Internal structure of a primary exhaust duct having a separator of which the geometry varies depending on the temperature

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United States of America Patent

PATENT NO 11519302
APP PUB NO 20210262364A1
SERIAL NO

17181566

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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An internal structure of a primary exhaust duct of a turbomachine, which has a primary wall allowing air to pass through orifices and forming an internal surface of the primary exhaust duct, an interior skin arranged inside the primary wall, and at least one separator of which a first edge region is attached to the interior skin and which has two geometries. A change from the first geometry to the second takes place when the temperature of the separator exceeds a first temperature, and the change from the second to the first takes place when the temperature of the separator drops below a second temperature. The coefficient of expansion of the separator is greater than that of the interior skin. The variation in the geometry of the separators depending on the temperature of the engine eases assembly at ambient temperature due to the compression of the separators.

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Patent Owner(s)

Patent OwnerAddress
AIRBUS OPERATIONS SAS316 ROUTE DE BAYONNE TOULOUSE 31060

International Classification(s)

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  • 2021 Application Filing Year
  • F02K Class
  • 347 Applications Filed
  • 209 Patents Issued To-Date
  • 60.24 % Issued To-Date
Click to zoom InYear of Issuance% of Matters IssuedCumulative IssuancesYearly Issuances202120222023202420250255075100

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Andre, Sandrine Toulouse, FR 4 9
Ferreira, Julien Toulouse, FR 6 0
Kilkenny, Michael Toulouse, FR 3 2
Trocellier, Vincent Toulouse, FR 2 0

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Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges1999401 - 100102030405060708090100110120130140150160170180190200210

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