[go: up one dir, main page]

CN107283137A - A kind of moulding technique of structural adhesive bonding part - Google Patents

A kind of moulding technique of structural adhesive bonding part Download PDF

Info

Publication number
CN107283137A
CN107283137A CN201610223917.7A CN201610223917A CN107283137A CN 107283137 A CN107283137 A CN 107283137A CN 201610223917 A CN201610223917 A CN 201610223917A CN 107283137 A CN107283137 A CN 107283137A
Authority
CN
China
Prior art keywords
web
tooling
place
vacuum bag
angle material
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
Application number
CN201610223917.7A
Other languages
Chinese (zh)
Inventor
李士豪
刘秀荣
姜吉明
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Harbin Aircraft Industry Group Co Ltd
Original Assignee
Harbin Aircraft Industry Group Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Harbin Aircraft Industry Group Co Ltd filed Critical Harbin Aircraft Industry Group Co Ltd
Priority to CN201610223917.7A priority Critical patent/CN107283137A/en
Publication of CN107283137A publication Critical patent/CN107283137A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P19/00Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)

Abstract

本发明提供一种结构胶接零件的成型工艺方法,包括以下步骤第一步:先将产品下表面的加强角材(4)放置在工装相对应凹槽进行固定;第二步:然后将产品的缘条(3)放入工装,并用机械加压区域(7)的构型压紧件进行加压固定,保证缘条(3)的位置尺寸;第三步:之后将腹板(2)放在缘条(3)及下表面加强角材上(4),将腹板(2)的上表面加强角材(1)放置在腹板(2)上面相应的位置上,腹板(2)的上表面加强角材(1)的位置由工装定位边条确定;第四步:铺放脱模薄膜、透气毡,安装真空嘴,并糊制真空袋;第五步:真空袋加压;第六步:入炉固化。

The invention provides a molding process method for structural glued parts, which includes the following steps. The first step: first place the reinforcing angle material (4) on the lower surface of the product in the corresponding groove of the tooling for fixing; the second step: then place the reinforcing angle material (4) of the product Put the flange (3) into the tooling, and press and fix it with the configuration pressing parts in the mechanical pressure area (7) to ensure the position and size of the flange (3); the third step: put the web (2) On the edge strip (3) and the lower surface reinforcement angle (4), place the upper surface reinforcement angle (1) of the web (2) on the corresponding position on the top of the web (2), and the upper surface of the web (2) The position of the surface reinforced angle material (1) is determined by the positioning edge of the tooling; the fourth step: laying the release film and air felt, installing the vacuum nozzle, and pasting the vacuum bag; the fifth step: pressurizing the vacuum bag; the sixth step : solidified in the furnace.

Description

一种结构胶接零件的成型工艺方法A molding process method for structural adhesive joint parts

技术领域technical field

本发明属于零件加工领域,具体涉及一种结构胶接零件的成型工艺方法。The invention belongs to the field of parts processing, and in particular relates to a forming process method of structural glued parts.

背景技术Background technique

某型机金属结构胶接零件较多,胶接面积约为整个飞机面积的70%以上。以油箱梁为例,由于其结构复杂,成型方法采用全部机械加压的方式,机械加压工装凭工人手工操作进行加压,压力不均匀,长期入炉高温固化致使工装机械加压压紧件变形,导致胶接质量不稳定及尺寸产生偏移,不能满足设计要求,产品合格率低,严重影响产品质量的稳定性,并且需频繁对工装进行返修,生产效率低下。The metal structure of a certain type of aircraft has many bonding parts, and the bonding area is about 70% of the entire aircraft area. Taking the fuel tank beam as an example, due to its complex structure, the forming method adopts all mechanical pressurization. The mechanical pressurization tooling is pressurized manually by workers, and the pressure is uneven. Long-term high-temperature curing in the furnace causes tooling mechanical pressurization to press the compression parts. Deformation leads to unstable bonding quality and size deviation, which cannot meet the design requirements. The product qualification rate is low, which seriously affects the stability of product quality, and frequent tooling repairs are required, resulting in low production efficiency.

