Aircraft door with oversizing

Aeronautics and astronautics – Aircraft structure – Details

Reexamination Certificate

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Details

Reexamination Certificate

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07896291

ABSTRACT:
An aircraft fuselage section is provided in which an outer skin construction provides at least one door opening having a width, such that it is divided by at least one rib of the fuselage skeleton of the aircraft fuselage section into multiple opening areas.

REFERENCES:
patent: 3119441 (1964-01-01), Furry, Jr.
patent: 5678787 (1997-10-01), Kahn et al.
patent: 6474600 (2002-11-01), Apps
patent: 144257 (1921-07-01), None
patent: 579708 (1946-08-01), None
patent: 98/25817 (1998-06-01), None
patent: 01/23254 (2001-04-01), None
patent: 03104080 (2003-12-01), None
patent: 2005110843 (2005-11-01), None
Chinese Office Action for Application No. 200780012653.X mailed Jun. 21, 2010.

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