Patent ID: 6736352
Filing Date: 2004-05-18
Classification: B64C

Abstract:
An aircraft window, comprising:a unitary window frame configured for installation in a passenger cabin of an aircraft, the window frame having a first aperture extending through the window frame and a second aperture extending through the window frame; an at least partially light transmissive first pane assembly carried by the window frame and positioned in the first aperture, the first pane assembly having a first face and a second face facing opposite from the first face, the first pane assembly being configured to withstand a pressure differential between the first and second faces of about 8.6 psi or more; and an at least partially light transmissive second pane assembly carried by the window frame and positioned in the second aperture, the second pane assembly having a first face and a second face facing opposite from the first face, the second pane assembly being configured to withstand a pressure differential between the first and second faces of about 8.6 psi or more.