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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.

Patent No.:

US 10151214 B1

PDFFull Text
Date of Patent:
Dec. 11, 2018

Filed:

Jan. 23, 2015

Integral instrumentation in additively manufactured components of gas turbine engines

Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

William W. Rice, South Glastonbury, CT (US);

Michael Ian Walker, Glastonbury, CT (US);

Douglas H. Thomesen, Cromwell, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:

Kinney & Lange, P.A.

Primary Examiner:

Nguyen Q Ha

Int. Cl.
CPC ...
F01D 17/04 (2006.01); F01D 17/08 (2006.01); F02C 7/00 (2006.01); G01M 15/14 (2006.01); G01P 5/14 (2006.01); F01D 21/00 (2006.01); G01P 5/175 (2006.01); B22F 5/00 (2006.01); B22F 3/105 (2006.01); B22F 5/04 (2006.01); B33Y 10/00 (2015.01); B33Y 80/00 (2015.01);
U.S. Cl.
CPC ...
F01D 21/003 (2013.01); B22F 3/1055 (2013.01); B22F 5/009 (2013.01); B22F 5/04 (2013.01); B33Y 10/00 (2014.12); B33Y 80/00 (2014.12); F01D 17/08 (2013.01); F02C 7/00 (2013.01); G01M 15/14 (2013.01); G01P 5/14 (2013.01); G01P 5/175 (2013.01); F05D 2220/32 (2013.01); F05D 2230/22 (2013.01); F05D 2230/31 (2013.01); F05D 2250/292 (2013.01); F05D 2260/83 (2013.01); F05D 2300/10 (2013.01); Y02P 10/295 (2015.11); Y02T 50/672 (2013.01);
Abstract

A pressure probe includes a non-deflecting airfoil, a sensing feature, and an interior passage. The non-deflecting airfoil is made of a metal and configured for use in a gas turbine engine. The airfoil extends from a base to a tapered portion, and then to a linear portion, along a primary axis. The sensing feature is formed monolithically with the airfoil, as by additive manufacturing. The interior passage is operatively connected to the sensing feature and passes through both the airfoil and the base.

Find Patent Forward Citations

Quick Actions:

Rice, William. (2018). Integral instrumentation in additively manufactured components of gas turbine engines (U.S. Patent No. 10151214). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10151214

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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