Abstract: Aircraft windows and associated methods for installation. The windows can be installed in a passenger cabin of an aircraft and can include a frame that supports a pane assembly having a viewing area of at least 180 square inches. The viewing area can have a triangular shape, with the sides of the window aligned with none of the major axis of the aircraft. Alternatively, the window can have a longitudinally extended rectangular shape, a diamond shape or an elliptical shape. The window frame can have a divider portion that separates two window apertures, each of which carries a separate pane assembly. Adjacent windows can be closed out with a common bezel.

Abstract: Aircraft windows and associated methods for installation. The windows can be installed in a passenger cabin of an aircraft and can include a frame that supports a pane assembly having a viewing area of at least 180 square inches. The viewing area can have a triangular shape, with the sides of the window aligned with none of the major axis of the aircraft. Alternatively, the window can have a longitudinally extended rectangular shape, a diamond shape or an elliptical shape. The window frame can have a divider portion that separates two window apertures, each of which carries a separate pane assembly. Adjacent windows can be closed out with a common bezel.

Abstract: A deformation compensation system for use with a large phased-array antenna system to electronically compensate for surface deformations occurring on the phased-array antenna which would otherwise compromise antenna performance. In one embodiment, a plurality of strain gauges are disposed on or integrally formed in structure forming the phased-array antenna. The strain gauges are placed at those locations on the antenna structure, where, through prior structural modeling and testing, it has been determined that high strains associated with the expected deformation of the phased-array antenna are expected to occur to a significant degree. The strain gauges output signals to a data acquisition system which uses a strain-to-displacement algorithm to produce displacements corresponding to the estimated, deformed shape of the phased-array antenna.