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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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