发明名称 Turbomachine e.g. gas turbine, has at least one guide blade or at least one guide blade segment of several guide blades assigned within region of outer covering strip
摘要 <p>The turbomachine (10) has at least a guide blade (14) or at least a guide blade segment (13) of several guide blades assigned within the region of an outer covering strip (17) with radially outward extending projections (20) and at least a pin (21) extending through the housing (11). The projection with the pin limits mobility of guide blades or guide blade segments in circumferential direction.</p>
申请公布号 DE102005006045(A1) 申请公布日期 2006.08.17
申请号 DE20051006045 申请日期 2005.02.10
申请人 MTU AERO ENGINES GMBH 发明人 MCARTHUR, SCOTT
分类号 F01D9/04 主分类号 F01D9/04
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