发明名称 GUIDE VANE RING AND TURBOMACHINE
摘要 The invention is directed to a guide vane ring for a turbomachine, in which a vane bearing is produced in the inner ring via platform plates of the vanes and reliability against disintegration is produced via journals that extend radially inward from the platform plates, as well as a turbomachine.
申请公布号 US2016146027(A1) 申请公布日期 2016.05.26
申请号 US201514942342 申请日期 2015.11.16
申请人 MTU Aero Engines AG 发明人 Humhauser Werner;Klingels Hermann
分类号 F01D9/04;F01D17/14 主分类号 F01D9/04
代理机构 代理人
主权项 1. A guide vane ring (1) for a turbomachine, having a plurality of rotatable guide vanes (2) that are borne radially outward in the radial direction, and having an inner ring (4) for the radially inner stabilizing of the guide vanes (2), wherein each of the guide vanes has an inner platform plate (8), and by the cylindrical surface (12) of this plate, the vanes are guided by sliding in an uptake (14) of the inner ring (4), wherein a journal (10) extends radially inward from the platform plate (8) in each case, the journal having a minimum length (I) that is greater than a minimum depth (t) of the uptake (14), and being disposed without contact in a journal borehole (16) without relative axial offset, between the inner ring (4) and the guide vanes (2), this borehole passing through a bottom segment (18) of the respective uptake (14).
地址 Munich DE