CN110901103A - Manufacturing method of low-cost modular composite material forming tool - Google Patents

Manufacturing method of low-cost modular composite material forming tool Download PDF

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CN110901103A
CN110901103A CN201911166145.8A CN201911166145A CN110901103A CN 110901103 A CN110901103 A CN 110901103A CN 201911166145 A CN201911166145 A CN 201911166145A CN 110901103 A CN110901103 A CN 110901103A
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tooling
composite material
manufacturing
profile
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CN110901103B (en
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贾彩霞
王乾
李志歆
许朋
梁禄忠
关振
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Shenyang Aerospace University
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C33/00Moulds or cores; Details thereof or accessories therefor
    • B29C33/38Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
    • B29C33/3842Manufacturing moulds, e.g. shaping the mould surface by machining
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Manufacturing & Machinery (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

一种低成本模块化复合材料成型工装制造方法,所属工装制造技术领域,制作步骤包含:(1)工装框架的制作,(2)工装型面背衬的制作,(3)工装型面配合面的制作,(4)工装型面的制作,(5)工装型面的粘贴;本发明方法可以省略母模的制造过程,以少量的工装框架结构配合多种不同型面轮廓的工装型面,通过材料的铺叠与堆积、固化和加工以完成复合材料工装的制造、更换及更正,适用于具有高型面及尺寸精度要求的小批量复合材料产品研发阶段的成型工装制造过程,能够大幅度节省研发成本,缩短研发周期。A low-cost modular composite material forming tooling manufacturing method belongs to the technical field of tooling manufacturing. (4) making the tooling profile, (5) pasting the tooling profile; the method of the present invention can omit the manufacturing process of the master mold, and use a small amount of tooling frame structure to match a variety of tooling profiles with different profile profiles, The manufacturing, replacement and correction of composite tooling are completed through material layup and accumulation, curing and processing. It is suitable for the manufacturing process of forming tooling in the research and development stage of small-batch composite products with high profile and dimensional accuracy requirements. Save R&D costs and shorten R&D cycle.

