摘要:
Passenger interface units include individual passenger modules (14a,14b) having co-located controls for passenger comfort and entertainment systems. The modules (14a,14b) will include a glass panel (40) having front and rear surfaces, a structural support panel (42) bonded to the rear surface of the glass panel (40) and a light-emitting unit (50) supported by the support panel (42) behind the rear surface of the glass panel (40). The rear surface of the glass panel (40) may include an opaque printed coating layer (46) having at least one unpainted region that is transparent to visible light emitted by the light-emitting unit (50) thereby allowing the visible light to be transmitted through the glass panel (40) and visible at the front surface thereof.
摘要:
Passenger interface units include individual passenger modules (14a,14b) having co-located controls for passenger comfort and entertainment systems. The modules (14a,14b) will include a glass panel (40) having front and rear surfaces, a structural support panel (42) bonded to the rear surface of the glass panel (40) and a light-emitting unit (50) supported by the support panel (42) behind the rear surface of the glass panel (40). The rear surface of the glass panel (40) may include an opaque printed coating layer (46) having at least one unpainted region that is transparent to visible light emitted by the light-emitting unit (50) thereby allowing the visible light to be transmitted through the glass panel (40) and visible at the front surface thereof.
摘要:
Adaptive, self-adjusting decorative trim assemblies are especially adapted for use in aircraft cabin interiors where the fuselage undergoes deformation and/or distortion due to pressurization during flight. The self-adjusting features of the decorative trim assemblies according to the embodiments described herein thus allow for relative movement between mutually intersecting interior cabin panels (12, 14) without jeopardizing the cabin interior aesthetics (e.g., since the relative positioning of the panels is not disrupted by virtue of such fuselage deformations).