| 主权项 |
1. An aircraft comprising:
a fuselage including a plurality of frame members disposed at predetermined intervals in a longitudinal direction of the fuselage and a plurality of stringers extending substantially linearly in the longitudinal direction, the fuselage defining an interior; a compartment located in the interior of the fuselage, the compartment defining an interior area; a first window assembly mounted to an upper portion of the fuselage for introducing daylight downwardly through a ceiling panel and into the interior area, the first window assembly is flanked by adjacent frame members of the plurality of frame members and adjacent stringers of the plurality of stringers, the first window assembly including a first window pane, a first inner cover and a first retainer, the first inner cover introduces the daylight from the first window pane into the interior area, the first retainer secures the first window pane and the first inner cover to the fuselage; and a second window assembly mounted to the upper portion of the fuselage opposite the first window assembly for introducing daylight downwardly through the ceiling panel and into the interior area, the second window assembly is flanked by adjacent frame members of the plurality of frame members and adjacent stringers of the plurality of stringers, the second window assembly including a second window pane, a second inner cover and a second retainer, wherein the interior area defines a lateral centerline and a vertical centerline, an intersection of the lateral and vertical centerlines defines a center point of the interior area, the first window assembly and the second window assembly are each angularly offset through the center point relative to the vertical centerline from a 0 degree position to a 60 degree position. |
