Aeronautics and astronautics – Aircraft power plants – Mounting
Reexamination Certificate
2007-09-11
2007-09-11
Swiatek, Robert P. (Department: 3644)
Aeronautics and astronautics
Aircraft power plants
Mounting
Reexamination Certificate
active
11116260
ABSTRACT:
An aircraft engine includes a mounting attached to an aircraft structure and transmitting forces between an engine casing and the aircraft structure. The mounting includes a fail safe assembly with a safety clevis with two lugs and a tab arranged between the two lugs. Either the clevis or the tab is fixed to an element of the engine casing and the other tab or clevis is fixed to the structure. A safety hinge pin is perpendicular to the axis of the engine and passes through the tab and the clevis, the two lugs and the tab being parallel to the engine axis.
REFERENCES:
patent: 4326682 (1982-04-01), Nightingale
patent: 4603821 (1986-08-01), White
patent: 5303880 (1994-04-01), Cencula et al.
patent: 5351930 (1994-10-01), Gwinn et al.
patent: 5474258 (1995-12-01), Taylor et al.
patent: 5620154 (1997-04-01), Hey
patent: 5649417 (1997-07-01), Hey
patent: 5725181 (1998-03-01), Hey
patent: 5860623 (1999-01-01), Dunstan et al.
patent: 5921500 (1999-07-01), Ellis et al.
patent: 5927644 (1999-07-01), Ellis et al.
patent: 6170252 (2001-01-01), Van Duyn
patent: 6330995 (2001-12-01), Mangeiga et al.
patent: 6682015 (2004-01-01), Levert et al.
patent: 6843449 (2005-01-01), Manteiga et al.
patent: 6988692 (2006-01-01), Pasquer et al.
patent: 0 997 653 (2000-05-01), None
patent: 2 799 432 (2001-04-01), None
Holzen Stephen A
Snecma Moteurs
Swiatek Robert P.
LandOfFree
Aircraft engine with means of suspension from the structure... does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Aircraft engine with means of suspension from the structure..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft engine with means of suspension from the structure... will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-3777916