发明名称 Rotor i.e. integral bladed rotor for gas turbine, has shrouding band covering outer edge of rotor base body and forming internal flow channel, and retaining element fastening shrouding band to rotor base body
摘要 <p>The rotor (10) has a set of blades (14) integrally fastened to a rotor base body (12) by friction welding or inductive high frequency pressure welding. A separate shrouding band (16) covers an outer edge (22) of the rotor base body and forms an internal flow channel. A retaining element (24) fastens the shrouding band to the rotor base body. A welding seam is arranged in an area between the rotor base body and the shrouding band. The blades are manufactured by die forging and milling at a flow through surface. The shrouding band is manufactured from fiber-reinforced plastic.</p>
申请公布号 DE102009023841(A1) 申请公布日期 2010.12.09
申请号 DE20091023841 申请日期 2009.06.04
申请人 MTU AERO ENGINES GMBH 发明人 TOMSIK, JOSEPH
分类号 F01D5/22;F01D5/08;F01D5/30;F01D5/34 主分类号 F01D5/22
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