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 代理人
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