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. 03, 2017

Filed:

Feb. 11, 2015
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Steven Tine, Middletown, CT (US);

Richard A. Lomenzo, Jr., Enfield, CT (US);

Kevin J. Klinefelter, Uncasville, CT (US);

Elizabeth F. Vinson, Wethersfield, CT (US);

Kaitlin Olsen, Manchester, CT (US);

Thomas R. Davis, Cheshire, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01H 13/00 (2006.01); G01H 9/00 (2006.01); F01D 21/00 (2006.01);
U.S. Cl.
CPC ...
F01D 21/003 (2013.01); G01H 9/00 (2013.01); G01H 13/00 (2013.01); F05D 2240/12 (2013.01); F05D 2240/30 (2013.01); F05D 2260/12 (2013.01);
Abstract

A resonant frequency testing system for airfoils comprises a broach block, a clamp, an acoustic speaker, a laser vibrometer, and a control processor assembly. The broach block has a slot disposed to receive the airfoil in an airfoil location. The clamp has a torque-actuated shutoff, and is disposed to lock the airfoil in the broach block slot under a fixed clamping force. The acoustic sensor is disposed adjacent the airfoil location to emit sonic pulses, and the laser vibrometer is oriented towards the airfoil location to sense vibration signatures of the airfoil when excited by the sonic pulses. The control processor assembly is configured to control the acoustic speaker and laser vibrometer, to decompose the sensed vibration signatures into resonant frequencies of the airfoil, and to store the resonant frequencies in a digital storage database, correlated with a unique ID corresponding to the airfoil.


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