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:
Sep. 08, 2020

Filed:

Sep. 11, 2018
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Daniel S. Rogers, Lyman, ME (US);

Taryn Narrow, Glastonbury, CT (US);

Gregory E. Reinhardt, South Glastonbury, CT (US);

Collin P. Fitzgerald, South Glastonbury, CT (US);

Christopher M. Valva, Manchester, CT (US);

Leonard Kolshak, Lake Worth, FL (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/06 (2013.01); F05D 2240/50 (2013.01); F05D 2240/55 (2013.01); F05D 2260/98 (2013.01); F16N 2210/02 (2013.01); F16N 2210/08 (2013.01); F16N 2210/14 (2013.01);
Abstract

A bearing assembly for a gas turbine engine includes, among other things, a bearing housing extending along an axis to define a bearing compartment, a lubricant seal assembly adjacent to the bearing housing to bound the bearing compartment, an air seal assembly defining a vent cavity along the bearing housing, wherein a mixing cavity is defined between the lubricant seal assembly and the air seal assembly, and wherein the bearing housing defines an airflow supply passage, an airflow vent passage and a scupper passage having respective fluid ports at different circumferential positions relative to the axis, the fluid port of the airflow vent passage fluidly coupled to the vent cavity, and the fluid ports of the airflow supply and scupper passages fluidly coupled to the mixing cavity. A method of sealing for a gas turbine engine is also disclosed.


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