发明内容Contents of the invention

本发明要解决的技术问题:The technical problem to be solved in the present invention:

由于成型工装采用机械加压的结构形式,其不稳定性严重影响了产品的胶接质量。本发明是通过采用新的成型工艺方法,目的是为了提高产品质量的稳定性及产品的合格率,满足设计要求,提高生产效率,降低生产成本。Since the forming tooling adopts a mechanically pressurized structure, its instability seriously affects the bonding quality of the product. The purpose of the invention is to improve the stability of product quality and the pass rate of products by adopting a new molding process method, meet design requirements, improve production efficiency and reduce production cost.

本发明的技术方案:Technical scheme of the present invention:

一种结构胶接零件的成型工艺方法,包括以下步骤A molding process method for structural adhesive parts, comprising the following steps

第一步:先将产品下表面的加强角材4放置在工装相对应凹槽进行固定;The first step: first place the reinforcing angle material 4 on the lower surface of the product in the corresponding groove of the tooling for fixing;

第二步:然后将产品的缘条3放入工装,并用机械加压区域7的构型压紧件进行加压固定,保证缘条3的位置尺寸;Step 2: Then put the edge strip 3 of the product into the tooling, and press and fix it with the configuration pressing parts in the mechanical pressure area 7, so as to ensure the position and size of the edge strip 3;

第三步:之后将腹板2放在缘条3及下表面加强角材上4,将腹板2的上表面加强角材1放置在腹板2上面相应的位置上,腹板2的上表面加强角材1的位置由工装定位边条确定;Step 3: After that, place the web 2 on the edge strip 3 and the lower surface reinforcing angle material 4, place the upper surface reinforcing angle material 1 of the web 2 on the corresponding position above the web 2, and strengthen the upper surface of the web 2 The position of angle material 1 is determined by the positioning edge of the tooling;

第四步:铺放脱模薄膜、透气毡,安装真空嘴,并糊制真空袋;Step 4: Lay out the release film and air felt, install the vacuum nozzle, and paste the vacuum bag;

第五步:真空袋加压;Step 5: Pressurize the vacuum bag;

第六步:入炉固化。Step 6: Curing in the oven.

本发明采用真空袋加压及机械加压相结合的工艺方法,有效的保证了零件的胶接质量。从工艺操作角度上分析,真空袋加压及机械加压相结合的方法比单一机械加压方法更可控,可以用设备检查真空袋的密封程度,并且可以通过设备控制压力,有效降低了工人成型时的操作难度,相比单一机械加压的操作方法,这种方法减少了工人的劳动强度,提高了生产效率,并且有效降低了因工人操作导致的压力不均匀的人为因素造成的缺陷。The invention adopts a process method combining vacuum bag pressurization and mechanical pressurization to effectively ensure the bonding quality of parts. From the perspective of process operation, the method of combining vacuum bag pressurization and mechanical pressurization is more controllable than a single mechanical pressurization method. Equipment can be used to check the degree of sealing of the vacuum bag, and the pressure can be controlled through the equipment, which effectively reduces the number of workers. Compared with the operation method of single mechanical pressing, this method reduces the labor intensity of workers, improves production efficiency, and effectively reduces the defects caused by human factors such as uneven pressure caused by workers' operation.

附图说明Description of drawings

图1为油箱梁产品结构剖面示意图;Figure 1 is a schematic cross-sectional view of the fuel tank beam product structure;

图2为产品在工装上加压区域的分布;Figure 2 shows the distribution of the pressurized area of the product on the tooling;

其中:1为上表面加强角材,2为腹板,3为缘条,4为下表面加强角材,5为胶接面,6为真空袋加压区域,7为机械加压区域。Among them: 1 is the upper surface reinforced angle material, 2 is the web, 3 is the edge strip, 4 is the lower surface reinforced angle material, 5 is the glue joint surface, 6 is the vacuum bag pressurized area, and 7 is the mechanical pressurized area.

