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COMBUSTION CHAMBERS FOR GAS TURBINE ENGINES

  • US 3,593,518 A
  • Filed: 09/17/1969
  • Issued: 07/20/1971
  • Est. Priority Date: 09/20/1968
  • Status: Expired due to Term
First Claim
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1. A combustion chamber which includes a primary air inlet duct, secondary air inlet nozzles and dilution air inlet nozzles, each air entry point incorporating a fluidic airflow control device arranged so that the proportions of the total airflow through the respective air entry points can be varied without variation of the total resistance of the combustion chamber to airflow therethrough.

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