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:
Feb. 13, 2018

Filed:

Dec. 19, 2014
Applicant:

Airbus Helicopters, Marignane, FR;

Inventors:

Guido Borchers, Marseilles, FR;

Romain Stephant, Aix en Provence, FR;

Assignee:

AIRBUS HELICOPTERS, Marignane, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 6/02 (2006.01); F02C 7/32 (2006.01); F02C 7/36 (2006.01); B64C 27/12 (2006.01); F02C 9/42 (2006.01); B64D 31/06 (2006.01);
U.S. Cl.
CPC ...
F02C 6/02 (2013.01); B64C 27/12 (2013.01); B64D 31/06 (2013.01); F02C 7/32 (2013.01); F02C 7/36 (2013.01); F02C 9/42 (2013.01); F05D 2220/329 (2013.01); F05D 2260/80 (2013.01); Y02T 50/671 (2013.01);
Abstract

A method of managing a power plant for a rotary wing aircraft, said power plant comprising two main engines, a secondary engine, and a main power transmission gearbox (MGB). Said main and secondary engines mechanically driving said MGB so as to rotate a main rotor of said aircraft. Said secondary engine delivers two distinct mechanical power levels so that said main and secondary engines together deliver sufficient mechanical power to enable said aircraft to fly, firstly a first secondary mechanical power MPand secondly a second secondary mechanical power MPsuitable for compensating for a loss of main mechanical power from at least one main engine.


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