发明名称 FAST LINE MAINTENANCE REPAIR METHOD AND SYSTEM FOR COMPOSITESTRUCTURES
摘要 A fast line maintenance repair process for damaged composite structures includes the application of a pre-cured patch that uses a quick curing paste adhesive to bond the patch to the structure. The adhesive is cured at relatively low elevated temperatures provided by a chemical heat pack. The low temperature cure eliminates the need to dry out the part and permits the application of the repair in a hazardous environment. In a typical commercial airline application, airline maintenance personnel can install the repair at the flight gate. The repair is intended to restore the structure to a desired load capability in approximately one hour. The repair can be removed if need be with less overall damage than would occur upon removal of typical mechanically fastened repairs. All or some of the repair materials and tools can be provided in a portable kit.
申请公布号 CA2565585(A1) 申请公布日期 2007.05.02
申请号 CA20062565585 申请日期 2006.10.25
申请人 THE BOEING COMPANY 发明人 SPALDING, JOHN F., JR.;BLANCHARD, STEVEN D.;KELLER, RUSSELL L.
分类号 B64F5/00;B29C73/10;B32B17/04;E04G23/02 主分类号 B64F5/00
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