公开(公告)号：US20160356182A1

公开(公告)日：2016-12-08

申请号：US14730958

申请日：2015-06-04

Applicant: General Electric Company

Inventor： Joseph Daniel Becker ,  John William Herbold

IPC: F01D25/28

CPC classification number: F01D25/285 ,  B23P11/02 ,  B23P2700/13 ,  F01D9/023 ,  F05D2230/644 ,  Y10T29/49323 ,  Y10T29/4987

Abstract: Various embodiments include approaches for installing a flow sleeve relative to a gas turbine transition piece. Some embodiments include an apparatus for coupling a gas turbine transition piece with a flow sleeve, the installation apparatus having: a radially inner ring; a plurality of expander segments extending radially outward from the radially inner ring, the plurality of expander segments each having an axially ramped segment sized to gradually expand the flow sleeve to couple with the gas turbine transition piece as the flow sleeve is moved along the plurality of expander segments; and a circumferentially disposed space separating each pair of adjacent expander segments in the plurality of expander segments.

Abstract translation: 各种实施例包括相对于燃气轮机过渡件安装流动套筒的方法。 一些实施例包括用于将燃气轮机过渡件与流动套管联接的装置，该装置具有：径向内环; 多个从径向内环径向向外延伸的膨胀器段，所述多个膨胀器段各自具有轴向倾斜的段，其尺寸被设计成随着流动套筒沿着多个 扩展器段 以及分隔在多个膨胀器段中的每对相邻膨胀器段的周向设置空间。