Patent ID: 9365281
Filing Date: 2016-06-14
CPC Classification: B64C,B64D

Claim Text:
1. An aircraft window mounting assembly comprising: a pressure pane in abutting contact with an inner surface of an exterior pressure pane frame; a bezel proximate a periphery of the pressure pane and defining an inner opening, the foam bezel including an inner wall, an outer wall, an exterior wall, and an interior wall; a dust cover proximate the interior wall of the bezel; an electro-optic element disposed in the opening and configured for reception by the inner wall, wherein the pressure pane, the bezel, and the electro-optic element define an exterior cavity, and wherein the bezel, the electro-optic element, and the dust cover define an interior cavity; a first relief passage in fluid communication with the exterior cavity and the interior cavity; and a second relief passage in fluid communication with the interior cavity and one of an aircraft interior cabin and an aircraft wall.