Abstract: A method is provided for operating a gas turbine installation which has at least one compressor for compressing combustion air, at least one combustion chamber for combusting a supplied fuel, using the compressed combustion air, and also at least one turbine which is exposed to throughflow by the hot gases from the at least one combustion chamber. Both a first fuel on a carbon base, especially in the form of natural gas, and also a second fuel, in the form of a hydrogen-rich fuel or pure hydrogen, are used as fuel. A reduction of the CO2 emission without basic modifications to the installation is achieved by the first and the second fuels being intermixed and combusted together in the at least one combustion chamber.

Abstract: A combustion system is provided for an oxy-combustion furnace. The combustion system includes at least one windbox mountable on the oxy-combustion furnace and having at least one main firing location. At least one primary inlet is positioned in the at least one main firing location for conveying fuel and the first oxidant into the oxy-combustion furnace. At least one secondary inlet is positioned in the at least one main firing location for conveying the second oxidant into the oxy-combustion furnace. The at least one secondary inlet is angularly offset from the at least one primary inlet.

Abstract: The invention concerns a combustion method for industrial furnace comprising an arrangement of two substantially parallel and symmetrical burner assemblies (G, D). Each burner assembly comprises a fuel injector (10<SUB>G</SUB>, 10<SUB>D</SUB>) and three oxidant injectors (1<SUB>G</SUB>, 2<SUB>G</SUB>, 3<SUB>G</SUB>, 1<SUB>D</SUB>, 2<SUB>D</SUB>, 3<SUB>D</SUB>) arranged at increasing distances from the fuel injector. An oxidant supply system cyclically distributes a specific flow of oxidant among some at least of the second and third injectors of the burner assemblies (2<SUB>G</SUB>, 3<SUB>G</SUB>, 2<SUB>D</SUB>, 3<SUB>D</SUB>). The amount of nitrogen monoxide produced upon combustion is thus reduced, while ensuring a good distribution of the heating power in the furnace.

Abstract: Counterflow burner having a combustion chamber (5) to which combustible gas (B) and an oxidising agent (0) can be fed from opposite sides, having three planar substrates (1, 2, 3) which are interconnected, lying one above the other, the middle substrate (2) having the combustion chamber (5), from which passages (4), lying in the plane of the substrate, lead to the edge, the upper substrate (3) and the lower substrate (1) being closed, and at least the middle substrate (2) is produced using methods of microsystem technology.

Abstract: Described is an apparatus for incinerating waste gas comprising; a plurality of combustion nozzles 20 arranged in periphery of an inner tube for discharging the waste gas into the combustion chamber, an incineration inner tube 30 for shielding the flare smoke, the flame light and the noise being generated during incineration of the waste gas and being discharged from the combustion nozzle 20, said incineration inner tube 30 having a plurality of air inlets 32 at its lower periphery, and an outer tube 40 for introducing the swirl air into the flame generation side for providing the swirl force to the combusted gas which is elevated within the inner tube 30, said outer tube 40 is provided with several air inlet passages 42 tangentially formed in communication with the incineration inner tube 30.

Abstract: A burner system with staged fuel injection includes a burner with a swirl generator (1) for a combustion air stream and device(s) for introducing fuel into the combustion air stream, wherein the fuel introducing devices include at least two separate fuel supply elements (4a, 4b) with groups of fuel outlet openings for corresponding premix fuel amounts, wherein a first group is arranged downstream from a second group. The burner system furthermore includes measurement value probes (8, 9) for measuring the pulsations and emissions of the combustion, as well as a control device (10) that controls the two stages (4a, 4b) for introducing fuel dependent on the measured measuring values. The burner system permits optimized operation of the system even under changing operating and environmental conditions.

