发明名称 Rotor of a turbomachine
摘要 A rotor of a turbomachine. The rotor includes at least one blade (4, 6, 8) that has a blade leaf (20) and a blade root (54, 55, 58), and a rotor base body (2), in particular a disk (2), that has an outwardly open, circumferential groove (12) for receiving the blade root (54, 55, 58). The circumferential groove (12) and the blade root (54, 55, 58) are shaped in a way that allows the blade root (54, 55, 58) to be secured in the circumferential groove (12) by the rotation of the blade (4, 6, 8) about an axis (Ar, AT).
申请公布号 US2015139808(A1) 申请公布日期 2015.05.21
申请号 US201414546699 申请日期 2014.11.18
申请人 MTU Aero Engines AG 发明人 Kloetzer Alexander;Hofmann Dieter
分类号 F01D5/30 主分类号 F01D5/30
代理机构 代理人
主权项
地址 Muenchen DE