Decompression panel assembly

- The Boeing Company
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Description

FIG. 1 is a front view of the decompression panel assembly showing the new design installed in an aircraft sidewall;

FIG. 2 is a front view of the decompression panel assembly of FIG. 1 shown without the environment;

FIG. 3 is a rear view of the decompression panel assembly shown in FIG. 2;

FIG. 4 is a top view of the decompression panel assembly shown in FIG. 2;

FIG. 5 is a bottom view of the decompression panel assembly shown in FIG. 2;

FIG. 6 is a left side view of the decompression panel assembly shown in FIG. 2;

FIG. 7 is a right side view of the decompression panel assembly shown in FIG. 2;

FIG. 8 is a perspective front view of the decompression panel assembly shown in FIG. 2;

FIG. 9 is a perspective rear view of the decompression panel assembly shown in FIG. 2; and,

FIG. 10 is an exploded view of the decompression panel assembly shown in FIG. 2.

In these drawings, the solid lines illustrate the claimed ornamental design, whereas the broken lines illustrate unclaimed environmental features and form no part of the claimed design.

Claims

We claim the ornamental design for a decompression panel assembly, as shown and described.

Referenced Cited
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Other references
  • HCL Experience Comfort, HCLtech.com, [online], [site visited Apr. 23, 2020]. <URL: https://www.hcltech.com/sites/default/files/wx8501_aircraft_interior-ife_v1_0.pdf> (Year: 2020).
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Patent History
Patent number: D908054
Type: Grant
Filed: Dec 19, 2018
Date of Patent: Jan 19, 2021
Assignee: The Boeing Company (Chicago, IL)
Inventors: Thomas Seth Perkins (Renton, WA), Adam R. Weston (Brier, WA)
Primary Examiner: T Chase Nelson
Assistant Examiner: Jonathan J. Han
Application Number: 29/674,060