Nozzle arrangement for a gas turbine engine

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United States of America Patent

PATENT NO 9239029
APP PUB NO 20090031730A1
SERIAL NO

12183921

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Abstract

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A nozzle arrangement for a gas turbine engine includes an engine nozzle and an ejector nozzle arranged axially downstream thereof. A gap S is formed between the outlet of the engine nozzle and the inlet of the ejector nozzle, and a flange which reduces the gap S is arranged at the outlet of the engine nozzle.

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Patent Owner(s)

Patent OwnerAddress
AIRBUS DEFENCE AND SPACE GMBHWILLY-MESSERSCHMITT-STRASSE 1 TAUFKIRCHEN 82024

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Herrmann, Otfrid Bruckmuehl, DE 3 54

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