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. 25, 2024

Filed:

Jul. 25, 2023
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventor:

William G. Sheridan, Southington, CT (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/18 (2006.01); B01D 19/00 (2006.01); F01D 25/20 (2006.01); F02C 7/06 (2006.01);
U.S. Cl.
CPC ...
F01D 25/18 (2013.01); B01D 19/0068 (2013.01); B01D 19/0073 (2013.01); F01D 25/20 (2013.01); F02C 7/06 (2013.01); F05D 2260/609 (2013.01); Y02T 50/60 (2013.01);
Abstract

A gas turbine engine has a fan drive turbine for driving a gear reduction. The gear reduction drives a fan rotor. A lubrication system supplies oil to the gear reduction, and includes a lubricant pump to supply an air/oil mixture to an inlet of a deaerator. The deaerator includes a separator for separating oil and air, delivering separated air to an air outlet, and delivering separated oil back into an oil tank. The separated oil is first delivered into a pipe outwardly of the oil tank, and then into a location beneath a minimum oil level in the tank. Air within the oil tank moves outwardly through an air exit into the deaerator. A method of designing a gas turbine engine is also disclosed.


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