TURBINE SHROUD SEGMENT WITH BUFFER AIR SEAL SYSTEM
摘要
A turbine shroud adapted for use in a gas turbine engine includes a plurality of metallic carrier segments and a plurality of blade track segments mounted to corresponding metallic carrier segments. Cooling air is directed onto the blade track segments to cool the blade track segments when exposed to high temperatures in a gas turbine engine.
申请公布号
EP3115560(A1)
申请公布日期
2017.01.11
申请号
EP20160173211
申请日期
2016.06.07
申请人
Rolls-Royce Corporation;Rolls-Royce North American Technologies, Inc.
发明人
O'Leary, Mark;Vetters, Daniel K.;Brandt, Matthew R.;Freeman, Ted J.