The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Dec. 24, 2024

Filed:

May. 15, 2023
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Neil J. Terwilliger, Cheshire, CT (US);

Simon W. Evans, Farmington, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/042 (2006.01); F02C 7/141 (2006.01); F02C 7/18 (2006.01); F02K 1/06 (2006.01); F02K 3/077 (2006.01); F02C 7/04 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/042 (2013.01); F02C 7/141 (2013.01); F02C 7/185 (2013.01); F02K 1/06 (2013.01); F02K 3/077 (2013.01); F02C 7/04 (2013.01); F02K 3/06 (2013.01);
Abstract

A propulsion system is provided for an aircraft. This propulsion system includes a turbine engine, and the turbine engine includes a propulsor rotor, an engine core and a heat exchanger. The propulsor rotor is configured to rotate about an axis and direct a first air stream along a primary flowpath that bypasses the engine core. The propulsor rotor is configured to direct a second air stream along a secondary flowpath with a geometry extending at least eighty degrees about the axis. The turbine engine is configured such that the first air stream enters the primary flowpath at a first pressure and the second air stream enters the secondary flowpath at a second pressure that is different than the first pressure. The engine core is configured to drive rotation of the propulsor rotor. The heat exchanger is disposed within the secondary flowpath.


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