发明名称 Turbomachine bucket having angel wing for differently sized discouragers and related methods
摘要 A turbomachine bucket may include an airfoil, a shank coupled to the airfoil, and an angel wing coupled to the shank, the angel wing having an axially extending tip sized to seal with a plurality of discouragers, each discourager having a different axial extent. Various methods for modifying an angel wing to accommodate different sized discouragers are also disclosed.
申请公布号 US9638051(B2) 申请公布日期 2017.05.02
申请号 US201314017690 申请日期 2013.09.04
申请人 General Electric Company 发明人 Lewis Gareth William David;Grafitti Andrew Daniel;Lomas Jonathan Matthew;Roman-Morales Felipe;Souther Ronald Lee
分类号 F01D25/24;F04D3/00;F04D19/00;F01D11/02;F01D5/14;B23P15/04;B23P6/00;F01D5/00;F01D5/28;F01D11/00 主分类号 F01D25/24
代理机构 Hoffman Warnick LLC 代理人 Cusick Ernest G.;Hoffman Warnick LLC
主权项 1. A turbomachine bucket comprising: an airfoil; a shank coupled to the airfoil; and an angel wing, the angel wing having a base portion, a body portion, and an axially extending tip, the angel wing coupled to the shank by the base portion, the body portion connecting the base portion with the axially extending tip, the axially extending tip having a foundation tip, a sealing surface, and an attached material section, the axially extending tip sized to seal with a plurality of discouragers, each discourager having a different axial extent, the foundation tip and the sealing surface having an initial axial extent, the axially extending tip being parallel to an axis of rotation of the turbomachine bucket, the attached material section extending the initial axial extent of the foundation tip and the sealing surface.
地址 Schenectady NY US