Combustor fuel injection system
AssigneeSundstrand Corporation
InventorsJack R. Shekleton, Michael W. Sledd, Steven S. Sachrison
Life of this patent
Estimating the term…
Loading patent…
AssigneeSundstrand Corporation
InventorsJack R. Shekleton, Michael W. Sledd, Steven S. Sachrison
Estimating the term…
In order to achieve ignition at altitude, particularly in relatively small combustors (10) with low fuel flow rates, a fuel injection system (20) includes an air nozzle (26), a fuel nozzle (28), and an air assist tube (34). The fuel nozzle (28) is disposed in a manner so as to direct fuel through the air nozzle (26) and includes a fuel metering orifice (30) or capillary tube (32) to control fuel flow therethrough. The air assist tube (34) is integrally associated with the fuel nozzle (28) downstream of the fuel metering orifice (30) or capillary tube (32) to accelerate fuel flowing through the fuel nozzle (28). With this arrangement, the air nozzle (26) may comprise an opening in a combustor wall (14) defining a combustion chamber (12) of a turbine engine combustor (10) wherein a combustor case (16) surrounds the combustor wall (14) to define an air flow path 18 in communication with a compressed air source whereby compressed air flows through the opening (26) and into the combustor (10) along with fuel from the fuel nozzle (28) and air from the air assist tube (34).
In a combustor for a turbine engine, said combustor having a combustion chamber defined by a combustor wall surrounded by a combustor case defining an air flow path therebetween, said air flow path being in communication with a source of compressed air, said combustor having a fuel injection system comprising a fuel manifold in communication with a plurality of fuel injectors associated with said combustor wall, the improvement comprising:
Dependencies are inferred from the claim text.