发明名称 A SPACER AND GASKET ASSEMBLY FOR USE ON AN AIRCRAFT
摘要 A spacer and gasket assembly is shown for receipt between a static structure having an outer and inner surface and fastener holes there through and a removable structure having a base with fastener holes and an upper surface and a lower surface. The static structure and removable structure are engaged through a multiplicity of fasteners having a shaft diameter. The fasteners are adapted to apply a compression on the gasket between the static structure and the removable structure. The static structure and the removable structure have opposed, typically flat, facing walls. The spacer and gasket assembly comprising a substantially non-compressible spacer adapted for receipt between the static structure and the removable structure having a spacer thickness. A gasket has a deformable, flowable, elastomeric body and a skeleton having a skeleton thickness, the skeleton substantially integral with the body. The gasket has an uncompressed gasket thickness. The spacer and the gasket are adapted to be placed substantially between the facing walls of the static structure and the removable structure and the removable structure will compress and deform the gasket when the fasteners are torqued down.
申请公布号 CA2820669(C) 申请公布日期 2017.02.21
申请号 CA20132820669 申请日期 2013.07.10
申请人 AVIATION DEVICES & ELECTRONIC COMPONENTS, LLC 发明人 BOYD, MATT;DRY, MICHAEL;BOOMER, KENT;BUSBY, JEFF
分类号 F16J15/06;B64C1/14 主分类号 F16J15/06
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