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. 20, 2020

Filed:

Mar. 26, 2018
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Weston Behling, Norwalk, CT (US);

Andrew C. Carmack, West Hartford, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/08 (2006.01); F02C 9/18 (2006.01); F01D 25/14 (2006.01); F01D 25/24 (2006.01); F02C 7/18 (2006.01); F02C 6/08 (2006.01); F01D 11/24 (2006.01); F01D 5/06 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); F01D 5/081 (2013.01); F01D 5/082 (2013.01); F01D 5/084 (2013.01); F01D 5/088 (2013.01); F01D 11/24 (2013.01); F01D 25/14 (2013.01); F01D 25/24 (2013.01); F02C 6/08 (2013.01); F02C 7/18 (2013.01); F01D 5/06 (2013.01); F01D 5/066 (2013.01); F05D 2220/3216 (2013.01); F05D 2230/642 (2013.01); F05D 2260/30 (2013.01); F05D 2260/606 (2013.01); F05D 2260/941 (2013.01); F05D 2300/171 (2013.01); F05D 2300/1723 (2013.01); F05D 2300/50212 (2013.01);
Abstract

A compressor section or a turbine section of a gas turbine engine having an axis includes a drum. The compressor section or the turbine section also includes a plurality of bores extending radially inward from the drum including a first bore and a second bore. The compressor section or the turbine section also includes a first bore basket at least partially defining a first cavity such that the first bore has at least one surface located in the first cavity. The compressor section or the turbine section also includes a second bore basket at least partially defining a second cavity that is isolated from the first cavity such that the second bore has at least one surface located in the second cavity.


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