Gas turbine engine reheat systems

Details Gas turbine engine reheat systems Gas turbine engine reheat systems

1978-03-02

2011-11-22

Collins, Timothy D (Department: 3644)

Power plants

Reaction motor

Having afterburner

C060S749000, C060S266000

Reexamination Certificate

active

08061143

ABSTRACT:
A gas turbine reheat system is provided with channel-shaped gutters, with a wall portion spaced from each gutter to form a space therebetween. The space is supplied with cooling air conveniently from the engine by-pass duct.

REFERENCES:
patent: 3315468 (1967-04-01), Vdoviak
patent: 3595024 (1971-07-01), Kohler et al.
patent: 3698186 (1972-10-01), Beane et al.

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