Description

Manufacturing method of low-cost modular composite material forming tool
Technical Field
The invention belongs to the technical field of tool manufacturing, and particularly relates to a manufacturing method of a low-cost modular composite material forming tool.
Background
The composite material product usually adopts aluminum, high-strength steel, invar steel, carbon fiber composite material and the like as the preferred materials of the forming tool, and the problems of heat efficiency, temperature uniformity, operability and the like are considered, and most of the composite material product mainly adopts a frame type structure. With the requirements of the application field on the profile precision and the size precision of composite material products and the continuous improvement of the manufacturing efficiency of the composite material products, the traditional metal mold has the problems of large thermal expansion coefficient, heavy weight, slow response and the like, and the traditional metal mold can not meet the development of the composite material industry gradually as a mold material; compared with the composite material tool, the composite material tool has the advantages of good thermal expansion performance matching, low density, small heat capacity, certain repairability and the like, and is increasingly applied to the manufacturing process of composite material products.
However, the conventional composite material tooling generally adopts tooling prepreg for manufacturing, and although a set of female die can be used for manufacturing a plurality of sets of composite material tooling, the requirement of a large-scale manufacturing process of composite material products can be met, high material cost and manufacturing cost can be generated, and the tooling is not suitable for manufacturing a forming tooling in a development stage of small-scale composite material products with high dimensional precision requirements.
Therefore, the invention provides a low-cost modular composite material forming tool manufacturing method, which is suitable for the forming tool manufacturing process in the research and development stage of small-batch composite material products with high profile and dimensional accuracy requirements, and can greatly save research and development cost and shorten the research and development period.
Disclosure of Invention
In order to solve the technical problems, the invention provides a method for manufacturing a low-cost modular composite material molding tool, which can omit the manufacturing process of a female die, match tool profiles with various profiles and contours by a small number of tool frame structures, and complete the manufacturing, replacing and correcting of a composite material tool through the material stacking, accumulation, solidification and processing. The method can quickly realize the manufacturing process of the composite material forming tool, is suitable for the development stage of small-batch composite material products with high requirements on precision, and comprises the following steps:
step 1: adopting a fixed connection method of riveting or screwing a matched gasket, combining the frame base materials into a frame structure through connecting pieces such as angle pieces or tee joints, and reserving an assembling hole or an embedded assembling bolt on one side of the frame close to the molded surface of the tool, namely finishing the manufacture of the tool frame 1;
step 2: machining a backing substrate into lining plates, wherein one side of each lining plate is provided with a cambered surface with a certain curvature, the other side of each lining plate is a straight surface and can be connected with a tool frame 1 through corner pieces, and the lining plates form a tool profile backing according to the distribution form of the tool frame 1, so that the manufacturing of a tool profile backing 2 is completed;
and step 3: matching surface base materials matched with the arc surface of the tool profile backing 2 are connected with one side of the arc surface of each lining plate through corner pieces, a plurality of matching surface base materials are spliced to form a tool profile matching surface 3, and a layer of non-porous isolating film is laid on the matching surface, so that the manufacturing of the tool profile matching surface 3 is completed; the composite material molding tool is shown in a schematic diagram in fig. 1;
and 4, step 4: sequentially laying a vacuum bag and a nonporous isolation film on the surface of the nonporous isolation film, laying or accumulating mold plastics on the nonporous isolation film to prepare a tool profile blank, curing and molding by adopting a vacuum bag pressing or autoclave molding process after packaging, and processing to a tool theoretical profile according to a tool digital model to finish the manufacturing of a tool profile 4;
and 5: sticking a layer of double-sided adhesive film on the fitting surface 3 of the tool profile, placing the tool profile 4 which completes the machining process of the theoretical profile of the tool on the double-sided adhesive film, and ensuring no gap between the tool profile 4 and the fitting surface 3 of the tool profile, namely completing the manufacture of the low-cost modular composite material forming tool;
the manufacturing method of the low-cost modular composite material forming tool comprises the following steps:
in the step 1, the frame base material is a carbon fiber fabric reinforced thermosetting resin-based composite material plate or tube, the compression strength is more than or equal to 550MPa, the bending strength is more than or equal to 820MPa, and the long-term use temperature is higher than the curing temperature of a composite material product;
