Gas turbine engine compressor case mounting arrangement

Details Gas turbine engine compressor case mounting arrangement Gas turbine engine compressor case mounting arrangement

2007-09-21

2011-12-13

Edgar, Richard (Department: 3745)

Rotary kinetic fluid motors or pumps

Working fluid passage or distributing means associated with...

Access opening through portion of casing or cover

C415S213100

Reexamination Certificate

active

08075261

ABSTRACT:
A compressor case support arrangement for a gas turbine engine includes a fan section having a central axis and a compressor case for housing a compressor. An inlet case guides air to the compressor. The compressor case is positioned axially further from the fan section than the inlet case. A support member extends between the fan section and the compressor case. The support member restricts movement of the compressor case relative to the inlet case. The support member is positioned axially further from the fan section than the plumbing access area.

REFERENCES:
patent: 4790137 (1988-12-01), Quinn
patent: 5174525 (1992-12-01), Schilling
patent: 5180281 (1993-01-01), Burge et al.
patent: 5180282 (1993-01-01), Lenhart et al.
patent: 5354174 (1994-10-01), Balkeum et al.
patent: 5452575 (1995-09-01), Freid
patent: 5642615 (1997-07-01), Porte et al.
patent: 5653581 (1997-08-01), Dixon et al.
patent: 5860275 (1999-01-01), Newton et al.
patent: 6145300 (2000-11-01), Romani
patent: 7634916 (2009-12-01), Mace et al.
patent: 2005/0022501 (2005-02-01), Eleftheriou et al.
patent: 2005/0109013 (2005-05-01), Eleftheriou et al.

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