Annular torsional rigid static component for an aircraft engine

Details Annular torsional rigid static component for an aircraft engine Annular torsional rigid static component for an aircraft engine

2011-03-15

2011-03-15

Dinh, Tien (Department: 3644)

Aeronautics and astronautics

Aircraft power plants

Mounting

C060S796000, C060S797000, C248S554000, C248S557000, C415S213100, C415S126000

Reexamination Certificate

active

07905448

ABSTRACT:
In an annular torsional rigid static component for an aircraft engine, the component includes at least one arrangement for mounting the engine to an aircraft. The mounting arrangement comprises a body formed in a composite material.

REFERENCES:
patent: 3042349 (1962-07-01), Pirtle et al.
patent: 4132069 (1979-01-01), Adamson et al.
patent: 4859143 (1989-08-01), Larrabee et al.
patent: 5160676 (1992-11-01), Singh et al.
patent: 5174525 (1992-12-01), Schilling
patent: 5275357 (1994-01-01), Seelen et al.
patent: 5452575 (1995-09-01), Freid
patent: 5467941 (1995-11-01), Chee
patent: 5484120 (1996-01-01), Blakeley et al.
patent: 5746391 (1998-05-01), Rodgers et al.
patent: 5860275 (1999-01-01), Newton et al.
patent: 6126110 (2000-10-01), Seaquist et al.
patent: 6223524 (2001-05-01), Durcan
patent: 6401448 (2002-06-01), Manteiga et al.
patent: 6474596 (2002-11-01), Cousin et al.
patent: 6547518 (2003-04-01), Czachor et al.
patent: 2003/0015623 (2003-01-01), Gladstone et al.
patent: 2004083605 (2004-09-01), None
International Search Report for corresponding International Application PCT/SE2005/001976.
International Preliminary Report on Patentability for corresponding International Application PCT/SE2005/001976.

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