Importance

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Abstract

A fuel mixture distribution system for a turbine engine assembly includes a combustor that includes a wall that defines a combustion chamber, a fuel mixture distributor that includes an air conduit that defines a mixing chamber that extends through the wall along between an inlet to an exit opening to the combustion chamber, the air conduit shape is defined to achieve the desired mixing and prevent flashback at all operating conditions, and a fuel distributor extends into the mixing chamber at a location upstream of the exit opening. The fuel distributor includes a plurality of fuel openings where a fuel flow is communicated and mixed with an airflow passing through the mixing chamber.

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First Claim