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:
Jan. 23, 2018

Filed:

Aug. 27, 2013
Applicant:

Turbomeca, Bordes, FR;

Inventors:

Pierre Harriet, Billere, FR;

Jean Philippe Jacques Marin, Jurancon, FR;

Assignee:

TURBOMECA, Bordes, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/268 (2006.01); F02C 7/264 (2006.01); F01D 19/00 (2006.01); F02C 7/275 (2006.01);
U.S. Cl.
CPC ...
F02C 7/268 (2013.01); F01D 19/00 (2013.01); F02C 7/264 (2013.01); F02C 7/275 (2013.01); F05D 2260/85 (2013.01); F05D 2270/04 (2013.01); F05D 2270/304 (2013.01); F05D 2270/309 (2013.01);
Abstract

The invention relates to a method for starting an aircraft turboshaft engine, said turboshaft engine comprising a combustion chamber, a compressor shaft on which a compressor wheel is mounted to feed compressed air to said combustion chamber, at least one starter connected to said shaft so as to provide it with a specified starting torque for driving it in rotation. The method comprises accelerating the compressor shaft during a first start-up phase, then stabilizing the rotational speed of the compressor shaft during a second start-up phase. During acceleration of the compressor shaft, the rotational speed of the shaft is regulated such that the acceleration of the shaft remains substantially constant.


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