A burner for producing synthesis gas by partial oxidation of liquid or gaseous, carbon-containing fuels in the presence of an oxygen-containing oxidant and a moderator, which burner can be operated uncooled, i.e. without a fluid coolant being passed through the burner, is proposed. Steam or carbon dioxide or else mixtures of these materials are used as moderator. This is achieved by the feed channels being configured so that mixing of the fuel, the moderator and the oxidant occurs only outside the burner.

A flare pilot assembly has inner and outer tubes, defining inner and outer passages. A manifold delivers air and fuel to the outer passage. A bleed off passage directs a portion of the fuel and air entering the manifold to the exterior of the manifold. A diversion port in the inner tube diverts into the inner passage a portion of the air and fuel flowing through the outer passage. An electrical sparking device ignites air and fuel flowing through the inner passage. An evacuating tube extends from the manifold through the inner passage to the distal portion of the inner tube. The evacuating tube conveys moisture that may accumulate at the distal portion of the inner passage through the bleed off passage to the exterior.

Systems and methods for use with water-fuel supply to industrial engines are provided. A method for controlling water supplied to an engine may include using both a desired water-fuel ratio, and a compensated fuel flow. This compensated fuel flow may be calculated by a controller-implemented complementary filter, which may include receiving, by the controller, a first signal and a second signal. The complementary filter may subtract the second signal from the first signal to create an error signal, lag the error signal to create a lagged error signal, and add the lagged error signal to the second signal to create a compensated signal. The controller may calculate a water flow request using a desired water-fuel ratio and the compensated signal.

The present disclosure describes a system and method for shaping and energizing fluids that can generate luminous fluid sculptures. The method comprises sculpting the pattern and/or shape of a plurality of fluids using nonvisible forces such as mechanically generated turbulence, controlled movement through a shaped chamber, magnetic fields, vibration, gravity, or other forces; energizing the sculpted fluids so that they emit visible light using sources of nonvisible energy such as chemicals, heat, electrical currents, electromagnetic radiation, or other sources; and controlling the color of the emitted light using chemical additives, selected wavelengths of electromagnetic radiation, layering of selected chemicals, or other methods.

An oxygen generator with an oxygen-producing having a center bore, including: an impact-activated ignition mechanism, an end cover, a cylinder, a bell-shaped hood, a thermally insulating inner cylinder, an oxygen-producing column, a thermally insulating material, a support bowl, a gas purification material, a safety valve, an isolation net, an oxygen-discharging end cover and an oxygen-discharging joint. The cylinder is provided with the end cover at one end; the impact-activated ignition mechanism is fixed on the end cover; the oxygen-producing column is coaxially located with the cylinder, one end of the oxygen-producing column is connected to the impact-activated ignition mechanism, and the other end of the oxygen-producing column is connected to the support bowl; the support bowl is connected to the isolation net; the thermally insulating inner cylinder is arranged on the outside of the oxygen-producing column and the thermally insulating material.

A well test burner system includes a plurality of burner nozzles, each including an air valve and a well product valve movable between an open position, where air and a well product are allowed to circulate through the burner nozzle to discharge an air/well product mixture, and a closed position, where the air and the well product are prevented from circulating through the burner nozzle. One or more actuation devices are operatively coupled to the air valve and the well product valve to move the air valve and the well product valve between the open and closed positions.

Systems and methods for hydroxyl driven combustion include introducing a first gas via at least a first orifice into a processing chamber having a substrate disposed on a substrate support. A second gas is introduced into the processing chamber via a plurality of second orifices. The plurality of first orifices and the plurality of second orifices are oriented in an alternating pattern such that each second orifice of the plurality of second orifices is at least partially surrounded by at least a first orifice of the plurality of first orifices. A radical is produced as a function of the first gas and the second gas while heating the chamber.

A rich-lean burner has on an upper end portion thereof: a lean flame port longitudinally extended to eject a lean fuel-air mixture which is leaner in fuel concentration than a theoretical fuel-air ratio; a blind clearance located on each lateral side of the lean flame port, the blind clearance being free from ejection of a fuel-air mixture; and a rich flame port located on lateral outside of each of the blind clearances to eject a rich fuel-air mixture which is richer in fuel concentration than the theoretical fuel-air ratio. The rich-lean burner further has a lean-flame deforming device to deform a lean flame formed by combustion of the lean fuel-air mixture ejected from the lean flame port such that the shape of one lateral side of the lean flame becomes asymmetrical with the shape of laterally opposite side of the lean flame.

A semi-submersible gas burner assembly for a fire-on-water feature, the assembly including a tubular void former having nominal waterline disposed between proximal and distal ends and a separable lid engaging the distal end. The lid includes inner and outer peripheral skirts projecting toward and past the waterline, respectively. At least one gas manifold arm extends through and outward from the tubular void former, and includes a gas port disposed proximate the sidewall. The sidewall at the distal end includes a communicating aperture which fluidly interconnects the interior of the tubular void former with a flame retention chamber defined by the sidewall, the lid, the inner peripheral skirt of the lid, and the nominal waterline.

An inertial electrode launcher may be configured to project charged particles or a voltage comprising an inertial electrode proximate a flame or combustion gas produced by the flame.