具体实施方式detailed description

第一步:先将下表面加强角材4放置在工装相对应凹槽进行固定。Step 1: First, place the lower surface reinforced angle material 4 in the corresponding groove of the tooling for fixing.

第二步:然后将缘条3放入工装,并用机械加压部分7的构型压紧件进行加压固定,保证缘条3的位置尺寸。Step 2: Then put the edge strip 3 into the tooling, and press and fix it with the configuration pressing part of the mechanical pressing part 7, so as to ensure the position and size of the edge strip 3.

第三步:之后将腹板2放在缘条3及下表面加强角材4上,将腹板上表面加强角材1放置在腹板2上面相应的位置上,位置由工装定位边条确定。Step 3: After that, place the web 2 on the edge strip 3 and the lower surface reinforcing angle material 4, place the upper surface reinforcing angle material 1 on the web on the corresponding position on the web 2, and the position is determined by the positioning edge strip of the tooling.

第四步:在组装后的上表面加强角材1和腹板2上面铺放脱模薄膜、透气毡,安装真空嘴,并糊制真空袋。Step 4: Lay a release film and an air felt on the assembled upper surface reinforcing angle material 1 and web 2, install a vacuum nozzle, and paste a vacuum bag.

第五步:抽真空负压,使真空袋对产品产生压力,通过设备检查糊制的真空袋的气密性,确保真空袋没有漏气,并确保真空袋没有架桥现象。Step 5: Vacuum the negative pressure to make the vacuum bag exert pressure on the product, check the airtightness of the pasted vacuum bag through the equipment to ensure that there is no air leakage in the vacuum bag and that there is no bridging phenomenon in the vacuum bag.

第六步:入炉固化。Step 6: Curing in the oven.

Claims (1)

1.一种结构胶接零件的成型工艺方法,其特征在于,包括以下步骤1. A molding process method for structurally bonded parts, characterized in that it comprises the following steps 第一步:先将产品下表面的加强角材(4)放置在工装相对应凹槽进行固定;The first step: first place the reinforcing angle material (4) on the lower surface of the product in the corresponding groove of the tooling for fixing; 第二步:然后将产品的缘条(3)放入工装,并用机械加压区域(7)的构型压紧件进行加压固定,保证缘条(3)的位置尺寸;Step 2: Then put the edge strip (3) of the product into the tooling, and press and fix it with the configuration pressing parts in the mechanical pressure area (7), so as to ensure the position and size of the edge strip (3); 第三步:之后将腹板(2)放在缘条(3)及下表面加强角材上(4),将腹板(2)的上表面加强角材(1)放置在腹板(2)上面相应的位置上,腹板(2)的上表面加强角材(1)的位置由工装定位边条确定;Step 3: After that, place the web (2) on the flange (3) and the lower surface reinforcement angle (4), and place the upper surface reinforcement angle (1) of the web (2) on the web (2) At the corresponding position, the position of the reinforcing angle material (1) on the upper surface of the web (2) is determined by the positioning edge strip of the tooling; 第四步:铺放脱模薄膜、透气毡,安装真空嘴,并糊制真空袋;Step 4: Lay out the release film and air felt, install the vacuum nozzle, and paste the vacuum bag; 第五步:真空袋加压;Step 5: Pressurize the vacuum bag; 第六步:入炉固化。Step 6: Curing in the oven.
CN201610223917.7A 2016-04-12 2016-04-12 A kind of moulding technique of structural adhesive bonding part Pending CN107283137A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610223917.7A CN107283137A (en) 2016-04-12 2016-04-12 A kind of moulding technique of structural adhesive bonding part

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610223917.7A CN107283137A (en) 2016-04-12 2016-04-12 A kind of moulding technique of structural adhesive bonding part

Publications (1)

Publication Number Publication Date
CN107283137A true CN107283137A (en) 2017-10-24

