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(A3)
申请公布日期
2016.12.21
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
