Automated Aircraft Management System
US-2024400203-A1 · Dec 5, 2024 · US
US9599138B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9599138-B2 |
| Application number | US-201313851838-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 27, 2013 |
| Priority date | Mar 28, 2012 |
| Publication date | Mar 21, 2017 |
| Grant date | Mar 21, 2017 |
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An attachment device for an aircraft monument is disclosed having a pair of spaced apart parallel plates having vertical sides and a rounded upper surface defining an arch. A panel attaches the spaced apart parallel plates along an inner radius, and a pair of lugs including a vertical channel is disposed below the plates for receiving fasteners to connect the attachment device to a rail or planar surface.
Opening claim text (preview).
I 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. 2. The aircraft monument wall of claim 1 , wherein the attachment device is made of a non-metallic material. 3. The aircraft monument wall of claim 1 , wherein the attachment device is made of titanium. 4. The aircraft monument wall of claim 1 , wherein the spaced apart inverted U-shaped parallel plates are in contact with the core material inside the monument wall.
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