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:
Apr. 14, 2020

Filed:

May. 31, 2016
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventors:

Fanping Sun, Glastonbury, CT (US);

Zaffir A. Chaudhry, Glastonbury, CT (US);

Avinash Sarlashkar, Jr., Pittsford, NY (US);

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01L 1/16 (2006.01); G01M 5/00 (2006.01); G01H 11/08 (2006.01); H01L 41/113 (2006.01);
U.S. Cl.
CPC ...
G01L 1/162 (2013.01); G01H 11/08 (2013.01); G01M 5/0033 (2013.01); G01M 5/0083 (2013.01); H01L 41/1132 (2013.01);
Abstract

A piezoelectric sensor assembly for measuring a force quantity on a structure includes at least one piezoelectric sensor, each including an element and two electrodes each projecting outward from the element. An electronic processor of the assembly is configured to receive data from the sensor, wherein the data includes a voltage with a magnitude that is indicative of a dynamic load (i.e., amplitude modulation mode) placed upon the structure. The processor may be configured to interrogate the piezoelectric sensor for its resonant frequency change which is indicative of the load applied to the structure at low operation frequency and to which the piezoelectric sensor would not otherwise respond well. The dual mode operation of the piezoelectric sensor extends the frequency range of the strain measurement from the dynamic range to static or quasi-static range.


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