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:
Jan. 25, 2022
Filed:
Mar. 30, 2017
Applicant:
Safran Aircraft Engines, Paris, FR;
Inventors:
Arnaud Nicolas Negri, Yerres, FR;
Nils Edouard Romain Bordoni, Melun, FR;
Michel Gilbert Rolland Brault, Quincy sous Senart, FR;
Guillaume Patrice Kubiak, Saint Pierre du Perray, FR;
Nathalie Nowakowski, Cesson, FR;
Romain Guillaume Cuvillier, Cesson, FR;
Assignee:
SAFRAN AIRCRAFT ENGINES, Paris, FR;
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); F01D 21/02 (2006.01); F02C 3/04 (2006.01); F02C 9/46 (2006.01); F01D 21/06 (2006.01); F02K 3/075 (2006.01); F02C 3/13 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); F01D 21/02 (2013.01); F02C 3/04 (2013.01); F01D 21/06 (2013.01); F02C 3/13 (2013.01); F02C 9/46 (2013.01); F02K 3/075 (2013.01); F05D 2270/021 (2013.01); F05D 2270/042 (2013.01); F05D 2270/091 (2013.01);
Abstract
Aircraft turbine engine, including at least one first compressor, an annular combustion chamber and at least one first turbine, which define a first flow duct for a primary flow. Between the combustion chamber and the first turbine is a device for discharging at least part of the primary flow.