Integrated propulsive system comprising a bypass turbojet...

Details Integrated propulsive system comprising a bypass turbojet... Integrated propulsive system comprising a bypass turbojet...

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.

Affiliated with

Also associated with

Rating

Integrated propulsive system comprising a bypass turbojet... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Integrated propulsive system comprising a bypass turbojet..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Integrated propulsive system comprising a bypass turbojet... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-2742063