DEFORMABLE AIRCRAFT WINDOW

摘要

An aircraft window assembly (10) includes a first panel (12) having a first surface (14) and a second surface (16). in a first state in which there is no pressure difference between the first surface (14) and the second surface (16), the first panel (12) has a cross-sectional shape selected from planar, outwardly convex, or inwardly convex. In a second state in which there is a pressure difference between first surface (14) and the second surface (16), the first panel (12) has an outwardly convex cross-sectional shape.