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:
Aug. 23, 2016

Filed:

May. 11, 2011
Applicants:

Guillaume Bodard, Verneuil l'Etang, FR;

Alexandre Alfred Gaston Vuillemin, Fontainebleau, FR;

Inventors:

Guillaume Bodard, Verneuil l'Etang, FR;

Alexandre Alfred Gaston Vuillemin, Fontainebleau, FR;

Assignee:

SNECMA, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/34 (2006.01); F02K 1/46 (2006.01);
U.S. Cl.
CPC ...
F02K 1/34 (2013.01); F02K 1/46 (2013.01); F05D 2240/40 (2013.01); F05D 2250/11 (2013.01); F05D 2250/13 (2013.01); F05D 2260/96 (2013.01);
Abstract

A gas exhaust nozzle for aircraft propulsion includes at least a downstream part with a trailing edge of chevron type formed of chevrons distributed along the periphery of the nozzle. Each chevron extends downstream between an upstream transverse plane and a downstream transverse plane with free edges oriented in two converging downstream directions and defining the trailing edge. The chevrons generate vortices at the boundary of the jet emitted by the nozzle. The gas exhaust nozzle includes a device to inject auxiliary gas jets upstream of the free edges of the chevrons in the main jet through orifices placed upstream of the upstream plane in such a way as to discharge upstream of the upstream plane of the chevrons to generate the vortices upstream of the free edges of the chevrons.


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