发明申请
US20110243742A1 STATOR STAGE FOR TURBOMACHINE COMPRESSOR 有权
涡轮压缩机的定期阶段

STATOR STAGE FOR TURBOMACHINE COMPRESSOR
摘要:
A turbomachine stator stage comprising two coaxial shrouds, respectively an inner shroud and an outer shroud with substantially radial vanes extending therebetween, the radially outer ends of the vanes being welded to the outer shroud and the radially inner ends of the vanes passing through orifices in an outer ring of the inner shroud, the inner ends being held by elastomer spacers in an annular cavity formed between the outer ring and an inner ring that is fastened to the outer ring.
公开/授权文献
信息查询
0/0