CN102814979A - 固定机舱罩加强筋工艺 - Google Patents

固定机舱罩加强筋工艺 Download PDF

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Publication number
CN102814979A
CN102814979A CN201110160673XA CN201110160673A CN102814979A CN 102814979 A CN102814979 A CN 102814979A CN 201110160673X A CN201110160673X A CN 201110160673XA CN 201110160673 A CN201110160673 A CN 201110160673A CN 102814979 A CN102814979 A CN 102814979A
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China
Prior art keywords
reinforcing rib
cabin cover
engine room
room cover
reinforcement
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CN201110160673XA
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English (en)
Inventor
周强
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XINJIANG YONGCHANG NEW MATERIAL TECHNOLOGY CO LTD
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XINJIANG YONGCHANG NEW MATERIAL TECHNOLOGY CO LTD
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Priority to CN201110160673XA priority Critical patent/CN102814979A/zh
Publication of CN102814979A publication Critical patent/CN102814979A/zh
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Abstract

一种“固定机舱罩加强筋工艺”,主要用于机舱罩的制作领域中。本发明型解决了固定机舱罩加强筋时质量不稳定、工作效率低的问题。解决该问题的主要技术方案是:先用树脂与玻璃纤维织物的混合物将机舱罩与加强筋接触面之间的缝隙密封,然后再用真空树脂导入工艺将加强筋整体固定在机舱罩上;此技术方案的要点是:用树脂与玻璃纤维织物的混合物将机舱罩与加强筋接触面之间的缝隙密封,它的作用是为使用“真空树脂导入工艺”做准备。

Description

固定机舱罩加强筋工艺
技术领域
本发明型涉及一种固定加强筋工艺,具体是一种固定机舱罩加强筋工艺,主要用于机舱罩制作工艺领域中。
背景技术
现有的此类“固定机舱罩加强筋的工艺”是采用手糊成型的。其缺点是:手糊成型的产品质量不稳定,而且生产效率低。
发明内容
本发明型的目的就是提供一种“固定机舱罩加强筋”工艺,以解决现有技术存在的成型产品质量不稳定、生产效率低的问题。
本发明型的技术方案是:先采用树脂与玻璃纤维织物的混合物将机舱罩与加强筋接触面之间的缝隙密封,然后再用真空树脂导入工艺将加强筋整体固定在机舱罩上。此技术方案的要点是:用树脂与玻璃纤维织物的混合物将机舱罩与加强筋接触面之间的缝隙密封,它的作用是为使用“真空树脂导入工艺”做准备。
本发明型具体有以下优点:
1、产品质量稳定;
2、生产效率高;
附图说明
图1是本发明型的局部密封结构示意图;
图2是图1中1-1剖视图;
具体实施方式
参见图1~图2,本发明型图1中1是机舱罩、2是加强筋、3是起密封作用的树脂与玻璃纤维织物混合物。
本发明型是先用树脂与玻璃纤维织物的混合物将机舱罩与加强筋接触面之间的缝隙密封,然后再用真空树脂导入工艺将加强筋整体固定在机舱罩上。

Claims (3)

1.一种“固定机舱罩加强筋工艺”,主要用于机舱罩的制作领域中。
2.根据权利要求1所述的机舱罩与加强筋接触面之间的缝隙采用树脂与玻璃纤维织物混合物密封。
3.根据权利要求2所述的缝隙密封之后,采用“真空树脂导入工艺”将加强筋固定在机舱罩内部。
CN201110160673XA 2011-06-08 2011-06-08 固定机舱罩加强筋工艺 Pending CN102814979A (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201110160673XA CN102814979A (zh) 2011-06-08 2011-06-08 固定机舱罩加强筋工艺

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201110160673XA CN102814979A (zh) 2011-06-08 2011-06-08 固定机舱罩加强筋工艺

Publications (1)

Publication Number Publication Date
CN102814979A true CN102814979A (zh) 2012-12-12

Family

ID=47299592

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201110160673XA Pending CN102814979A (zh) 2011-06-08 2011-06-08 固定机舱罩加强筋工艺

Country Status (1)

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CN (1) CN102814979A (zh)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030019567A1 (en) * 2001-07-26 2003-01-30 Burpo Steven J. Vacuum assisted resin transfer method for co-bonding composite laminate structures
US6942915B1 (en) * 1999-03-19 2005-09-13 Toray Industries, Inc. FRP roofing material, manufacturing method, and its connecting structure and connecting method
WO2006112823A1 (en) * 2005-04-13 2006-10-26 The Boeing Company Method to eliminate undulations in a composite panel
CN101417511A (zh) * 2008-12-02 2009-04-29 东华大学 一种带真空加强筋结构部件的真空导入制造方法
CN101649817A (zh) * 2009-09-17 2010-02-17 秦皇岛耀华玻璃钢股份公司 网栅型增强结构

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6942915B1 (en) * 1999-03-19 2005-09-13 Toray Industries, Inc. FRP roofing material, manufacturing method, and its connecting structure and connecting method
US20030019567A1 (en) * 2001-07-26 2003-01-30 Burpo Steven J. Vacuum assisted resin transfer method for co-bonding composite laminate structures
WO2006112823A1 (en) * 2005-04-13 2006-10-26 The Boeing Company Method to eliminate undulations in a composite panel
CN101417511A (zh) * 2008-12-02 2009-04-29 东华大学 一种带真空加强筋结构部件的真空导入制造方法
CN101649817A (zh) * 2009-09-17 2010-02-17 秦皇岛耀华玻璃钢股份公司 网栅型增强结构

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Application publication date: 20121212