发明名称 |
DEVICE, SYSTEM AND METHOD FOR PREVENTING LEAKAGE IN A TURBINE |
摘要 |
A turbine disk and blade assembly comprises a turbine disk including a plurality of disk posts extending radially therefrom and a plurality of disk slots between adjacent disk posts. The turbine disk is of a first material having a first coefficient of thermal expansion. The assembly further comprises a plurality of turbine blades. One of the turbine blades is received in each disk slot. The turbine blades are of a second material having a second coefficient of thermal expansion. The assembly further comprises a plurality of seal plates, wherein one of the seal plates is positioned in each disk slot radially inward of the turbine blade. The seal plates are of a material having a coefficient of thermal expansion substantially similar to that of either the disk posts or the turbine blade. |
申请公布号 |
US2014286756(A1) |
申请公布日期 |
2014.09.25 |
申请号 |
US201313790758 |
申请日期 |
2013.03.08 |
申请人 |
General Electric Company |
发明人 |
Hile Michael Alan;Agnew Brian;Grooms James Hamilton;Jendrix Richard William |
分类号 |
F01D11/00;B23P15/00;F01D5/30 |
主分类号 |
F01D11/00 |
代理机构 |
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代理人 |
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主权项 |
1. A turbine disk and blade assembly, comprising:
a turbine disk including a plurality of disk posts extending radially therefrom and a plurality of disk slots between adjacent disk posts, said turbine disk being of a first material having a first coefficient of thermal expansion; a plurality of turbine blades, one of said turbine blades being received in each said disk slot, said turbine blades being of a second material having a second coefficient of thermal expansion; and a plurality of seal plates, wherein one of said seal plates is positioned in each disk slot radially inward of the turbine blade, said seal plates being of a material having a coefficient of thermal expansion substantially similar to that of either said disk posts or said turbine blade such that said seal plates thermally expand or contract an amount similar to a thermal expansion or contraction of at least one of the plurality of disk posts or the plurality of turbine blades. |
地址 |
US |