Snecma

Centre National De La Recherche Scientifique

Safran Aircraft Engines

Université De Poitiers

Ensma

Maxime Koenig

Jacky Novi Mardjono

Marc Versaevel

Alexandre Alfred Gaston Vuillemin

Philippe Gerard Chanez

Peter Jordan

Yves Gervais

Guillaume Bodard

Henri Yesilcimen

Norman Jodet

Franck Zaganelli

Jeremy Paul Gonzalez

Pierre Comte

Cyprien Georges Eric Henry

Pierre (decede) Comte

Jacky Mardjono

Jérémy Gonzalez

Alexandre Alfred Vuillemin

Jeremy Gonzalez

A device for reducing the jet noise of a turbine engine includes an outer cover having an inside wall defining the outside of an annular passage for passing a bypass stream from the engine, the wall of the outer cover including a plurality of microjet circuits, each including intakes for taking a gas stream from the bypass stream flow passage and leading to a single feed duct, which in turn opens out into the trailing edge of the outer cover via at least one ejection grating suitable for splitting the intake gas stream into a plurality of gas streams of right sections of dimensions less than a right section of the feed duct.

Device with gratings for ejecting microjets in order to reduce the jet noise of a turbine engine

The invention relates to a rear casing for a turbine engine comprising a primary body generating a primary flow () to be ejected through a primary nozzle (), said rear casing () being shaped so as to be positioned downstream from the primary body and to define, on the inside of the turbine engine, the path followed by the primary flow downstream from the primary nozzle (). The tail cone is characterised in that it comprises a connection to a system for supplying a pressurised gas and at least one perforation () for injecting the pressurised gas through the perforation and into the primary flow. The casing preferably comprises at least one means for rotating same about the axis of rotation of the mobile elements of the primary body.

Tail cone for a microjet rotary turbine engine

A mixer for a confluent-flow nozzle of a turbine engine is provided. The mixer includes: an annular cap designed to be centered on a longitudinal axis of the nozzle and having a stationary upstream portion and a downstream portion that is movable in rotation about the longitudinal axis relative to the stationary portion, the movable portion of the cap terminating at its downstream end in inner lobes alternating circumferentially with outer lobes; and a mechanism which imparts reciprocating rotary motion to the movable portion of the cap.

Mixer that performs reciprocating rotary motion for a confluent-flow nozzle of a turbine engine, and a method of controlling it

Growing community of inventors

Moissy-Cramayel, France

Maxime Koenig