A gas turbine engine includes a buffer system that includes a first circuit and a second circuit. The first circuit can communicate a first buffer supply air to a first portion of the gas turbine engine and the second circuit can communicate a second buffer supply air to a second portion of the gas turbine engine.
申请公布号
WO2013154633(A3)
申请公布日期
2013.12.05
申请号
WO2013US21641
申请日期
2013.01.16
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
GLAHN, JORN, A.;ACKERMANN, WILLIAM, K.;CRAWLEY, CLIFTON, J.;STRIPINIS, PHILIP, S.
