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. 11, 2020

Filed:

Apr. 01, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Tewfik Boudebiza, Paris, FR;

Gilles Alain Charier, La Grande Paroisse, FR;

Augustin Marc Michel Curlier, Boissise la Bertrand, FR;

Jean-Christophe Duffet, Saint-Mande, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/06 (2006.01); F02C 3/067 (2006.01); F02K 3/062 (2006.01); F02C 7/18 (2006.01); F01D 25/24 (2006.01); F02C 3/10 (2006.01); F02K 3/072 (2006.01);
U.S. Cl.
CPC ...
F02C 7/18 (2013.01); F01D 25/24 (2013.01); F02C 3/067 (2013.01); F02C 3/10 (2013.01); F02K 3/072 (2013.01); F05D 2220/32 (2013.01); F05D 2260/20 (2013.01);
Abstract

A non-faired propeller turbo-engine includes a gas generator and a propulsion unit that is separated from the gas generator by an intermediate housing. The turbo-engine includes a housing and a radially internal ferrule that are coaxial and are connected by hollow radial arms. The housing of the turbo-engine also defines, in part, a gas flow duct of a secondary gas flow. Each radial arm is hollow and is traversed by at least one service of the turbo-engine. Additionally, at least one arm is traversed by a ventilation gas circulation duct from the secondary gas flow and which leads to at least one component from among a power turbine and a mechanical transmission of said propulsion unit.


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