Abstract: An object of the present invention is to provide a combustion apparatus in which a space which does not contribute effectively to the combustion of fuel is less prone to be produced in a furnace because burners are not disposed at the corners of the furnace.The furnace having a square horizontal cross section is provided with the burners so that an in-furnace injection direction axis line of the burner is tangent to an imaginary circle. The burner is disposed at one place on a front wall, rear wall, right side wall, and left side wall of the furnace each, at a total of four places. The burner on each wall is installed so that the intersection of the in-furnace injection direction axis line of the burner and the furnace wall surface is apart from a furnace corner (corner point) by a length L1. The value of the length L1 is 15% of a length L of one side of width of the inside wall of the furnace when the furnace is viewed from the top.

Abstract: Fuel is fed by a feeding pump to a pressurized container. A predetermined amount of fuel is kept constant in the container by a floater which carries a needle for opening and closing a return as required. In the pressurized container the fuel is kept by a compressor under compressed air pressure which may be regulated by a pressure control valve, so that when the valve is opened fuel and air both under the same pressure are pressed into a nozzle unit in which air is highly pressed in the fuel so that when it leaves the nozzle channel it expands in an explosive manner and bursts the fuel into fine droplets. Secondary combustion air from an air generator is blown into the flame perpendicularly to the axis of the flame and fed to the fuel-air mixture.

Abstract: A burner has first and second nozzles communicated with a combustion chamber and defined in a wall structure surrounding the combustion chamber. The first and second nozzles are opposed to each other and positioned adjacent an exit opening of a fuel supply passage that is defined in the wall structure. The burner also has first and second secondary air supply ports defined in the wall structure adjacent the exit of the combustion chamber in opposition to each other.

Abstract: A burner includes a number of flame ports each having a fuel supply passage and provided on a pair of opposite walls of a combustion chamber such that each of the walls and the fuel supply passages define a cooling passage. In the burner, a wide stable flame region is achieved at a high excess air ratio, the amount of NOx produced is reduced and backfire is prevented by cooling the fuel supply passages. Furthermore, a flame area per unit area of each flame port is increased such that the burner can effect high-load combustion.

Abstract: A combustion chamber is subdivided vertically into layers with each layer having sets of burners disposed in angular spaced apart relation. In addition, the sets of burners are offset from one layer to another and all of the jet axes of the burners are directed in the same direction tangentially of a vertically disposed imaginary cylinder within the combustion chamber. The jets create a vortex flame within the combustion chamber.

Abstract: A method for reducing nitric oxide emissions from a gaseous fuel combustor includes introducing a combustion gas containing nitrogen and oxygen, such as air, into a combustion chamber and introducing a fuel gas into the same chamber. A cooling gas, such as steam, is interleaved between the combustion gas and the fuel gas substantially at the point where they are introduced into the chamber. The concentration of cooling gas in the flame front is maximized by this method, resulting in a lower temperature for the flame front and, correspondingly, lower production of nitric oxide emissions. Apparatus for carrying out the invention includes a combustion chamber, a body having a channel through which combustion gas can be introduced into the combustion chamber, a fuel gas nozzle for introducing fuel gas into the combustion chamber, and an orifice around the nozzle for interleaving cooling gas between the fuel gas and the combustion gas.

Abstract: The dual cannister gas housing of the present invention permits combustion of two separate gases of different heating values for industrial applications. The housing includes a first annular chamber surrounding a combustion zone, the first chamber receiving a first gas. Holes in the inner wall of the chamber permit entry of the first gas into the combustion zone. A second chamber surrounds the first chamber and receives a second gas. Tubes connect the second chamber to the combustion zone, the tubes passing through the first chamber to prevent mixing of gas. The number and size of the tubes and holes are selected for each application to insure proper entry velocity and pressure drop for the first and second gases.

Abstract: Apparatus for supplying air and fuel to a flame tube of a combustion chamber of a gas turbine engine which includes primary air supply ports for supplying air under high pressure toward the center of the flame tube and fuel tubes projecting into and opening at the primary supply ports for admitting fuel for entrainment by the primary air as it passes through the primary supply ports. In certain preferred embodiments, an annular member forms a supply port, as well as a mounting arrangement for fuel tube. Preferred embodiments also include deflector baffles or plates for preventing flow of fuel from the fuel tubes into portions of the air being supplied as secondary air to the combustion chamber.