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:
Mar. 24, 2020

Filed:

Oct. 20, 2017
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

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

Alfred F. Covino, Simsbury, CT (US);

Richard C. Hendricks, Tolland, CT (US);

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

Bryan J. Hackett, Newington, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 21/00 (2006.01); F02C 7/04 (2006.01); G01M 15/14 (2006.01); F01D 17/08 (2006.01); F02C 7/32 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F01D 21/003 (2013.01); F01D 17/08 (2013.01); F02C 7/04 (2013.01); F02C 7/32 (2013.01); G01M 15/14 (2013.01); F02C 3/04 (2013.01); F05D 2220/32 (2013.01); F05D 2240/121 (2013.01); F05D 2240/55 (2013.01); F05D 2260/30 (2013.01); F05D 2260/83 (2013.01);
Abstract

A performance measurement system of an inlet of a gas turbine engine includes a probe strut configured for installation to a case strut of an inlet case of a gas turbine engine. The probe strut includes one or more probes extending therefrom configured to measure one or more characteristics of an airflow past the one or more probes, a first attachment point configured to secure the probe strut to a hub portion of the inlet case, and a second attachment point configured to secure the probe strut to an outer case portion of the inlet case. A data acquisition module is located at a central longitudinal axis of the inlet and is operably connected to the probe to collect sensed data therefrom. The probe strut and the data acquisition module are configured to be installed, removed, and/or relocated without removal of the inlet case from the gas turbine engine.


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