发明名称 Radial turbine used as part of exhaust gas turbocharger for reciprocating piston engine comprises inlet coating arranged on inside of housing and comprising metallic matrix and lubricating or sliding additive
摘要 <p>A radial turbine comprises an inlet coating arranged on the inside of a housing and comprising a metallic matrix based on nickel, cobalt and/or iron and a lubricating or sliding additive in the form of hexagonal boron nitride, bentonite and/or graphite. An independent claim is also included for the production of a radial turbine.</p>
申请公布号 DE102005033588(A1) 申请公布日期 2007.01.25
申请号 DE20051033588 申请日期 2005.07.19
申请人 MTU AERO ENGINES GMBH 发明人 FANDEL, MARCO;HERTTER, MANUEL;KRAENZLER, THOMAS;STEINWANDEL, JUERGEN
分类号 F01D11/12 主分类号 F01D11/12
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