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 |
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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