Engine fueling method

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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Details

C060S039281, C060S736000, C431S011000, C431S207000

Reexamination Certificate

active

11184264

ABSTRACT:
A gas turbine engine is piloted with a pilot flow of fuel delivered to a combustor as a liquid. A first additional flow of the fuel is also delivered to the combustor as a liquid. A second additional flow of the fuel is vaporized and delivered to the combustor as a vapor. A fuel injector may have passageways associated with each of the three flows.

REFERENCES:
patent: 5584171 (1996-12-01), Sato et al.
patent: 6105370 (2000-08-01), Weber

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