in the step 2, the backing substrate is a carbon fiber fabric reinforced thermosetting resin-based composite material plate, the compression strength is more than or equal to 550MPa, and the long-term use temperature is higher than the curing temperature of a composite material product;
in the step 3, the base material on the matching surface is a carbon fiber fabric reinforced thermosetting resin-based composite material plate, the bending strength is more than or equal to 820MPa, the modulus is more than or equal to 60GPa, and the long-term use temperature is higher than the curing temperature of a composite material product;
in the step 3, when the matched surface substrates are spliced, a gap of 0.8-1.0 mm needs to be reserved between the adjacent substrates, and the matched surface profile of the tool formed by splicing the substrates with a plurality of matched surfaces is close to the profile of the tool;
in the step 4, the size of the vacuum bag is not less than 2 times of the area of the molded surface of the tool;
in the step 4, the molding compound comprises a sheet molding compound or/and a bulk molding compound, wherein the reinforcing phase is chopped carbon fibers or recycled carbon fiber fabric, and the matrix phase is high-temperature-resistant epoxy resin;
in the step 4, the packaging is to wholly coat the tool profile blank by adopting a vacuum bag;
in the step 5, the double-sided adhesive film is a high-temperature-resistant adhesive with a carrier, and the long-term use temperature of the double-sided adhesive film is higher than the curing temperature of the composite material product.
Compared with the prior art, the low-cost modular composite material forming tool manufacturing method has the beneficial effects that:
the molding compound containing chopped carbon fibers or recycled carbon fiber fabrics is used as a tool profile material, and the material and manufacturing cost is far lower than that of a tool prepreg used in the prior art;
the manufacturing of the tool frame can be completed through the combination of the composite material plates or the composite material pipes, the universality is strong, and the material and manufacturing cost is far lower than that of the traditional composite material forming tool frame;
the manufacturing method does not need a female die, and the processing difficulty of the molding compound cured material is lower than that of the tool prepreg cured material, so that the manufacturing link is reduced, and the manufacturing period is shortened;
the packaging and curing mode of the tool profile blank solves the problem of poor air tightness of the traditional composite material forming tool, and the combination and disassembly mode of the tool profile and the tool profile matching surface is simple and easy to implement;
the manufacturing process of the composite material forming tool with different profiles can be realized through the replacement of the tool profile backing, the tool profile matching surface and the tool profile, the tool profile is easy to correct and maintain, and the tool has the advantage of convenience in subsequent maintenance.
Drawings
Fig. 1 is a schematic view of a composite material molding tool assembly according to the present invention: 1-tool frame, 2-tool profile backing, 3-tool profile matching surface and 4-tool profile.
Detailed Description
The invention discloses key technical points including a combination form of a composite material forming tool, a tool profile backing, a tool profile matching surface, material selection, a connection mode, a forming method and the like in the manufacturing, replacing and correcting processes of a tool profile.
The present invention will be further described with reference to specific examples, but the present invention is not limited to these examples.
A manufacturing method of a low-cost modular composite material forming tool comprises the following steps:
step 1: riveting a composite material square tube (DS1207.3) to form a tool frame 1 through a tee joint, and reserving an assembling hole on one side, close to the tool profile, of the tool frame 1;
step 2: machining a composite material plate (DS1207.3) to form a lining plate with a curvature arc surface on one side and a connection with a tool frame through a corner piece on the other side, wherein the lining plates form a tool profile backing 2 according to the distribution form of the tool frame 1;
and step 3: connecting a composite material plate (DS1207.3) with one side of the cambered surface of each lining plate through a corner piece, combining a plurality of plates into a tool profile matching surface 3, wherein the clearance between the plates is
Figure BDA0002287503020000031
In order to avoid the damage of the matching surface caused by the high-temperature expansion of the base material, a pressure sensitive adhesive tape (FLASHBREAKER1) is pasted at the gap, and a layer of non-porous isolating membrane (WL5200) is laid on the matching surface 3 of the tool profile;
and 4, step 4: sequentially laying a vacuum bag (IPPLONDPT1000) and a nonporous isolation film (WL5200) on the nonporous isolation film to ensure that the nonporous isolation film, the vacuum bag and the nonporous isolation film are laid smoothly without folds, laying a carbon fiber sheet molding compound (DS1209.5) to prepare a tool profile blank, integrally coating and packaging by adopting an autoclave molding process, curing and molding, and processing to a tool profile 4 according to a tool profile model;
and 5: pasting a double-sided tape (Airhold1CBS) on the tool profile matching surface 3, placing the tool profile 4 on the tool profile matching surface 3, ensuring no clearance between the tool profile 4 and the tool profile matching surface 3, and finishing the manufacturing process of the low-cost modular composite material molding tool; the composite material molding tool is schematically combined as shown in fig. 1.

