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. 02, 2020

Filed:

Jan. 26, 2018
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Colin G Amadon, Kennebunk, ME (US);

Thomas Freeman, Kennebunk, ME (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/24 (2006.01); F01D 9/04 (2006.01);
U.S. Cl.
CPC ...
F01D 25/24 (2013.01); F01D 9/04 (2013.01); F05D 2220/323 (2013.01); F05D 2230/60 (2013.01); F05D 2240/14 (2013.01); F05D 2250/36 (2013.01); F05D 2260/30 (2013.01); F05D 2300/431 (2013.01); F05D 2300/50211 (2013.01); F05D 2300/603 (2013.01); F05D 2300/6012 (2013.01);
Abstract

A gas turbine engine includes an annular structure disposed around an engine central longitudinal axis of the gas turbine engine. The annular structure defines an annular channel and comprises a first density, according to various embodiments. The gas turbine engine may further include a weight-saving filler disposed within the annular channel. The weight-saving filler may have a second density that is less than the first density. The gas turbine engine may further include an annular retention strap disposed around the engine central longitudinal axis of the gas turbine engine. The annular retention strap is at least partially embedded in the weight-saving filler, according to various embodiments.


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