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:
Aug. 02, 2016

Filed:

Aug. 23, 2011
Applicant:

Jean-michel Haillot, Beuste, FR;

Inventor:

Jean-Michel Haillot, Beuste, FR;

Assignee:

TURBOMECA, Bordes, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 1/00 (2006.01); F02C 6/08 (2006.01); B64D 41/00 (2006.01); F02C 3/13 (2006.01); F02C 7/32 (2006.01); B64D 13/06 (2006.01);
U.S. Cl.
CPC ...
F02C 6/08 (2013.01); B64D 41/00 (2013.01); F02C 3/13 (2013.01); F02C 7/32 (2013.01); B64D 2013/0611 (2013.01); F05D 2220/50 (2013.01); Y02T 50/53 (2013.01);
Abstract

A method for optimizing operability of an aircraft propulsive unit, and a self-contained power unit implementing the method. The method removes mechanical bleed constraints in engines during transient flight phases of an aircraft to optimize operability of the engine assembly during the phases. To this end, a supply of power is provided, particularly during the phases, by an additional indirectly propulsive engine power source. The method for optimizing operability of the propulsive unit of an aircraft including main engines as main drive sources includes, using a main engine power unit GPP as a power source, providing all the non-propulsive power and, during the transient engine phases, at most partially providing additional power to the body of the main engines.


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