发明名称 Rotor of a turbomachine, in particular gas turbine rotor
摘要 <p>The rotor has a rotor base unit with a groove extending in circumferential direction of the unit, and a set of rotor blades. Each rotor blade has a blade platform positioned between a blade and a blade root (24). The groove and the root are profiled so that the root is inserted to the groove by tilt or swivel motion. The root is dimensioned in the direction such that width of the root corresponds to width of the platform. An independent claim is also included for a gas turbine comprising a rotor.</p>
申请公布号 EP1650405(A1) 申请公布日期 2006.04.26
申请号 EP20050022065 申请日期 2005.10.10
申请人 MTU AERO ENGINES GMBH 发明人 KLINGELS, HERMANN
分类号 F01D5/30 主分类号 F01D5/30
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