DUAL-FLOW TURBINE ENGINE FOR AIRCRAFT WITH LOW NOISE EMISSION

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20110047960A1
SERIAL NO

12990733

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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The invention relates to a dual-flow turbine engine for an aircraft with low noise emission, wherein the opening (6) for the cold flow (9) of the turbine engine is provided with short, narrow, and spaced chevrons (15) that penetrate deeply, like claws, into said cold flow (9).

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Patent Owner(s)

Patent OwnerAddress
AIRBUS OPERATIONS (SAS)31060 TOULOUSE

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
André, Amadou Toulouse, FR 1 1
Debatin, Klaus Bonrepos Sur Aussonnelle, FR 2 3
Huber, Jérôme Toulouse, FR 2 3
Pelagatti, Olivier Toulouse, FR 5 29

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