发明名称 APPARATUS FOR MOUNTING A BLADE ON A TURBINE DISK
摘要 A turbine wheel or disk having a plurality of dovetail slots formed in its circumference for receiving a dovetail root of a blade such as a compressor or turbine blade. Each of the dovetail slots has a load face positioned to oppose a centrifugal load exerted by the dovetail root when a turbine is in operation. Each of the dovetail slots has a pair of opposing acute bottom corners formed between a radially inner edge of the load face and a bottom of the dovetail slot. Each of the acute bottom corners may have an undercut formed that includes a first radius of curvature and a second radius of curvature to form a clearance between the dovetail root and the dovetail slot. Each of the dovetail slots may have a curved bottom for receiving a rounded dovetail root.
申请公布号 US2016312629(A1) 申请公布日期 2016.10.27
申请号 US201615096453 申请日期 2016.04.12
申请人 Evans Charles;Narcus Andrew;DiCristoforo Paul 发明人 Evans Charles;Narcus Andrew;DiCristoforo Paul
分类号 F01D5/30;F01D5/02;F01D5/12;F04D29/32 主分类号 F01D5/30
代理机构 代理人
主权项 1. A turbine disk comprising: a dovetail slot formed in a circumference of the turbine disk for receiving a dovetail root of a blade; a load face in the dovetail slot, the load face positioned to oppose a centrifugal load exerted by the dovetail root; an acute bottom corner formed in the dovetail slot between a radially inner edge of the load face and a bottom of the dovetail slot; and an undercut formed in the acute bottom corner that widens a portion of the dovetail slot beyond a width of the dovetail root.
地址 Tequesta FL US
您可能感兴趣的专利