Aeronautics and astronautics – Aircraft power plants – Mounting
Reexamination Certificate
2011-06-14
2011-06-14
Dinh, Tien (Department: 3644)
Aeronautics and astronautics
Aircraft power plants
Mounting
C244S05300R, C244S129400
Reexamination Certificate
active
07959106
ABSTRACT:
An integrated propulsive turbofan engine system includes a downstream cylindrical nacelle structure in two parts. The first of the two parts is fixed and fastens engine attachment elements and an intermediate casing to the aircraft. The second of the two parts may move between a closed position used during operation and an open position during maintenance when access to engine components is needed.
REFERENCES:
patent: 2944766 (1960-07-01), Freeding et al.
patent: 4055041 (1977-10-01), Adamson et al.
patent: 4365775 (1982-12-01), Glancy
patent: 5350136 (1994-09-01), Prosser et al.
patent: 5524847 (1996-06-01), Brodell et al.
patent: 6170253 (2001-01-01), Newton
patent: 6220546 (2001-04-01), Klamka et al.
patent: 2007/0267539 (2007-11-01), Bulin
patent: 2007/0278345 (2007-12-01), Oberle et al.
patent: 0 453 360 (1991-10-01), None
patent: 2 757 823 (1998-07-01), None
patent: 2 259 954 (1993-03-01), None
patent: WO 94/24430 (1994-10-01), None
U.S. Appl. No. 12/103,258, filed Apr. 15, 2008, Dron, et al.
U.S. Appl. No. 11/857,735, filed Sep. 19, 2007, Guibert, et al.
Guibert Thibaud Jean-Baptiste
Lefort Guillaume
Tesniere Marc Patrick
Dinh Tien
Green Richard R
Oblon, Spivak McClelland, Maier & Neustadt, L.L.P.
SNECMA
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