Methods and apparatus for injecting fluids in gas turbine...

Details Methods and apparatus for injecting fluids in gas turbine... Methods and apparatus for injecting fluids in gas turbine...

2006-05-30

2006-05-30

Nguyen, Hoang (Department: 3748)

Rotary kinetic fluid motors or pumps

With passage in blade, vane, shaft or rotary distributor...

C415S116000, C415S175000, C416S09600A

Reexamination Certificate

active

07052231

ABSTRACT:
A method enables a nozzle support for a gas turbine engine to be fabricated. The method comprises forming an annular assembly including a plurality of circumferentially-spaced gas injector assemblies, wherein each gas injector assembly includes a plenum and a unitarily formed injector that extends outwardly from an outer surface of the plenum, and forming a passageway through the injector such that the passageway extends between an inlet and an outlet, and is obliquely aligned with respect to the plenum exterior surface.

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patent: 6224329 (2001-05-01), North
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patent: 6435816 (2002-08-01), Czachor

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