A gas turbine engine has a surface cooler having a cooler member defining a fluid passage
and at least partially contained in an airfoil shaped flow guide member. The cooler member …

2020-12-18 Assigned to UNITED TECHNOLOGIES CORPORATION reassignment UNITED
TECHNOLOGIES CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE …

The invention relates to an assembly for a turbine engine (1), the assembly including: a
casing (20) extending along a longitudinal axis (XX′) of the turbine engine (1), a surface …

(57) ABSTRACT A heat exchanger includes a plurality of fins arranged as a network and
delimiting corridors, and an envelope having an internal wall and an external wall, the …

(57) ABSTRACT A heat exchanger includes a metal tube and a composite polymer fin in
thermal contact with the metal tube. The fin is formed of a polymer and a thermally …

A thermal management system for a geared architecture of a gas turbine engine includes an
evaporator portion located at the geared architecture and configured to exchange thermal …

Geared turbo fan engines are capable of offering higher propulsive efficiencies when
compared to conventional gas turbine engines. This is achieved by providing a gearbox …

2021-08-17 Assigned to GENERAL ELECTRIC COMPANY reassignment GENERAL
ELECTRIC COMPANY ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR …

A combustor for a gas turbine engine includes a combustor liner with a wall defining a
combustion chamber. The wall has an inner surface facing the combustion chamber and an …

The gas turbine engine described includes a first centrifugal compressor, a second
centrifugal compressor, and intercompressor pipes extending therebetween. The …