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:
Oct. 22, 2024

Filed:

Sep. 24, 2021
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Natalie C Wong, Bristol, GB;

Thomas S Binnington, Bristol, GB;

David A Jones, Bristol, GB;

Daniel Blacker, Bristol, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/18 (2006.01); F01D 25/12 (2006.01); F02C 7/04 (2006.01); F02C 7/143 (2006.01); F02K 3/065 (2006.01);
U.S. Cl.
CPC ...
F02C 7/18 (2013.01); F01D 25/12 (2013.01); F02C 7/04 (2013.01); F02C 7/143 (2013.01); F02C 7/185 (2013.01); F02K 3/065 (2013.01); F05D 2260/213 (2013.01); F05D 2260/232 (2013.01); F05D 2260/36 (2013.01); F05D 2260/606 (2013.01);
Abstract

A turbofan gas turbine engine comprises, in axial flow sequence, a heat exchanger module, a fan assembly, a compressor module, and a turbine module. The fan assembly comprises a plurality of fan blades defining a fan diameter (D), and the heat exchanger module comprises a plurality of heat exchanger elements. The heat exchanger module is in fluid communication with the fan assembly by an inlet duct, with the heat exchanger module having an axial length along a central axis between an upstream-most face of the heat exchanger elements and a downstream-most face of the heat exchanger elements. The axial length is in the range of 0.1*D to 5.0*D.


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