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:
May. 14, 2019

Filed:

May. 04, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Josselin Coupard, Moissy-Cramayel, FR;

Ronan Louis Castrec, Moissy-Cramayel, FR;

Rafik Zouari, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01M 1/22 (2006.01); G07C 5/00 (2006.01); B64D 45/00 (2006.01); G01H 1/00 (2006.01); G01H 3/14 (2006.01); G01M 1/14 (2006.01); G01M 15/12 (2006.01); G01M 15/14 (2006.01); G01M 1/28 (2006.01); G07C 5/08 (2006.01); G05B 23/02 (2006.01);
U.S. Cl.
CPC ...
G01M 1/22 (2013.01); B64D 45/00 (2013.01); G01H 1/003 (2013.01); G01H 3/14 (2013.01); G01M 1/14 (2013.01); G01M 1/28 (2013.01); G01M 15/12 (2013.01); G01M 15/14 (2013.01); G05B 23/0283 (2013.01); G07C 5/004 (2013.01); G07C 5/008 (2013.01); G07C 5/085 (2013.01); G07C 5/0808 (2013.01); B64D 2045/0085 (2013.01);
Abstract

A method for monitoring an aircraft engine during flight, which includes the steps of: for at least one characteristic frequency of the operation of the engine, measuring at least one synchronous vibration level value; for at least one module of the engine, estimating an out-of-balance value of the module in accordance with the one or more vibration level values measured and at least one sensitivity coefficient; estimating a balancing margin of the module in accordance with the out-of-balance value of said module and a maximum threshold; (d) estimating a remaining number of flights of the aircraft prior to balancing and/or a quality indicator of a preceding balancing operation in accordance with the one or more estimated balancing margins and data representing past balancing operations of the engine.


Find Patent Forward Citations

Coupard, Josselin. (2019). Method for monitoring an aircraft engine in operation during a flight (U.S. Patent No. 10288518). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10288518

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

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