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 |
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代理人 |
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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 |