发明名称 Adjustable guide vane for turbines, compressors, or the like
摘要 A guide vane for an axial guide baffle of an axial flow engine, such as a jet engine, is adjustable in its position about a guide vane adjustment axis extending radially to a rotational engine axis. The guide vane has a vane body and an adjustment lever extending at an angle of about 90 DEG away from the adjustment axis. The vane body, the adjustment lever, and at least one bearing journal form an integral one piece construction either of molded fiber composite material or of forged, e.g. drop forged, metal.
申请公布号 US5380152(A) 申请公布日期 1995.01.10
申请号 US19930144575 申请日期 1993.10.28
申请人 MTU MOTOREN-UND TURBINEN-UNION MUENCHEN GMBH 发明人 SIKORSKI, SIEGFRIED;SCHOBER, MICHAEL;SCHOENACHER, REINHOLD
分类号 B29D99/00;F01D5/28;(IPC1-7):F01D9/02 主分类号 B29D99/00
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