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
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