RTX Corporation
MULTI-MODE HEAT REJECTION SYSTEM
Last updated:
Abstract:
A turbine engine includes a duct defining an annular passage, at least two heat exchangers arranged within the annular passage and spaced circumferentially apart, a passage between the at least two heat exchangers, and a forward flow control device operable for controlling airflow through the passages.
Status:
Application
Type:
Utility
Filling date:
5 May 2020
Issue date:
19 Nov 2020