摘要:
A window frame assembly (218) for an aircraft (10) includes a window frame (226) of composite material, adapted for attachment in a window opening (236) of an aircraft (10), having an outer flange (230) with an exterior surface (262) and an interior surface (264), a metal erosion shield (252) attached to the exterior surface (262) of the outer flange (230), and a polymer adapter ring (256) attached to the interior surface (264) of the outer flange (230). The window frame (226) has a substantially constant thickness, and the erosion shield (252) has a substantially constant cross-sectional shape. The adapter ring (256) has a sloped engagement surface (250) configured for supporting a window pane assembly (218).
摘要:
A mobile platform interior panel (10) is provided that includes a body (14) formed by a low pressure injection process and at least one of a duct (18) and a layer of insulation (22) integrated with the body. The low pressure injection process allows the duct (18) and insulation (22) to be integrated with the body (14) simultaneously with the forming of the panel (10). More specifically, the duct (18) is integrated with the panel (10) by forming at least one internal cavity within the panel as the panel (10) is formed. Additionally, the insulation (22) is integrated with the panel by forming the panel using a low pressure injection material having desired insulative properties.