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. 11, 2019

Filed:

Sep. 16, 2015
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

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

Stephen W. Milks, Sanford, ME (US);

Steven J. Feigleson, Falmouth, ME (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/20 (2006.01); F02C 7/06 (2006.01); F02C 3/04 (2006.01); F01D 25/24 (2006.01); F01D 25/28 (2006.01);
U.S. Cl.
CPC ...
F02C 7/06 (2013.01); F01D 25/246 (2013.01); F02C 3/04 (2013.01); F02C 7/20 (2013.01); F01D 25/28 (2013.01); F05D 2220/32 (2013.01); F05D 2240/50 (2013.01); F05D 2260/30 (2013.01); F05D 2260/36 (2013.01); F05D 2300/50212 (2013.01);
Abstract

Conduits for guiding the motion of an inner diameter shroud of a low pressure compressor of a gas turbine engine are disclosed. The inner diameter shroud has at least three slots formed in one or more radially inwardly extending flanges. Each of the conduits are configured to assemble with a respective one of the at least three slots. Each conduit comprises a bushing having a first panel, and the first panel is capable of being inserted in a respective one of the slots of the inner diameter shroud. The conduit further comprises a bracket capable of being attached to a bearing support of a fan intermediate case of the gas turbine engine. The bushing is capable of being attached to the bracket. A contact between the first panel and the at least one slot of the inner diameter shroud restricts a circumferential rotation of the inner diameter shroud with respect to a central axis of the gas turbine engine when the first panel is inserted in the at least one slot, but allows a radial motion of the inner diameter shroud with respect to the central axis.


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