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:
Dec. 03, 2019

Filed:

Feb. 16, 2017
Applicants:

Airbus Operations Sas, Toulouse, FR;

Airbus Sas, Blagnac, FR;

Inventors:

Patrick Zaccaria, Grisolles, FR;

Pierre-Henri Brousse, Ramonville, FR;

Alexis Manneville, Toulouse, FR;

Paul-Emile Roux, Toulouse, FR;

Damien Lozach, Colomiers, FR;

Christine Molliet, Toulouse, FR;

Assignees:

AIRBUS OPERATIONS SAS, Toulouse, FR;

AIRBUS SAS, Blagnac, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 31/12 (2006.01); F02C 7/264 (2006.01); F02C 7/27 (2006.01);
U.S. Cl.
CPC ...
B64D 31/12 (2013.01); F02C 7/264 (2013.01); F02C 7/27 (2013.01); F05D 2220/323 (2013.01); F05D 2240/20 (2013.01); F05D 2260/85 (2013.01);
Abstract

A system and a method for the automatic starting of the engines of a twin-engine aircraft. When a first engine is made by the pilots of the aircraft to follow an automatic starting procedure, this engine follows the conventional four-phase starting cycle. The rotor of the high-pressure stage of the second engine is spun up for a predetermined duration and to a speed that is substantially constant and less than the nominal value during the starting cycle for the first engine. Once the starting cycle for the first engine is complete, the second engine is made by the pilots of the aircraft to follow an automatic starting procedure. The starting cycle for the second engine comprises just three phases.


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