Optimized fuselage structure

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Reexamination Certificate

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Details

C244S120000

Reexamination Certificate

active

07735779

ABSTRACT:
A fuselage structure including an upper fuselage portion defined by a first cross-section including at least three different radii of curvature. The fuselage structure may also include a lower fuselage portion defined by a second cross-section including at least three different radii of curvature, wherein the first cross-section is different from the second cross-section.

REFERENCES:
patent: 3511456 (1970-05-01), Fehring et al.
patent: 4593870 (1986-06-01), Cronkhite et al.
patent: 4674712 (1987-06-01), Whitener et al.
patent: 6834833 (2004-12-01), Sankrithi
patent: 6959894 (2005-11-01), Hayashi
patent: 2002/0153454 (2002-10-01), Seidel
patent: 2005/0061916 (2005-03-01), Sankrithi
patent: 2007/0108347 (2007-05-01), Sankrithi et al.
patent: 199715492 (1997-05-01), None
patent: 2007057411 (2007-05-01), None
UK Intellectual Property Office, Combined Search and Examination Report under Sections 17 and 18(3), for United Kingdom Patent Application No. GB0721312.7, dated Feb. 13, 2008.
“Aeronautics Lifting Fuselage: The Lifting Fuselage Body.” Meridian International Research. http://www.meridian-int-res.com/Aeronautics/Burnelli.htm.
Fuselage. http://wikipedia.org/wiki/Fuselage.
Ilcewicz, L.B. “Advanced Technology Composite Fuselage—Program Overview.” NASA Contractor Report 4734, Apr. 1997.
Longeron. http://wikipedia.org/wiki/Longeron.

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