Invention Grant
- Patent Title: Composite leg structure for a lightweight aircraft seat assembly
- Patent Title (中): 用于轻型飞机座椅组件的复合腿结构
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Application No.: US11614978Application Date: 2006-12-22
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Publication No.: US08205833B2Publication Date: 2012-06-26
- Inventor: Max U. Kismarton , James A. Fullerton
- Applicant: Max U. Kismarton , James A. Fullerton
- Applicant Address: US IL Chicago
- Assignee: The Boeing Company
- Current Assignee: The Boeing Company
- Current Assignee Address: US IL Chicago
- Agency: Tung & Associates
- Main IPC: B64D25/04
- IPC: B64D25/04 ; B64D11/06

Abstract:
An aircraft passenger seat configured in accordance with an embodiment of the invention utilizes composite materials to achieve significant weight savings relative to conventional seat designs. The seat includes one or more lightweight composite support legs, a lightweight composite seat pan, and a lightweight composite seat back structure. The support legs are coupled to the seat pan, which is in turn coupled to the seat back structure. The support legs utilize composite frame elements that are formed as continuous compression molded composite extrusions. The seat pan includes composite fore and aft cross beams that are also formed as continuous compression molded composite extrusions. The aft cross beam includes a rear flange that serves as a flexible “hinge” for the seat back structure. The seat can leverage producible and relatively inexpensive composite manufacturing techniques such that the seat can be economically produced for use as an economy class seat.
Public/Granted literature
- US20080290242A1 COMPOSITE LEG STRUCTURE FOR A LIGHTWEIGHT AIRCRAFT SEAT ASSEMBLY Public/Granted day:2008-11-27
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