Fuel manifold inlet tube

Power plants – Combustion products used as motive fluid – Combustion products generator

Reexamination Certificate

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Details

C060S740000

Reexamination Certificate

active

07451599

ABSTRACT:
An inlet tube supplies fuel to a manifold of a combustor in a gas turbine engine, the manifold defining a manifold plane. The inlet tube comprises a tube body having a channel providing fluid flow communication between first and second ends of the tube body. At least a portion of the channel defines a tube body plane which is spaced apart from the manifold plane.

REFERENCES:
patent: 3213523 (1965-10-01), Boehler
patent: 3879940 (1975-04-01), Stenger et al.
patent: 4185462 (1980-01-01), Morse, II et al.
patent: 4467610 (1984-08-01), Pearson et al.
patent: 4499735 (1985-02-01), Moore et al.
patent: 5076242 (1991-12-01), Parker
patent: 5259185 (1993-11-01), Peterson
patent: 5261240 (1993-11-01), Oyler et al.
patent: 5263314 (1993-11-01), Anderson
patent: 5279112 (1994-01-01), Halila
patent: 5771696 (1998-06-01), Hansel et al.
patent: 6354085 (2002-03-01), Howell et al.

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