Patent ID: 11952099
Assignee: THE BOEING COMPANY
Field: Other special machines (Mechanical engineering)
Classification: CPC B | IPC B

Claim 1:
2. The aircraft window assembly of claim 1, further comprising a plurality of window frame fastener bores extending through and spaced-apart around the circumferential flange portion and configured to receive a respective plurality of window frame fasteners to retain the window frame to the aircraft skin, wherein the at least one overmolded feature comprises a plurality of overmolded protrusions, wherein each overmolded protrusion is molded atop a window frame fastener bore of the plurality of window frame fastener bores, and wherein each overmolded protrusion is configured to receive a window frame fastener receiver, and wherein each window frame fastener receiver is configured to receive and engage a window frame fastener of the plurality of window frame fasteners.