Invention Grant
- Patent Title: Fuselage structure including an integrated fuselage stanchion
- Patent Title (中): 机身结构包括一个集成的机身支柱
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Application No.: US11842414Application Date: 2007-08-21
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Publication No.: US07861970B2Publication Date: 2011-01-04
- Inventor: Kenneth H. Griess , Gary E. Georgeson
- Applicant: Kenneth H. Griess , Gary E. Georgeson
- Applicant Address: US IL Chicago
- Assignee: The Boeing Company
- Current Assignee: The Boeing Company
- Current Assignee Address: US IL Chicago
- Agency: Moore & Van Allen PLLC
- Agent Charles I. Moore
- Main IPC: B64C1/00
- IPC: B64C1/00
Abstract:
A fuselage structure for an aircraft or similar vehicle may include an upper fuselage portion and a lower fuselage portion. A floor may be disposed between the upper fuselage portion and the lower fuselage portion. At least one unitized stanchion may be disposed between the floor and the lower fuselage portion. The at least one unitized stanchion may form the only structural support between the floor and the lower fuselage portion without any vertical beams.
Public/Granted literature
- US20090294588A1 FUSELAGE STRUCTURE INCLUDING AN INTEGRATED FUSELAGE STANCHION Public/Granted day:2009-12-03
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