Family

ID=60092900

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610223917.7A Pending CN107283137A (en) 2016-04-12 2016-04-12 A kind of moulding technique of structural adhesive bonding part

Country Status (1)

Country Link
CN (1) CN107283137A (en)

Citations (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0439259A1 (en) * 1990-01-16 1991-07-31 Lord Corporation Improved method for rubber-to-metal bonding
CN101673880A (en) * 2009-10-21 2010-03-17 中国电子科技集团公司第五十四研究所 Method for manufacturing antenna reflecting surface with aluminum skin honeycomb sandwich structure
CN101905528A (en) * 2010-07-16 2010-12-08 沈阳飞机工业(集团)有限公司 Wedge-shaped autoclave forming process of composite material I-shaped section
CN102765198A (en) * 2012-07-13 2012-11-07 中国人民解放军国防科学技术大学 Vacuum assisted molding system of composite and molding method of composite
CN103029307A (en) * 2012-12-12 2013-04-10 江西洪都航空工业集团有限责任公司 Manufacture method of box-shaped structural main beam made from composite material
CN103273665A (en) * 2013-06-14 2013-09-04 沈阳飞机工业(集团)有限公司 Forming technology of square pipe part made of composite material
CN203579263U (en) * 2013-11-25 2014-05-07 德阳汉沣数控机械制造有限公司 Upper rim strip machining tool
CN104149228A (en) * 2014-07-08 2014-11-19 中国电子科技集团公司第二十研究所 Integrated forming die and method for glass fiber reinforced plastic antenna housing
CN104441696A (en) * 2014-09-22 2015-03-25 成都飞机工业(集团)有限责任公司 Manufacture method of special-shaped composite material rib
CN104441631A (en) * 2014-11-10 2015-03-25 沈阳黎明航空发动机(集团)有限责任公司 Manufacturing method of easily worn silicon rubber ring and metal cementing part
CN104626606A (en) * 2015-01-04 2015-05-20 哈尔滨飞机工业集团有限责任公司 Carbon fiber composite material forming tool
CN104691779A (en) * 2015-01-13 2015-06-10 哈尔滨飞机工业集团有限责任公司 Process method for replacement and repair of iron clad of main blade made of composite material
CN104847762A (en) * 2015-05-07 2015-08-19 哈尔滨飞机工业集团有限责任公司 Device and method for gluing and pressurizing helicopter tail duct skin
CN105082569A (en) * 2015-08-17 2015-11-25 江苏恒神股份有限公司 Technology for improving compression performance of composite material laminated board
CN105235236A (en) * 2015-11-12 2016-01-13 江苏恒神股份有限公司 Autoclave die for improving surface quality of workpiece and method
CN105437536A (en) * 2015-12-11 2016-03-30 昌河飞机工业(集团)有限责任公司 Composite reinforcing rib wall panel forming tool
CN105437537A (en) * 2015-12-08 2016-03-30 成都飞机设计研究所 Assembling method for airfoil total composite transonic flutter model

