Patent ID: 9599138
Date: 2017-03-21
CPC Classifications: B64C,B64D,F16B,Y02T

Claim:
1. An aircraft monument wall assembly, comprising: first and second composite panels; a core material filling a space between the first and second composite panels; an attachment device integrated into the first and second composite panels, comprising: a pair of spaced apart inverted U-shaped parallel plates sandwiched between the first and second composite panels, respectively, each plate having an outer surface facing the monument wall, a radially outer edge along the U-shaped profile, a radially inner edge along the U-shaped profile, and a bottom edge; a member connecting the respective radially inner edges of the pair of spaced apart inverted U-shaped parallel plates, forming an open channel radially outward of the member and between the plates; a base connecting the respective radially inner edges of the pair of spaced apart inverted U-shaped parallel plates, the base including a lug and fastener hole, where the fastener hole is disposed directly beneath one of the spaced apart inverted U-shaped parallel plates; and wherein the first and second composite panels, core material, and attachment device are fabricated as a single unit.