The Boeing Company
Decompression panel assembly and methods of assembling the same

Last updated:

Abstract:

A decompression panel assembly for use in an aircraft includes a body panel having an opening defined therein and a cover panel positioned within the opening and spaced from the body panel. The decompression panel assembly also includes an annular spacer panel positioned outboard from the cover panel and the body panel. The spacer panel is spaced from the cover panel to define a first annular flow path between the cover panel and the spacer panel, and the spacer panel is spaced from the body panel to define a second annular flow path between the body panel and the spacer panel.

Status:
Grant
Type:

Utility

Filling date:

19 Dec 2018

Issue date:

23 Feb 2021