发明名称 AIRCRAFT STRUCTURE WITH MEANS FOR REDUCING THE RISK OF DISBONDING IN AREAS OF DIFFERENT STRAIN
摘要 Technologies for reducing the risk of disbonding between two bonded members at areas of differing strain in the members are provided. Where the difference in strain between the two bonded members becomes excessing, movement of the members relative to each other may cause a traditional rigid adhesive to fail, resulting in a disbond or delamination in one or both composite members at the point of differing strain. Disbonding may be minimized or prevented by placing a compliant material, such as a thin sheet of rubber, between the structural members at the point of differing strain. The compliance of the material may allow the compliant material to deform enough to remain bonded to both structural members when subjected to a stress that might otherwise disbond or delaminate the bonded members.
申请公布号 EP2776314(B1) 申请公布日期 2016.08.10
申请号 EP20120834607 申请日期 2012.08.28
申请人 THE BOEING COMPANY 发明人 KISMARTON, MAX
分类号 B23B3/08;B29C65/00;B32B3/02;B32B3/08;B32B7/12;B32B25/00;B32B25/02;B64C1/06;B64C3/18;B64C3/20;B64C3/26 主分类号 B23B3/08
代理机构 代理人
主权项
地址