Apparatus and method for selecting a flow mixture
AssigneeThe Boeing Company
InventorsKenneth M. Sprouse, Alan V. von Arx, David R. Matthews
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AssigneeThe Boeing Company
InventorsKenneth M. Sprouse, Alan V. von Arx, David R. Matthews
Estimating the term…
A counter-flow system for use in a turbine for selecting various mixtures of fluids for use with the system. The system may be used for a combustor for a gas powered turbine which employs a heat exchanger to combust a fuel without the emission of undesired chemical species. A gas powered turbine requires expanding gases to power the turbine blades. Fuel is combusted to produce the required gases. An oxidizer is introduced into the counter-flow system in a first direction before a first portion of fuel is introduced into the oxidizer. The fuel and oxidizer mixture is then flowed through a second pathway wherein the fuel and oxidizer mixture obtains a selected amount of thermal energy. Moreover, in a second pathway an equivalence ratio of the fuel and oxidizer mixture may be altered from the original fuel and oxidizer mixture.
A counter-flow combustor apparatus for use in a turbine for combusting a fuel in the presence of an oxidizer, the apparatus comprising:
A counter-flow combustor apparatus for use in a turbine for combusting a fuel in the presence of an oxidizer, the apparatus comprising:
A combustor for use in a gas powered turbine, the combustor comprising:
Dependencies are inferred from the claim text.