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.
Patent No.:
Date of Patent:
Jul. 07, 2020
Filed:
Jan. 29, 2015
Applicants:
Safran Aircraft Engines, Paris, FR;
Safran, Paris, FR;
Safran Power Units, Toulouse, FR;
Inventors:
Nicolas Claude Parmentier, Moissy Cramayel, FR;
Pierre Froment, Moissy Cramayel, FR;
Jean-François Rideau, Tournefeuille, FR;
Bruno Thoraval, Moissy Cramayel, FR;
Assignees:
Primary Examiner:
Int. Cl.
CPC ...
B64D 13/06 (2006.01); F02C 6/20 (2006.01); B64D 13/00 (2006.01); B64D 13/02 (2006.01); B64D 13/08 (2006.01); B64D 27/10 (2006.01); F04D 29/32 (2006.01); F04D 29/52 (2006.01); F04D 29/56 (2006.01); F04D 29/58 (2006.01); F02C 7/27 (2006.01); F02C 9/18 (2006.01);
U.S. Cl.
CPC ...
B64D 13/06 (2013.01); B64D 13/00 (2013.01); B64D 13/02 (2013.01); B64D 13/08 (2013.01); B64D 27/10 (2013.01); F02C 6/206 (2013.01); F02C 7/27 (2013.01); F02C 9/18 (2013.01); F04D 29/321 (2013.01); F04D 29/522 (2013.01); F04D 29/563 (2013.01); F04D 29/5833 (2013.01); B64D 2013/0618 (2013.01); B64D 2013/0696 (2013.01); F05B 2220/303 (2013.01); F05B 2260/20 (2013.01); F05D 2220/323 (2013.01); F05D 2220/324 (2013.01); F05D 2220/325 (2013.01); F05D 2240/60 (2013.01); F05D 2260/4031 (2013.01); Y02T 50/56 (2013.01); Y02T 50/671 (2013.01); Y02T 50/675 (2013.01);
Abstract
An aircraft turboprop engine includes at least a low-pressure body and a high-pressure body. The low-pressure body drives a propeller by means of a gearbox. The turboprop engine also includes means for supplying air to an air-conditioning circuit of an aircraft cabin, wherein the supply means has at least one compressor borne by the gearbox and of which the rotor is coupled to the low-pressure body by means of the gearbox.