发明申请
US20120128476A1 NOZZLE STAGE FOR A TURBINE ENGINE 审中-公开
涡轮发动机喷嘴级

NOZZLE STAGE FOR A TURBINE ENGINE
摘要:
A nozzle stage for a turbine engine includes two substantially cylindrical rings, respectively an inner ring and an outer ring, with, extending between them: vanes carried by a first one of the rings; vanes carried by the second ring; and spacer-forming vanes interconnecting the two rings; the vanes of the first and second rings being arranged in alternation.
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