SAE ARP 5143-2002
热固性复合材料修理的真空装袋

Vacuum Bagging of Thermosetting Composite Repairs


SAE ARP 5143-2002 发布历史

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.

SAE ARP 5143-2002由美国机动车工程师协会 US-SAE 发布于 2002-07-01。

SAE ARP 5143-2002 在中国标准分类中归属于: V13 航空与航天用非金属材料,在国际标准分类中归属于: 49.025.01 航空航天制造用材料综合。

SAE ARP 5143-2002 发布之时,引用了标准

SAE ARP 5143-2002的历代版本如下:

 

 

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标准号
SAE ARP 5143-2002
发布日期
2002年07月01日
实施日期
废止日期
中国标准分类号
V13
国际标准分类号
49.025.01
发布单位
US-SAE
引用标准
SAE AIR 4844-1994 SAE ARP 4916-1997 SAE ARP 4977-1996 SAE ARP 4991-1998 SAE ARP 5144-2000 SAE ARP 5319-2002
适用范围
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.

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