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:
Jun. 08, 2021

Filed:

Aug. 23, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Steve G. Mackin, Bellevue, WA (US);

Samuel J. Tutko, Covington, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/14 (2006.01); F01D 25/20 (2006.01); F01M 5/00 (2006.01); F02C 6/08 (2006.01); F02C 7/18 (2006.01); F02C 9/18 (2006.01); F02C 3/32 (2006.01);
U.S. Cl.
CPC ...
F02C 7/14 (2013.01); F01D 25/20 (2013.01); F01M 5/002 (2013.01); F02C 6/08 (2013.01); F02C 7/18 (2013.01); F02C 9/18 (2013.01); F02C 3/32 (2013.01); F05D 2260/213 (2013.01); F05D 2260/601 (2013.01); F05D 2260/98 (2013.01);
Abstract

An aircraft engine system has a turbofan engine with a lubricating oil system. An oil pump is connected to pump oil from the oil tank through a cooling circuit to the turbofan engine. The cooling circuit has a bleed air boosted engine oil cooler assembly with a liquid/air heat exchanger (LAHEX) connected to an oil inlet conduit and receiving fan air from a high bypass fan of the turbofan engine as the cooling working fluid. The LAHEX is connected to an oil exit conduit. An ejector downstream of the LAHEX receives bleed air from a compressor section of the turbofan engine. The ejector draws the fan air through the LAHEX.


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