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:
Jul. 25, 2023

Filed:

May. 09, 2018
Applicant:

Ratier-figeac Sas, Figeac, FR;

Inventors:

Brian P. Huth, West Hartford, CT (US);

Abdellah El Haloui, Figeac, FR;

Assignee:

RATIER-FIGEAC SAS, Figeac, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 45/00 (2006.01); G01M 5/00 (2006.01); G01L 1/22 (2006.01); G01M 1/28 (2006.01);
U.S. Cl.
CPC ...
B64D 45/00 (2013.01); G01L 1/2262 (2013.01); G01M 5/0016 (2013.01); G01M 5/0025 (2013.01); G01M 5/0033 (2013.01); G01M 5/0041 (2013.01); G01M 5/0083 (2013.01); B64D 2045/0085 (2013.01); G01M 1/28 (2013.01);
Abstract

A method of monitoring the health of an aircraft propeller whilst the propeller is in operation, the propeller having a plurality of blades extending radially outwardly from hub arms of a propeller hub, which in turn extend radially outwardly from a central axis extending through the propeller and a propeller drive shaft, is provided. The method comprises obtaining measurements representative of the strain in each of at least some of the hub arms using strain sensors, each of the strain sensors being provided on a respective hub arm. A corresponding propeller health monitoring system, an aircraft propeller comprising the system and an aircraft comprising the propeller are also provided.


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