Abstract: A vehicle window assembly includes first and second substrates substantially transparent to visible light and a seal with internal and external portions. The second substrate is disposed in a spaced apart relationship relative to the first substrate and defines a space therebetween. The internal portion is disposed in the space between the first and second substrates along at least part of peripheries thereof. The external portion is disposed external relative to space between the first and second substrates, has a substantially flexible construction, and substantially extends outward from the first and second substrates. The seal substantially inhibits at least one of water and oxygen from entering the space. A coupling agent is disposed between the first and second substrates, laminates the substrates together, and adheres the seal thereto. When disposed in a window opening, the external portion of the seal deflects against an edge of the opening.

Abstract: A variable transmission element includes a first substrate that has a first surface and a second surface opposite the first surface. A second substrate includes a third surface and a fourth surface opposite the third surface. The first and second surfaces face each other and are disposed in a spaced apart relationship so as to define a space therebetween. A seal formed of a sealing material extends along a perimeter of the first and second substrates. A first lamination layer comprises a first lamination material that is different from the sealing material and the first lamination layer is coupled to the second surface. A second lamination layer comprises a second lamination material that is different from the sealing material and the second lamination layer is coupled to the second substrate. An electro-optic device is disposed between the first lamination layer and the second lamination layer.

Abstract: An aircraft window includes an outer window assembly that includes a pressure pane coupled to a pressure pane frame. An inner window assembly includes a bezel adapted to couple to a perimeter of the inner window assembly against the outer window assembly. The bezel has a plurality of attachment features disposed thereon. A plurality of retaining features is disposed around the perimeter of the window. The retention features are configured to engage the attachment features for retaining the inner window assembly on the outer window assembly.

Abstract: A window mounting assembly includes a multi-piece bezel having a first portion having an attachment feature, and a second portion having a retention feature. The retention feature is configured to engage the attachment feature such that an inner opening is defined having an inner wall. The inner wall defines a channel. An electro-optic element is disposed in the opening and configured for reception in the channel of the inner wall.

Abstract: A window mounting assembly includes a multi-piece bezel having a first portion having an attachment feature, and a second portion having a retention feature. The retention feature is configured to engage the attachment feature such that an inner opening is defined having an inner wall. The inner wall defines a channel. An electro-optic element is disposed in the opening and configured for reception in the channel of the inner wall.

Abstract: An aircraft window includes an outer window assembly that includes a pressure pane coupled to a pressure pane frame. An inner window assembly includes a bezel adapted to couple to a perimeter of the inner window assembly against the outer window assembly. The bezel has a plurality of attachment features disposed thereon. A plurality of retaining features is disposed around the perimeter of the window. The retention features are configured to engage the attachment features for retaining the inner window assembly on the outer window assembly.

Abstract: An aircraft window foam mounting assembly having an exterior pressure pane frame including an inner surface and an outer surface. A pressure pane is in abutting contact with the inner surface of the exterior pressure pane frame. A foam bezel is proximate a periphery of the pressure pane and defines an inner opening. The foam bezel includes an inner wall and an outer wall. The inner wall includes a channel. An electrochromic element is disposed in the opening and is configured for reception in the channel of the inner wall. An electrically conductive member is operably coupled to the foam bezel and extends from the inner wall to the outer wall.

Abstract: An aircraft window foam mounting assembly having an exterior pressure pane frame including an inner surface and an outer surface. A pressure pane is in abutting contact with the inner surface of the exterior pressure pane frame. A foam bezel is proximate a periphery of the pressure pane and defines an inner opening. The foam bezel includes an inner wall and an outer wall. The inner wall includes a channel. An electrochromic element is disposed in the opening and is configured for reception in the channel of the inner wall. An electrically conductive member is operably coupled to the foam bezel and extends from the inner wall to the outer wall.