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. 08, 2022

Filed:

Jun. 06, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Almeric Pierre Louis Garnier, Moissy Cramayel, FR;

Tony Alain Roger Joel Lhommeau, Moissy Cramayel, FR;

Lorris Michel Cognot, Moissy Cramayel, FR;

Thierry Raymond Poix, Moissy Cramayel, FR;

Alexandre Jean Joseph Salvi, Moissy Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 21/00 (2006.01); G01B 7/30 (2006.01); G01B 11/26 (2006.01); F01D 21/04 (2006.01); F01D 17/04 (2006.01); F01D 17/02 (2006.01); F01D 17/06 (2006.01); F04D 27/00 (2006.01);
U.S. Cl.
CPC ...
F01D 21/003 (2013.01); F01D 17/02 (2013.01); F01D 17/04 (2013.01); F01D 17/06 (2013.01); F01D 21/04 (2013.01); F04D 27/001 (2013.01); F04D 27/008 (2013.01); G01B 7/30 (2013.01); G01B 11/26 (2013.01); F05D 2220/30 (2013.01); F05D 2260/80 (2013.01); F05D 2260/83 (2013.01);
Abstract

A method of detecting the angular positions of blades of a rotor wheel of a turbine engine, in which the turbine engine has first and second rotor wheels including respective first and second numbers of blades regularly distributed around their circumferences, includes: detecting the passage of each blade of the first wheel past a first sensor; detecting the passage of each blade of the second wheel past a second sensor; calculating the time intervals between the passage of a blade of the first wheel and the passages of each of the blades of the second wheel; and determining the relative angular position of each blade of the first wheel relative to the angular positions of the blades of the second wheel, the first number and the second number being distinct and mutually prime.


Find Patent Forward Citations

Garnier, Almeric Pierre Louis. (2022). Method and a system for detecting the angular position of blades of a turbine engine rotor wheel (U.S. Patent No. 11268400). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/11268400

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

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