Cowling arrangement

Rotary kinetic fluid motors or pumps – With passage in blade – vane – shaft or rotary distributor...

Reexamination Certificate

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Details

C415S178000

Reexamination Certificate

active

08052377

ABSTRACT:
A gas turbine engine including a bypass duct defined by radially outer and inner walls, the radially inner wall defined by acoustic panels. The acoustic panels define the outer wall of a heated fire zone. In conventional engines an insulating blanket is attached to the panels, however, this is heavy and costly. Cooling film means are configured to pass bypass air through and over an internal surface of the panel.

REFERENCES:
patent: 6122892 (2000-09-01), Gonidec et al.
patent: 0 702 141 (1996-03-01), None
patent: 2 873 167 (2006-01-01), None
patent: 1 429 240 (1976-03-01), None
patent: 2 169 696 (1986-07-01), None
patent: 2 225 381 (1990-05-01), None
Rolls-Royce PLC. “The Jet Engine,” 5thEdition, p. 204 (1996).

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