Aeronautics and astronautics – Aircraft structure – Fuselage and body construction
Reexamination Certificate
2011-06-07
2011-06-07
Lee, Benjamin P (Department: 3641)
Aeronautics and astronautics
Aircraft structure
Fuselage and body construction
C244S118600, C297S216100, C297S452180
Reexamination Certificate
active
07954762
ABSTRACT:
An aircraft seat assembly configured in accordance with an example embodiment of the invention utilizes composite materials to achieve significant weight savings relative to conventional seat designs. The seat assembly includes a lightweight composite support structure, a lightweight composite seat base, and a seat back assembly that employs a lightweight inner frame. The seat cushion and the seat back cushion may utilize a sealed pneumatic element that self-inflates to provide increased air cushioning during flight. The seat assembly can leverage inexpensive manufacturing techniques such that the seat assembly can be economically produced for use as an economy class seat.
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Boren Kelly L.
Kismarton Max U.
Retz Kevin M.
Lee Benjamin P
The Boeing Company
Tung & Associates
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