Integrated thermal system for a gas turbine engine
摘要
An integrated thermal system (80) for a gas turbine engine (20) includes an Air-Oil Cooler (88) and an Air-Air PreCooler (92) within a housing (89), the Air-Air PreCooler (92) being downstream of the Air-Oil Cooler (88).
申请公布号
EP2584168(A2)
申请公布日期
2013.04.24
申请号
EP20120188711
申请日期
2012.10.16
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
SUCIU, GABRIEL L.;PENDA, ALLAN R.;MERRY, BRIAN D.;DYE, CHRISTOPHER M.;SNAPE, NATHAN
