发明名称 SLOTS FOR TURBOMACHINE STRUCTURES
摘要 A component for a turbomachine includes an annular body defining an inner diameter portion and an outer diameter portion, and a crack guiding slot defined in a surface of the annular body extending from the inner diameter portion radially outward toward the outer diameter portion or extending from the outer diameter portion radially inward toward the inner diameter portion. The outer diameter portion can be mountable to a stationary structure of a turbomachine. The inner diameter portion can be mountable to a turbine vane.
申请公布号 US2016169039(A1) 申请公布日期 2016.06.16
申请号 US201514969426 申请日期 2015.12.15
申请人 United Technologies Corporation 发明人 Hayford Richard K.;Bruskotter Michael J.;Vandenbosch Ross A.
分类号 F01D25/12;F01D25/24 主分类号 F01D25/12
代理机构 代理人
主权项 1. A component for a turbomachine, comprising: an annular body defining an inner diameter portion and an outer diameter portion; and a crack guiding slot defined in a surface of the annular body extending from the inner diameter portion radially outward toward the outer diameter portion or extending from the outer diameter portion radially inward toward the inner diameter portion.
地址 Farmington CT US