Cowl structure for a gas turbine engine

Details Cowl structure for a gas turbine engine Cowl structure for a gas turbine engine

2006-08-08

2006-08-08

Koczo, Jr., Michael (Department: 3746)

Power plants

Reaction motor

Interrelated reaction motors

C060S799000, C244S05300R

Reexamination Certificate

active

07086219

ABSTRACT:
A cowl structure (18) for a gas turbine engine (10) comprises an outer skin (26) defining a first path for a load applied to the engine (10). The cowl structure (18) includes an inner skin (24) defining a second path for the load. The inner and outer skins (24, 26) are constructed such that a major proportion of the load is transmitted along the first path.

REFERENCES:
patent: 4361296 (1982-11-01), Hall et al.
patent: 5524847 (1996-06-01), Brodell et al.
patent: 5609313 (1997-03-01), Cole et al.
patent: 5941061 (1999-08-01), Sherry et al.
patent: 6360989 (2002-03-01), Maguire
patent: 6729140 (2004-05-01), Care et al.

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