Claims (9)

1.一种低成本模块化复合材料成型工装制造方法,包含如下步骤:1. A method for manufacturing a low-cost modular composite material forming tool, comprising the following steps: 步骤1:采用铆接或螺接配合垫片的固定连接方法,将框架基材通过角片或三通等连接件组合成框架结构,并在框架上贴近工装型面的一侧预留出装配孔或预埋装配螺栓,即完成工装框架的制造;Step 1: Using the fixed connection method of riveting or screwing with gaskets, the frame base material is combined into a frame structure through connectors such as corner pieces or tee, and an assembly hole is reserved on the side of the frame close to the tooling profile. Or pre-embedding assembly bolts, that is, to complete the manufacture of the tooling frame; 步骤2:将背衬基材通过机械加工成一侧具有一定曲率弧面,另一侧为直面并可以通过角片与工装框架相连接的衬板,若干衬板按照工装框架分布形式组成工装型面背衬,即完成工装型面背衬的制造;Step 2: The backing substrate is machined into a liner with a certain curvature arc on one side and a straight surface on the other side that can be connected to the tooling frame through corner pieces. Several linings are distributed according to the tooling frame to form a tooling profile. Backing, that is, to complete the manufacture of the tooling surface backing; 步骤3:采用与工装型面背衬弧面相匹配的配合面基材,通过角片与各衬板弧面一侧相连接,若干配合面基材拼接形成工装型面配合面,并在配合面上铺叠一层无孔隔离膜,即完成工装型面配合面的制造;Step 3: Use the mating surface base material that matches the arc surface of the backing of the tooling profile, connect it with one side of the arc surface of each liner through the corner piece, and splicing several mating surface substrates to form the mating surface of the tooling profile, and on the mating surface Lay a layer of non-porous isolation film on the top to complete the manufacture of the matching surface of the tooling surface; 步骤4:在无孔隔离膜表面依次铺叠一层真空袋和一层无孔隔离膜,在其上铺叠或堆积模塑料制成工装型面坯料,封装后采用真空袋压或热压罐成型工艺固化成型,依据工装数模加工至工装理论型面,即完成工装型面的制造;Step 4: Lay a layer of vacuum bag and a layer of non-porous isolation film on the surface of the non-porous isolation film in turn, lay or stack molding compound on it to make a tooling profile blank, and use a vacuum bag or autoclave after packaging. The molding process is solidified and formed, and the tooling is processed to the theoretical profile of the tooling according to the numerical model of the tooling, that is, the manufacture of the tooling profile is completed; 步骤5:在工装型面配合面上粘贴一层双面胶膜,将完成工装理论型面加工过程的工装型面置于其上,确保工装型面与工装型面配合面之间无间隙,即完成低成本模块化复合材料成型工装的制造。Step 5: Paste a layer of double-sided adhesive film on the matching surface of the tooling surface, and place the tooling surface that has completed the theoretical tooling surface processing process on it to ensure that there is no gap between the tooling surface and the matching surface of the tooling surface. That is, the manufacture of low-cost modular composite molding tooling is completed. 2.根据权利要求1所述的一种低成本模块化复合材料成型工装制造方法,其特征在于,所述的步骤1中,框架基材为碳纤维织物增强热固性树脂基复合材料板或管,压缩强度≥550MPa,弯曲强度≥820MPa,长期使用温度大于复合材料产品的固化温度。2. The method for manufacturing a low-cost modular composite material forming tool according to claim 1, wherein in the step 1, the frame base material is a carbon fiber fabric reinforced thermosetting resin matrix composite material plate or tube, and the compressed The strength is ≥550MPa, the bending strength is ≥820MPa, and the long-term use temperature is higher than the curing temperature of the composite product. 3.根据权利要求1所述的一种低成本模块化复合材料成型工装制造方法,其特征在于,所述的步骤2中,背衬基材为碳纤维织物增强热固性树脂基复合材料板,压缩强度≥550MPa,长期使用温度大于复合材料产品的固化温度。3. The method for manufacturing a low-cost modular composite material forming tool according to claim 1, wherein in the step 2, the backing base material is a carbon fiber fabric reinforced thermosetting resin matrix composite material board, and the compressive strength ≥550MPa, the long-term use temperature is greater than the curing temperature of composite products. 4.根据权利要求1所述的一种低成本模块化复合材料成型工装制造方法,其特征在于,所述的步骤3中,配合面基材为碳纤维织物增强热固性树脂基复合材料板,弯曲强度≥820MPa,模量≥60GPa,长期使用温度大于复合材料产品的固化温度。4. The method for manufacturing a low-cost modular composite material molding tool according to claim 1, wherein in the step 3, the mating surface base material is a carbon fiber fabric reinforced thermosetting resin matrix composite material board, and the bending strength is ≥820MPa, modulus ≥60GPa, long-term use temperature is higher than the curing temperature of composite products. 5.根据权利要求1所述的一种低成本模块化复合材料成型工装制造方法,其特征在于,所述的步骤3中,配合面基材拼接时,相邻基材间需留0.8mm~1.0mm的间隙,若干配合面基材拼接形成的工装型面配合面轮廓接近于工装型面轮廓。5 . The method for manufacturing a low-cost modular composite material molding tool according to claim 1 , wherein, in the step 3, when the mating surface substrates are spliced, 0.8mm~0.8mm to With a gap of 1.0mm, the contour of the tooling surface mating surface formed by the splicing of several mating surface substrates is close to the contour of the tooling surface. 6.根据权利要求1所述的一种低成本模块化复合材料成型工装制造方法,其特征在于,所述的步骤4中,真空袋的尺寸不小于工装型面面积的2倍。6 . The method for manufacturing a low-cost modular composite material forming tool according to claim 1 , wherein, in the step 4, the size of the vacuum bag is not less than twice the surface area of the tool. 7 . 7.根据权利要求1所述的一种低成本模块化复合材料成型工装制造方法,其特征在于,所述的步骤4中,模塑料包括片状模塑料或/和团状模塑料,其中,增强相为短切碳纤维或回收碳纤维织物,基体相为耐高温环氧树脂。7. The method for manufacturing a low-cost modular composite material forming tool according to claim 1, wherein in the step 4, the molding compound comprises sheet molding compound or/and bulk molding compound, wherein, The reinforcing phase is chopped carbon fiber or recycled carbon fiber fabric, and the matrix phase is high temperature resistant epoxy resin. 8.根据权利要求1所述的一种低成本模块化复合材料成型工装制造方法,其特征在于,所述的步骤4中,封装是采用真空袋将工装型面坯料进行整体包覆。8 . The method for manufacturing a low-cost modular composite material molding tool according to claim 1 , wherein, in the step 4, the encapsulation is to use a vacuum bag to wrap the tool profile blank as a whole. 9 . 9.根据权利要求1所述的一种低成本模块化复合材料成型工装制造方法,其特征在于,所述的步骤5中,双面胶膜为带载体耐高温胶黏剂,长期使用温度大于复合材料产品的固化温度。9 . The method for manufacturing a low-cost modular composite material molding tooling according to claim 1 , wherein in the step 5, the double-sided adhesive film is a high-temperature resistant adhesive with a carrier, and the long-term use temperature is greater than The curing temperature of the composite product.
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113771386A (en) * 2021-09-27 2021-12-10 沈阳航空航天大学 A manufacturing method of composite parts forming tool suitable for wet forming process
CN115179568A (en) * 2022-06-20 2022-10-14 成都飞机工业(集团)有限责任公司 Rib forming die for RFI liquid forming reinforced wall plate and preparation method
CN118061405A (en) * 2024-03-15 2024-05-24 成都飞机工业(集团)有限责任公司 A 3D printing composite mold and manufacturing method

