Heat exchanger assembly configuration for a gas turbine engine

Abstract

A gas turbine engine defines a radial direction and an axial direction. The gas turbine engine includes an inlet duct comprising a splitter, a fan duct downstream from the inlet duct and the splitter, and a core duct downstream of the inlet duct and the splitter. The core duct may be radially inward of the fan duct. A heat exchanger assembly may extend annularly about at least one of the inlet duct, the fan duct, or the core duct. The heat exchanger assembly may include a sheet extending circumferentially about the at least one of the inlet duct, the fan duct, and the core duct. One or more aerodynamic features extend from the sheet, the one or more aerodynamic features within the at least one of the inlet duct, the fan duct, and the core duct.

Dependencies are inferred from the claim text.