A cooling fluid system for a gas turbine engine (20) includes a fluid source (52). A turbine section (28) includes first and second components (59, 68). A fluid supply system has a primary pipe (60) that is configured to provide a cooling supply fluid from the fluid source to a fluid fitting (62) having a fluid junction. The fluid junction is in fluid communication with and is configured to supply a first cooling fluid to the first component (59) and to supply a second cooling fluid to the second component (68). A flow meter (64) is upstream from the fluid junction and is configured to receive the cooling supply fluid.
申请公布号
EP2985425(A1)
申请公布日期
2016.02.17
申请号
EP20150181153
申请日期
2015.08.14
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
MOSLEY, JOHN H.;STEARNS, MICHELLE DIANA;COMEAU, MICHAEL LUTHER;CHASSE, JAMES P.