PREMIXER INJECTOR IN GAS TURBINE ENGINE
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United States of America Patent
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Issued Date -
Mar 14, 2024
app pub date -
Feb 23, 2021
filing date -
Feb 23, 2021
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Abstract
A premixer injector in a gas turbine engine includes an inlet end, an outlet end, a first wall and a second wall between the inlet end and the outlet end. The first wall has a plurality of apertures circumferentially separated around the first wall and axially separated along the first wall. Each aperture passes through the first wall. A premixer duct is defined by an interior of the first wall. The second wall at least partially surrounds the first wall. A secondary duct is defined between the first wall and the second wall.
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