Abstract:
A low emissions combustor for use in gas turbines which operate at turbine inlet temperatures below about 1250 degrees Kelvin, which comprises;a multiplicity of microlith catalyst elements; andmeans for providing an admixture of fuel and air having an adiabatic flame temperature within the range of 600 to 1250 degrees Kelvin.
Abstract:
Disclosed is a method of operating a catalytic ignition internal combustion engine wherein the fuel is injected into a combustion chamber at a time near maximum compression such that at least part of the fuel impinges upon an oxidation catalyst surface comprising a portion of the wall of said combustion chamber, said catalytic surface being insulated from the surroundings external to the combustion chamber by a low thermal conductivity material, said catalytic surface preferably comprising platinum. Also disclosed are combustion chambers constructed specially for the use of this method and the methods of constructing them.
Abstract:
A method and system are provided for starting a combustion system utilizing a catalyst, and at the same time provide low emissions of unburned hydrocarbons and carbon monoxide. The method is particularly applicable to starting such combustion systems which are subject to intermittent operation, such as for example, gas turbines used to power automotive vehicles in which carbonaceous fuels are combusted to provide the motive fluid, or furnaces which are used intermittently. In the method, heat, such as produced by electrical means or by thermal combustion of a carbonaceous fuel, is employed to bring the catalyst to an operating temperature which will permit rapid oxidation of the carbonaceous fuel. When the catalyst has been heated to reach such operating temperatures, the start-up heating may be terminated and the normal operation of the combustion zone including the catalyst may proceed.
Abstract:
The present invention provides a combustor for an aerospace gas turbine engine comprising two stages wherein each stage defines an inlet and an exit. The second stage inlet is in fluid communication with the first stage exit such that a first flowpath is defined and it passes substantially through the second stage. A plurality of flow channel tubes is positioned within the second stage and each flow channel tube passes sealingly through a header plate positioned upstream of the second stage inlet thereby defining a second flowpath that also passes substantially through the second stage. The first flowpath exit and the second flowpath exit are positioned adjacent and proximate to one another to provide for the generation of microflames or microflame jets exiting the second stage from between and around the flow channel tube exits. The first stage of the combustor provides a gasifier and a reformer. The present invention also may comprise an igniter for further combustion of the reacted products or an external heat source for start-up. The second stage also may comprise a microflame combustor.
Abstract:
A method is provided for operating a lean-burn homogeneous charge reciprocating internal combustion engine that includes providing an unthrottled fuel-air compression charge having a lean fuel-air ratio, passing the fuel-air compression charge to fill no more than sixty percent of a cylinder within the internal combustion engine, compressing the fuel-air compression charge within the cylinder, igniting the compressed fuel-air compression charge for combustion, and passing exhaust resulting from the combustion to a NOx removal system. A non-platinum oxidation catalyst may be used to control carbon monoxide emissions in the exhaust Engine power may be varied by controlling the engine speed with a continuously variable transmission, by varying the applied engine load to charge a hybrid system battery, or by varying the amount of the lean fuel-air mixture charged.
Abstract:
A method is provided for achieving low NOx operation of homogeneous charge, lean burn reciprocating internal combustion engines. The method incorporates providing a fuel-air compression charge having a lean fuel-air ratio of less than the lean flammable limit, compressing the fuel-air compression charge to raise the adiabatic flame temperature to a predetermined value above the lean flammable limit, and igniting the compressed charge for combustion. A non-platinum oxidation catalyst may be included to control carbon monoxide emissions in the exhaust.
Abstract:
A method for the partial oxidation of hydrocarbons is provided wherein an endothermic catalyst and an oxidation catalyst are positioned upon a short channel-length metallic substrate; the endothermic catalyst positioned under a surface layer of the oxidation catalyst positioned on the metallic substrate. A fuel-rich supply of hydrocarbons and oxygen is then passed over the substrate. The method includes providing an oxidation catalyst on at least a portion of a surface of the metallic substrate wherein a hydrocarbon is oxidized by an oxygen mass-transfer-limited reaction on the oxidation catalyst surface; and providing an endothermic catalyst on the metallic substrate below the oxidation catalyst surface whereby an endothermic reaction follows the oxygen mass-transfer-limited reaction below the oxidation catalyst surface.
Abstract:
A method for generating a heated product stream downhole is provided wherein a fuel rich mixture is reacted downhole by contact with a catalyst to produce a partially reacted product stream, the fuel rich mixture comprising fuel and oxygen. The partially reacted product stream is brought into contact with an oxidant thereby igniting combustion upon contact producing a combustion product stream. The combustion product stream may be cooled by injecting a diluent flow such as water or CO2. The cooled combustion product stream may be into an oil bearing strata in order to reduce the energy requirements for the production of heavy oil.
Abstract:
A method is provided for controlling the operating temperature of a catalytic reactor using a closed-loop system that provides for varying the reactor input and other operating parameters in order to maintain the operating temperature of the reactor at or near the initial setpoint temperature for operation of the reactor. In one example, maximum and minimum operating temperatures with a catalytic partial oxidation reactor are controlled, as well as maintaining control over the corresponding minimum required ratio of oxygen atoms to carbon atoms, such that the operating temperature within the reactor is maintained below the material limits but above threshold temperatures for coking.
Abstract:
A method of producing natural gas fuel from gas hydrate beds is provided wherein natural gas is oxidized in a fuel cell producing electricity and heat. At least a portion of the heat is transferred to water and the heated water is passed downhole and brought into thermal contact with a hydrate bed. The hydrate is disassociated thereby producing hydrate gas. A sufficient amount of fuel is then passed to the fuel cell for operation of the fuel cell.