A windshield for a pressurized aircraft includes a single transparent unit that functions structurally to allow pressurization of the aircraft and to support the aircraft's fuselage in response to external loads. The windshield also functions operationally to provide the pilot with an unobstructed field of vision through an extended arc of more than two hundred degrees. For its manufacture, layers of the transparent unit are respectively bent along a straight center line to establish two curved portions that are symmetrical relative to a common plane. The layers are then laminated.
申请公布号
WO2008097383(A3)
申请公布日期
2008.11.13
申请号
WO2007US81288
申请日期
2007.10.12
申请人
SPECTRUM AERONAUTICAL, LLC;BLUE, LINDEN, S.;COONEY, DANIEL, E.