INTEGRATED THERMAL SYSTEM FOR A GAS TURBINE ENGINE
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).
Saved in:
Main Authors | , , , , |
---|---|
Format | Patent |
Language | English French German |
Published |
28.07.2021
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Summary: | 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). |
---|---|
Bibliography: | Application Number: EP20120188711 |