 2007-06-21 | Chomarat Composites | Complexe textile destine a etre utilise comme couche de renfort pour la fabrication de pieces composites, et procede de fabrication d'un tel complexe |
CN105431286A (zh) * | 2013-07-29 | 2016-03-23 | 波音公司 | 具有通过受控纤维铺放生产的孔图案的复合材料层压板 |
US20170291253A1 (en) * | 2016-04-06 | 2017-10-12 | Honda Motor Co., Ltd. | Hybrid structures for joining of metals and continuous fiber materials |
CN110549638A (zh) * | 2019-09-06 | 2019-12-10 | 杭州友凯船艇有限公司 | 纤维增强塑料基材的复合材料防脆断的技术方案 |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2021138751A1 (zh) * | 2020-01-10 | 2021-07-15 | 杭州友凯船艇有限公司 | 纤维复合材料连接孔周边的增强及其制备方案 |
Also Published As
Publication number | Publication date |
---|---|
CN111016301B (zh) | 2023-11-17 |
WO2021138751A1 (zh) | 2021-07-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2206597B1 (en) | Method and apparatus for manufacturing composite spars | |
EP3668725B1 (en) | Rim fibre architecture of a composite wheel | |
EP2441571B1 (en) | Proces for manufacturing a composite component | |
US6510961B1 (en) | Integrally-reinforced braided tubular structure and method of producing the same | |
US20130139961A1 (en) | Dual-skin structures | |
JP2012016948A (ja) | 複合構造物の構成部材を製造する方法 | |
US6406580B1 (en) | Method for manufacturing composite parts | |
EP1775106B1 (en) | Manufacturing method for a curved object of composite material and curved object obtained thereby | |
US10407159B2 (en) | Reinforced blade and spar | |
WO2006118448A1 (en) | Method for the manufacturing of a hollow fiber reinforced structural member | |
JP2008069972A6 (ja) | 滑り要素、滑り要素を製造するための方法および装置 | |
JP4309748B2 (ja) | 航空機に用いられるfrp製窓枠用のドライプリフォーム | |
CN111016301A (zh) | 纤维复合材料连接孔周边的增强及其制备方案 | |
JP2015214151A (ja) | 航空機構造用の複合材料部品を製造する方法 | |
US5091029A (en) | Method of manufacturing a unitary, multi-legged helicopter rotor flexbeam made solely of composite materials | |
US10668672B2 (en) | Radially extending composite structures | |
AU2016219741B2 (en) | A method and system for fabricating a composite structure | |
EP0167120B1 (en) | A process for preparing a fiber-reinforced plastic structure having branching points | |
KR20160120270A (ko) | 서로 교차하는 중공 보강 구조체들을 생산하기 위한 방법 | |
JP5342171B2 (ja) | 繊維強化プラスチック製段付きパイプ及びその製造方法 | |
CN116176002A (zh) | 一种增强单向碳纤维复合材料纤维间强度的快速制备方法 | |
US20160016365A1 (en) | Method of fabricating a spar for a blade, and a method of fabricating a blade | |
JP3299617B2 (ja) | 繊維強化樹脂材 | |
EP3321178B1 (en) | Reinforced propeller blade and spar | |
CN116113539A (zh) | 用于风力涡轮机叶片的翼梁帽的混合拉挤板 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |