发明名称 |
Verdichter in mehrstufiger Axialbauart |
摘要 |
Compressor comprises a cantilevered rotor (7) having several moving blade rings (4-6) on interconnected disk- and/or ring-shaped blade supports (11-13). At least one (12, 13) of the rotating blade supports is designed as a metal matrix composite, i.e. an at least partly fiber-reinforced metal component. The pivot bearing (18) absorbing at least the majority of the radial loads exerted on the rotor has a pre-determined breaking point (19) which, on exceeding a defined radial load, allows limited radial yielding of the rotor with subsequent contact with the stator (2) to reduce the speed, optionally to a complete stop. Preferred Features: The blade support has in the fiber-reinforced region (14-16) a metal matrix, preferably based on titanium, and at least one long fiber of silicon carbide arranged in windings. |
申请公布号 |
DE50304419(D1) |
申请公布日期 |
2006.09.14 |
申请号 |
DE2003504419 |
申请日期 |
2003.03.25 |
申请人 |
MTU AERO ENGINES GMBH |
发明人 |
ALBRECHT, GUENTER;TARTSCH, KLAUS-DIETER;TOMSIK, JOSEPH;WOEHRL, BERNHARD, DR. |
分类号 |
F04D19/02;F04D29/04;F01D21/04;F04D27/02;F04D29/02;F04D29/059;F04D29/10;F04D29/18 |
主分类号 |
F04D19/02 |
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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