Patent Citations (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0439259A1 (en) * 1990-01-16 1991-07-31 Lord Corporation Improved method for rubber-to-metal bonding
CN101673880A (en) * 2009-10-21 2010-03-17 中国电子科技集团公司第五十四研究所 Method for manufacturing antenna reflecting surface with aluminum skin honeycomb sandwich structure
CN101905528A (en) * 2010-07-16 2010-12-08 沈阳飞机工业(集团)有限公司 Wedge-shaped autoclave forming process of composite material I-shaped section
CN102765198A (en) * 2012-07-13 2012-11-07 中国人民解放军国防科学技术大学 Vacuum assisted molding system of composite and molding method of composite
CN103029307A (en) * 2012-12-12 2013-04-10 江西洪都航空工业集团有限责任公司 Manufacture method of box-shaped structural main beam made from composite material
CN103273665A (en) * 2013-06-14 2013-09-04 沈阳飞机工业(集团)有限公司 Forming technology of square pipe part made of composite material
CN203579263U (en) * 2013-11-25 2014-05-07 德阳汉沣数控机械制造有限公司 Upper rim strip machining tool
CN104149228A (en) * 2014-07-08 2014-11-19 中国电子科技集团公司第二十研究所 Integrated forming die and method for glass fiber reinforced plastic antenna housing
CN104441696A (en) * 2014-09-22 2015-03-25 成都飞机工业(集团)有限责任公司 Manufacture method of special-shaped composite material rib
CN104441631A (en) * 2014-11-10 2015-03-25 沈阳黎明航空发动机(集团)有限责任公司 Manufacturing method of easily worn silicon rubber ring and metal cementing part
CN104626606A (en) * 2015-01-04 2015-05-20 哈尔滨飞机工业集团有限责任公司 Carbon fiber composite material forming tool
CN104691779A (en) * 2015-01-13 2015-06-10 哈尔滨飞机工业集团有限责任公司 Process method for replacement and repair of iron clad of main blade made of composite material
CN104847762A (en) * 2015-05-07 2015-08-19 哈尔滨飞机工业集团有限责任公司 Device and method for gluing and pressurizing helicopter tail duct skin
CN105082569A (en) * 2015-08-17 2015-11-25 江苏恒神股份有限公司 Technology for improving compression performance of composite material laminated board
CN105235236A (en) * 2015-11-12 2016-01-13 江苏恒神股份有限公司 Autoclave die for improving surface quality of workpiece and method
CN105437537A (en) * 2015-12-08 2016-03-30 成都飞机设计研究所 Assembling method for airfoil total composite transonic flutter model
CN105437536A (en) * 2015-12-11 2016-03-30 昌河飞机工业(集团)有限责任公司 Composite reinforcing rib wall panel forming tool

Similar Documents

Publication Publication Date Title
CN102909866A (en) Method for forming control of long joist axial line of composite material stiffened wall panel
CN101905538B (en) Process for integrally manufacturing megawatt wind turbine blade
CN105398181B (en) For bend glass cover plate and the laminating apparatus and applying method of flat-faced screen
CN106827557B (en) Composite material is glued reinforced structure and is glued face compensation method altogether
CN103660309B (en) Method for section bar of the composite production with re-entrant angle with stratified fiber
CN110171183A (en) A kind of the positioning pressure-equalizing device and forming method of the honeycomb sandwich construction containing built-in fitting
CN104325577B (en) Flanging die, assembling die, into the laying method of mold materialss and into mould method
CN109109341B (en) A kind of preparation method of wind turbine blade
CN103921450A (en) Manufacturing method of wing-body integrated honeycomb sandwiched composite material skin
CN105082568A (en) Liquid molding process of special-shaped composite structural part
CN108673909A (en) A kind of carbon fiber product molding/decoration integrated technique
CN110576593B (en) Film pasting method and application thereof and glass panel
CN104742382A (en) Pressure-assisted VARI (vacuum assisted resin infusion) forming device and method
CN102226446B (en) Method for preparing megawatt fan blade shear web and auxiliary bonding angle thereof
CN106965448A (en) A Secondary Bonding and Pressing Method for Thin Composite Material Plates
CN204488168U (en) A kind of vacuum gum adhering jig
CN104325636B (en) A kind of acrylonitrile-butadiene rubber metal adhesive part vacuum-bag process manufacture method
CN111037946A (en) Manufacturing method of I-shaped web of megawatt wind driven generator blade
CN215242964U (en) Vacuum bonding solidification forming device
CN107283137A (en) A kind of moulding technique of structural adhesive bonding part
CN109203516A (en) A kind of manufacturing method of wind electricity blade
CN112373051B (en) A kind of profile matching laying method for thermal insulation layer
CN109849351B (en) Composite material wing wall plate and metal wing rib sealing method based on co-bonding process
CN113547831A (en) Optical adhesive attaching method, display screen and preparation method of display screen
CN104847762A (en) Device and method for gluing and pressurizing helicopter tail duct skin

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
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20171024