FUEL DELIVERY SYSTEM WITH A CAVITY COUPLED FUEL INJECTOR
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United States of America Patent
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Issued Date -
Jan 7, 2021
app pub date -
Apr 13, 2020
filing date -
Sep 6, 2012
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Abstract
A fuel injection system for a gas turbine engine includes a fuel delivery conduit, a nozzle block with a nozzle aperture, and a cavity block with a cavity. The nozzle aperture has a first cross sectional area, and injects fuel received from the fuel delivery conduit into the cavity. The cavity has a second cross sectional area that is greater than the first cross sectional area.
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