公开(公告)号：US09610644B2

公开(公告)日：2017-04-04

申请号：US13022641

申请日：2011-02-08

申请人： Andy Turko ,  Tracy A. Propheter-Hinckley

发明人： Andy Turko ,  Tracy A. Propheter-Hinckley

IPC分类号： F01D9/04 ,  B23K1/00 ,  B23K101/00

CPC分类号： B23K1/0018 ,  B23K2101/001 ,  F01D9/044 ,  F05D2230/237 ,  Y10T29/49229

摘要： A turbine component is formed of at least a plurality of adjacent turbine subcomponents. Each turbine component has a mate face secured to the mate face of an opposed turbine subcomponent. A wedge member is positioned between the mate faces of the turbine subcomponents, and a braze material between outer faces of the wedge and the mate faces of each of the turbine subcomponents.

公开(公告)号：US20120201684A1

公开(公告)日：2012-08-09

申请号：US13022641

申请日：2011-02-08

申请人： Andy Turko ,  Tracy A. Propheter-Hinckley

发明人： Andy Turko ,  Tracy A. Propheter-Hinckley

IPC分类号： F01D5/30 ,  B23P17/00

CPC分类号： B23K1/0018 ,  B23K2101/001 ,  F01D9/044 ,  F05D2230/237 ,  Y10T29/49229

摘要： A turbine component is formed of at least a plurality of adjacent turbine subcomponents. Each turbine component has a mate face secured to the mate face of an opposed turbine subcomponent. A wedge member is positioned between the mate faces of the turbine subcomponents, and a braze material between outer faces of the wedge and the mate faces of each of the turbine subcomponents.

摘要翻译： 涡轮机部件由至少多个相邻的涡轮机子部件形成。 每个涡轮机部件具有固定到相对的涡轮机副部件的配合面的配合面。 楔形构件位于涡轮机副部件的配合面之间，并且在楔形件的外表面与每个涡轮机副部件的配合面之间形成钎焊材料。