Invention Application
- Patent Title: Serrated Fitting
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Application No.: US18482451Application Date: 2023-10-06
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Publication No.: US20250116284A1Publication Date: 2025-04-10
- Inventor: Kenneth D. Cominsky
- Applicant: The Boeing Company
- Applicant Address: US VA Arlington
- Assignee: The Boeing Company
- Current Assignee: The Boeing Company
- Current Assignee Address: US VA Arlington
- Main IPC: F16B5/02
- IPC: F16B5/02 ; B64C1/18 ; B64D9/00 ; B64F5/10

Abstract:
A serrated fitting and method for installing fixed length roller tray segments spanning an aircraft fuselage integration zone. The serrated fitting includes a first surface for attachment to a fixed length roller tray segment. The serrated fitting also includes a serrated surface for engagement with a serrated plate attached to a floor beam of an aircraft. A fastener connects the serrated surface to the serrated plate and the floor beam through a pre-drilled hole in the floor beam. The pre-drilled hole is larger than the diameter of the fastener to accommodate accumulated tolerance between joined fuselage sections at a fuselage integration zone.
Public/Granted literature
- US12286998B1 Serrated fitting Public/Granted day:2025-04-29
Information query
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