【英文标准名称】:Selfadhesivetapes-Terminology;GermanversionEN12481:2000
【原文标准名称】:自粘胶带.术语
【标准号】:EN12481-2000
【标准状态】:现行
【国别】:
【发布日期】:2001-03
【实施或试行日期】:
【发布单位】:欧洲标准学会(EN)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:定义;定义;自粘的;多语种的;词汇;粘接带;胶粘连接;术语
【英文主题词】:Adhesive-bondedjoints;Definition;Definitions;Multilingual;Self-adhesive;Splicingtapes;Terminology;Vocabulary
【摘要】:
【中国标准分类号】:G38
【国际标准分类号】:01_040_83;83_180
【页数】:23P.;A4
【正文语种】:英语
基本信息
| 标准名称： | 295硅脂 |
| 中标分类： |
化工 >>
化学试剂 >>
高纯试剂、高纯物质 |
| 替代情况： | 被HG/T 2502-93代替 |
| 发布日期： | |
| 实施日期： | 1994-07-01 |
| 首发日期： | |
| 作废日期： | |
| 出版日期： | |
适用范围
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前言
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目录
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引用标准
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所属分类： 化工 化学试剂 高纯试剂 高纯物质
Product Code:SAE ARP5143
Title:Vacuum Bagging of Thermosetting Composite Repairs
Issuing Committee:Ams Cacrc Commercial Aircraft Composite Repair Committee
Scope: This Aerospace Recommended Practice (ARP) describes methods of vacuum bagging, a process used to apply pressure in adhesive bonding and heat curing of thermosetting epoxy and polyester matrix fabrications for commercial aircraft composite parts. If this document is used for the vacuum bagging of other than thermosetting epoxy and polyester materials, the fitness for this purpose must be determined by the user.The methods shall only be used when specified in an approved repair document or with the agreement of the Original Equipment Manufacturer (OEM) or regulatory authority.The purpose of this ARP is to provide a set of standard methods for the bagging of thermosetting composite materials that may be referenced in repair documents produced by airlines or airframe and engine manufacturers. It is intended that this ARP be one of a number of ARPs that will cover other aspects of the techniques required to perform composite repairs.
Rationale: This Aerospace Recommended Practice (ARP) describes methods of vacuum bagging, a process used to apply pressure in adhesive bonding and heat curing of thermosetting epoxy and polyester matrix fabrications for commercial aircraft composite parts. If this document is used for the vacuum bagging of other than thermosetting epoxy and polyester materials, the fitness for this purpose must be determined by the user.The methods shall only be used when specified in an approved repair document or with the agreement of the Original Equipment Manufacturer (OEM) or regulatory authority.The purpose of this ARP is to provide a set of standard methods for the bagging of thermosetting composite materials that may be referenced in repair documents produced by airlines or airframe and engine manufacturers. It is intended that this ARP be one of a number of ARPs that will cover other aspects of the techniques required to perform composite repairs.