Invention Grant
US08365536B2 Dual fuel combustor nozzle for a turbomachine 有权
用于涡轮机的双燃料燃烧器喷嘴

Dual fuel combustor nozzle for a turbomachine
Abstract:
A dual fuel combustor nozzle includes a body member including a first end portion that extends to a second end portion through an intermediate portion. The intermediate portion includes an outer wall portion and an inner wall portion with the inner wall portion defining a first fuel plenum. The dual fuel nozzle also includes an inner nozzle member arranged within the first fuel plenum. The inner nozzle member includes a first end section that extends to a second end section through an intermediate section. The intermediate section defines a second fuel plenum. The second end section being spaced from the second end portion of the body member so as to define a pre-emergence zone.
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