Turbine engine combustion assembly with a variable air supply

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United States of America Patent

PATENT NO 10054056
APP PUB NO 20150247459A1
SERIAL NO

14432855

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Abstract

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A turbine engine combustion assembly including a casing, a combustion chamber, and at least one fuel injector. The combustion chamber includes an internal wall and an external wall extending one inside the other and connected by an annular chamber base wall. The external wall of the chamber is secured to an annular external wall of the casing. The injector is attached to the annular external wall of the casing and includes a fuel ignition enclosure extending inside the casing successively through openings in the casing wall and in the external wall before opening into the chamber. At least one wall of the ignition enclosure extending between the casing wall and the combustion chamber wall includes at least one air intake port. The external wall of the combustion chamber is solidly connected to a device for plugging the air intake port according to a thermal expansion state of the combustion chamber.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN HELICOPTER ENGINES64510 BORDES

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  • 2013 Application Filing Year
  • F02C Class
  • 960 Applications Filed
  • 829 Patents Issued To-Date
  • 86.36 % Issued To-Date
Click to zoom InYear of Issuance% of Matters IssuedCumulative IssuancesYearly Issuances201320142015201620172018201920202021202220230255075100

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Carrere, Bernard Joseph Jean Pierre Pau, FR 4 8

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  • F02C Class
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Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges762501012101 - 1011 - 2021 - 3031 - 4051 - 60020406080100120140160180200220240260280

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