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. 03, 2020

Filed:

Mar. 20, 2015
Applicant:

Safran Helicopter Engines, Bordes, FR;

Inventors:

Fabien Lescher, Aressy, FR;

Jean Philippe Jacques Marin, Jurancon, FR;

Philippe Etchepare, Pau, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/56 (2006.01); F02K 3/12 (2006.01); F02C 3/10 (2006.01); F02C 9/46 (2006.01); B64D 31/06 (2006.01);
U.S. Cl.
CPC ...
F02C 9/56 (2013.01); B64D 31/06 (2013.01); F02C 3/10 (2013.01); F02C 9/46 (2013.01); F02K 3/12 (2013.01); F05D 2220/329 (2013.01); F05D 2270/091 (2013.01); F05D 2270/093 (2013.01); F05D 2270/095 (2013.01); F05D 2270/335 (2013.01); Y02T 50/671 (2013.01);
Abstract

The invention relates to a method for detecting a malfunction in a first turboshaft engine, referred to as an inoperative engine (), of a twin-engine helicopter, and for controlling a second turboshaft engine, referred to as a healthy engine (), each engine () comprising protective stops regulated by a regulation device which define a maximum power regime, characterised in that it comprises: a step () of detecting an indication of failure of said inoperative engine (); a step () of modifying said protective stops of said healthy engine () into protective stops which correspond to a maximum power single-engine regime, in the case of the detected indication of failure; a step () of confirming a failure of said inoperative engine (); a step () of controlling an increase in the flow rate of fuel supply of said healthy engine (), in the event of a confirmed failure.


Find Patent Forward Citations

Loading…