Run-on linings for turbo-engines are arranged between the free ends of moving blades and a housing of a compressor or a turbine of a turbo-engine. The run-on linings are formed of a carrier and fiber bundles and are fastened on the circumference of the housing.
申请公布号
US5622474(A)
申请公布日期
1997.04.22
申请号
US19950528053
申请日期
1995.09.14
申请人
MTU MOTOREN- UND TURBINEN-UNION MUENCHEN GMBH
发明人
WERNER, KLEMENS;LOTTES, PAUL;SCHMUHL, HANS-JUERGEN;REISINGER, LOTHAR;WYDRA, GERHARD;SCHULTE, DIETRICH
