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:
Feb. 23, 2021

Filed:

May. 24, 2017
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Chao-Hsin Lin, Redmond, WA (US);

Raymond H. Horstman, Snohomish, WA (US);

George Bates, III, Bothell, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 29/08 (2006.01); F01D 25/18 (2006.01); F04D 27/00 (2006.01); F04D 29/056 (2006.01); F04D 29/063 (2006.01); F04D 29/52 (2006.01);
U.S. Cl.
CPC ...
F04D 29/083 (2013.01); F01D 25/183 (2013.01); F04D 27/009 (2013.01); F04D 29/056 (2013.01); F04D 29/063 (2013.01); F04D 29/522 (2013.01); F05D 2260/609 (2013.01);
Abstract

A seal assembly for a gas turbine engine employs a first seal forming an oil chamber around a bearing. The first seal is configured to maintain the oil chamber at a first pressure. A second seal forms a ventilating cavity around the oil chamber. The second seal is configured to maintain the ventilating cavity at a second pressure, the second pressure being less than the first pressure and less than an ambient pressure of a primary flow path in the engine. A pressure reducing device is coupled to the ventilating cavity. The pressure reducing device is configured to maintain the second pressure.


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