发明申请
US20110067379A1 DUAL FUEL COMBUSTOR NOZZLE FOR A TURBOMACHINE 有权
双燃料燃烧器喷嘴用于涡轮发动机

DUAL FUEL COMBUSTOR NOZZLE FOR A TURBOMACHINE
摘要:
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.
公开/授权文献
信息查询
0/0