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6012883A (en) * 1997-05-06 2000-01-11 The Boeing Company Hybrid lay-up tool
CA2592592A1 (en) * 2004-12-30 2006-07-06 Airbus Espana, S.L. Hybrid tooling for the curing of composite pieces
CN101396852A (en) * 2007-09-27 2009-04-01 通用电气公司 Wind turbine blade molds
CN103568161A (en) * 2013-10-08 2014-02-12 天津东汽风电叶片工程有限公司 Method for machining megawatt wind turbine blade mould
CN203864033U (en) * 2014-05-09 2014-10-08 浙江华荣航空装备有限公司 Frame-type forming tooling for airplane composite material component
CN104608400A (en) * 2010-06-14 2015-05-13 兰博基尼汽车公开有限公司 Mould made of a composite material, as well as master and process for its manufacturing
CN105459296A (en) * 2015-12-23 2016-04-06 中国电子科技集团公司第五十四研究所 Light-weight die for high-precision large-sized antenna for radio astronomy and manufacturing method thereof
WO2017123575A1 (en) * 2016-01-11 2017-07-20 Anthony Jerry Hybrid lay-up mold
CN207432830U (en) * 2017-10-23 2018-06-01 固瑞特模具(太仓)有限公司 Compound carbon fiber heating wind-powered blade mold
CN108263497A (en) * 2016-12-31 2018-07-10 郑州吉田专利运营有限公司 Carbon fiber fabric composite vehicle frame and preparation method thereof
CN109501312A (en) * 2018-11-26 2019-03-22 中国商用飞机有限责任公司北京民用飞机技术研究中心 A kind of composite material mould and its application method of modularized design
CN209738315U (en) * 2018-11-26 2019-12-06 中国商用飞机有限责任公司北京民用飞机技术研究中心 A Modular Design Composite Mold

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6012883A (en) * 1997-05-06 2000-01-11 The Boeing Company Hybrid lay-up tool
CA2592592A1 (en) * 2004-12-30 2006-07-06 Airbus Espana, S.L. Hybrid tooling for the curing of composite pieces
CN101396852A (en) * 2007-09-27 2009-04-01 通用电气公司 Wind turbine blade molds
CN104608400A (en) * 2010-06-14 2015-05-13 兰博基尼汽车公开有限公司 Mould made of a composite material, as well as master and process for its manufacturing
CN103568161A (en) * 2013-10-08 2014-02-12 天津东汽风电叶片工程有限公司 Method for machining megawatt wind turbine blade mould
CN203864033U (en) * 2014-05-09 2014-10-08 浙江华荣航空装备有限公司 Frame-type forming tooling for airplane composite material component
CN105459296A (en) * 2015-12-23 2016-04-06 中国电子科技集团公司第五十四研究所 Light-weight die for high-precision large-sized antenna for radio astronomy and manufacturing method thereof
WO2017123575A1 (en) * 2016-01-11 2017-07-20 Anthony Jerry Hybrid lay-up mold
CN108263497A (en) * 2016-12-31 2018-07-10 郑州吉田专利运营有限公司 Carbon fiber fabric composite vehicle frame and preparation method thereof
CN207432830U (en) * 2017-10-23 2018-06-01 固瑞特模具(太仓)有限公司 Compound carbon fiber heating wind-powered blade mold
CN109501312A (en) * 2018-11-26 2019-03-22 中国商用飞机有限责任公司北京民用飞机技术研究中心 A kind of composite material mould and its application method of modularized design
CN209738315U (en) * 2018-11-26 2019-12-06 中国商用飞机有限责任公司北京民用飞机技术研究中心 A Modular Design Composite Mold

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113771386A (en) * 2021-09-27 2021-12-10 沈阳航空航天大学 A manufacturing method of composite parts forming tool suitable for wet forming process
CN115179568A (en) * 2022-06-20 2022-10-14 成都飞机工业(集团)有限责任公司 Rib forming die for RFI liquid forming reinforced wall plate and preparation method
CN118061405A (en) * 2024-03-15 2024-05-24 成都飞机工业(集团)有限责任公司 A 3D printing composite mold and manufacturing method

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