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US07752850B2 Controlled pilot oxidizer for a gas turbine combustor 失效
用于燃气轮机燃烧器的控制先导氧化器

Controlled pilot oxidizer for a gas turbine combustor
摘要:
A combustor (22) for a gas turbine (10) includes a main burner oxidizer flow path (34) delivering a first portion (32) of an oxidizer flow (e.g., 16) to a main burner (28) of the combustor and a pilot oxidizer flow path (38) delivering a second portion (36) of the oxidizer flow to a pilot (30) of the combustor. The combustor also includes a flow controller (42) disposed in the pilot oxidizer flow path for controlling an amount of the second portion delivered to the pilot.
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