Gas turbine engines

Details Gas turbine engines Gas turbine engines

1978-03-02

2011-11-22

Collins, Timothy D (Department: 3644)

Power plants

Reaction motor

Having afterburner

C060S749000, C060S262000, C060S266000

Reexamination Certificate

active

08061144

ABSTRACT:
In a by-pass gas turbine engine having a lobed type by-pass air and turbine exhaust mixer unit, the reheat gutters are arranged in the mixer in the turbine exhaust duct. The gutters extend radially and are substantially Y-shaped, each of the two legs of the Y extending radially along the sides of a mixer lobe.

REFERENCES:
patent: 3118276 (1964-01-01), Keenan et al.
patent: 3698186 (1972-10-01), Beane et al.
patent: 4134260 (1979-01-01), Lefebvre et al.

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