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:
May. 16, 2023

Filed:

Sep. 24, 2021
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Stephen J Bradbrook, Bristol, GB;

Martin N Goodhand, Bristol, GB;

Paul M Hield, Bristol, GB;

Andrew Parsley, Bristol, GB;

Natalie C Wong, Bristol, GB;

Robert J Corin, Bristol, GB;

Thomas S Binnington, Bristol, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/18 (2006.01); F02C 6/08 (2006.01); F28D 9/00 (2006.01); B64D 33/02 (2006.01); F28D 21/00 (2006.01);
U.S. Cl.
CPC ...
F02C 7/185 (2013.01); F02C 6/08 (2013.01); F28D 9/0018 (2013.01); B64D 2033/0286 (2013.01); F05D 2260/20 (2013.01); F28D 2021/0021 (2013.01);
Abstract

A turbofan gas turbine engine includes, in axial flow sequence, a heat exchanger module, a fan assembly, a compressor module, a turbine module, and an exhaust module. The fan assembly includes a plurality of fan blades defining a fan diameter (D). The heat exchanger module is in fluid communication with the fan assembly by an inlet duct, and the heat exchanger module includes a plurality of radially-extending hollow vanes arranged in a circumferential array with a channel extending axially between each pair of adjacent hollow vanes. An airflow entering the heat exchanger module is divided between a set of vane airflows through each of the hollow vanes and a set of channel airflows through each of the channels.


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