Fuel nozzle attachment in gas turbine combustors

Details Fuel nozzle attachment in gas turbine combustors Fuel nozzle attachment in gas turbine combustors

1993-12-21

1995-11-14

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60740, 60748, F02C 722

Patent

active

054655714

ABSTRACT:
In a gas turbine, a linear stem extends through a diffuser and a combustor cowl into a sleeve that is attached to the swirler in such a way that the sleeve can move relative to the swirler but is supported on the swirler. The stem slides into the sleeve and contains a fuel nozzle that supplies fuel through a sleeve outlet to a swirler inlet.

REFERENCES:
patent: 3032990 (1962-05-01), Rogers
patent: 4441323 (1984-04-01), Colley
patent: 4453384 (1984-06-01), Pask
patent: 5020329 (1991-06-01), Ekstedt
patent: 5333459 (1994-08-01), Berger

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