COMBUSTOR FOR A GAS TURBINE ENGINE
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United States of America Patent
Stats
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N/A
Issued Date -
Jul 25, 2024
app pub date -
Feb 23, 2024
filing date -
Jun 7, 2021
priority date (Note) -
Published
status (Latency Note)
Importance
Abstract
A combustor for a gas turbine engine, the gas turbine engine defining a longitudinal centerline extending in a longitudinal direction, a radial direction extending orthogonally outward from the longitudinal centerline, and a circumferential direction extending concentrically around the longitudinal centerline, the combustor including: a forward liner segment; an aft liner segment disposed downstream from the forward liner segment relative to a direction of flow through the combustor, the forward and aft liner segments at least partially defining a combustion chamber; and an intermediate member disposed at least partially between the forward and aft liner segments and extending in the circumferential direction.
First Claim
Other Claims data not available