Prutech Ii

Alzeta Corporation

Other

Frederick E Moreno

Robert M Kendall

Narendra D Joshi

Creighton D Hartman

David Frederick Bartz

Michael J Duret

The disposal of troublesome substances, especially global-warming halogenated compounds is difficult enough, but is particularly difficult when associated with particulate-forming matter, such as silane and arsine commonly encountered in waste gas streams of the semiconductor industry. The combustive destruction of the troublesome substances in such a waste gas stream is simply and successfully achieved by injecting the stream admixed with fuel gas into a combustion zone surrounded by the radiant surface of a foraminous gas burner that is separately fed fuel gas and excess air sufficient to burn all the combustibles entering the combustion zone. A simple apparatus integrates the combustion zone with a quenching zone for the combustion product stream.

Apparatus for combustive destruction of troublesome substances

Combustive destruction of halogenated compounds

A gaseous fuel burner and method in which a high-firing rate (blue/non-surface radiant) zone is created between two lower firing rate (red/surface radiant) combustion zones. The method of the invention can be achieved by selective perforation of porous sintered fiber mat burner surfaces to achieve improved burner performance and relatively low NO.sub.x emissions.

Multiple firing rate zone burner and method

In a staged low NOx lean premix hot wall gas turbine combustor, the interior wall of the combustor is maintained at or near the flame temperature to provide stable operation over a wide range of heat release values. One or more stages of the staged combustor includes a Stirred Reactor region followed by a Plug Flow Reactor region. In one embodiment, a lean premixture of fuel and air is inducted tangentially into an annular intake manifold for inducting a cyclonic flow of the premixture into the combustion chamber. In another embodiment, the Stirred Reactor region is developed by colliding, preferably head-on, a plurality of jets of lean premixture within the combustion chamber.

Staged low NOx premix gas turbine combustor

A staged low NO.sub.x gas turbine combustor includes a refractory fibrous thermally insulatively lined primary combustion chamber, operating fuel-rich, and exhausting through a throat into a metallic secondary combustion chamber containing a fuel-lean secondary combustion zone in which combustion is completed. A radiation cooling zone is provided intermediate the throat and secondary combustion zone for cooling of the primary combustion products before quick quench in the secondary combustion zone. The fibrous lining of the primary combustion chamber is densified at its interior surface with a refractory such as zirconia or silicon carbide to inhibit flame erosion. The liner is wrapped with a supportive compliant blanket of fibrous refractory insulation. Air cooling of the metallic wall of the secondary chamber surrounding the radiation cooling zone is intensified relative to the remainder of the secondary combustion chamber.

Staged low NO.sub.x gas turbine combustor

In a staged lean premix low NOx gas turbine combustor, the inside of the combustor is lined with a low density refractory thermal insulator for maintaining the hot face of the lining at or near the flame temperature, i.e., within 200.degree. F. and preferably within 50.degree. F. The heat release value in the first stage is held at a maximum value consistent with low NOx emission while decreasing the heat release value in the second or third stage to achieve a wide range of turndown. The flame temperature in the respective stages are maintained between a low of 1700.degree. F. and a maximum of 2700.degree. F. The flow of compressed air into the combustor is maintained generally uniform over the entire operating range of 5 to 1 turndown.

Staged lean premix low nox hot wall gas turbine combustor with improved

In a low NO.sub.x stage combustor, the hot fuel rich combustion gases exit the primary combustion chamber through a constriction including a throat portion and pass into a secondary combustion chamber wherein burning is completed by injection of secondary air such as the exhaust from a turbine. Swirl is imparted to the primary gas stream in the primary combustion chamber so as to cause the primary gas stream to fill the entire primary combustion chamber and for increasing the residence time within the primary chamber for reducing fuel NO.sub.x emissions. Swirl suppression means are employed in the throat of the flow constrictor, between the primary and secondary combustion chambers, for suppressing swirl in the outermost regions of the primary gas stream so as to reduce turbulent mixing with the injected, secondary air thereby reducing the peak flame temperature in the secondary combustion chamber and for reducing thermal NO.sub.x emissions. The swirl suppression means comprises means for roughing the throat of the flow constrictor such as by forming lands and grooves in a castable, refractory material lining the interior wall of the throat.

Low NO.sub.x staged combustor with swirl suppression

A low NO.sub.x staged combustor for a TEOR steam generator includes a primary combustion chamber lined with an improved refractory lining. The refractory lining includes a first layer of low density ceramic fibrous thermal insulation as of 4' in thickness coated on its hot face with a protective coating of a durable tough material. The ceramic fibers of the insulative layer are oriented normal to the plane of the hot face. In one embodiment, a low density castable refractory thermally insulative layer is sandwiched between the shell of the combustion chamber and the first layer of fibrous insulation. In a second embodiment, a low density thermally insulative ceramic fibrous layer is sandwiched between the shell of the combustion chamber and the first layer of fibrous insulation. In the second embodiment, the ceramic fibrous layers are adhered to the shell by refractory hangers embedded in the fibrous insulation and resistance welded to the shell.

Primary stage combustor lining

In a low NO.sub.x power and steam generator for thermally enhanced oil recover, a gas turbine fired with nitrogen-bearing crude oil and air produces power and hot turbine exhaust. A portion of the turbine exhaust is fed into the primary combustion chamber of a two-stage combustor for supplying the combustion air for burning a high nitrogen-containing crude oil in the primary combustion zone under fuel-rich conditions. The combustion is completed in a secondary combustion zone supplied with air derived from a second portion of the turbine exhaust at about 1200.degree. F. A third portion of the turbine exhaust is fed into a convection stage disposed to receive the exhaust from the secondary combustion zone for capturing the heat from the turbine exhaust and from the exhaust of the secondary zone and converting it to steam. The output exhaust flow from the turbine is relatively constant with time, whereas the steam requirements for oil recovery decrease with time as production falls off and, thus, means are provided for bypassing an increasing percentage of the turbine exhaust around the two-stage combustor for heat recovery in the convection stage.

Turbine exhaust fed low NO.sub.x staged combustor for TEOR power and

In an extraction method and apparatus for extracting low biomass solid materials from a pneumatic transport line, the stream of gas having the solids entrained therein is caused to flow over a toothed extractor wheel. The toothed wheel picks out of the stream the solid materials which are then doffed from the tooth extractor wheel by the vanes of a rotating valve which seals the pressure of the pneumatic transport line from the ambient. The material doffed from the extractor wheel falls into the region between the vanes of the rotary valve and is then removed from the system as the vanes of the valve rotate. The air stream which is inducted into the extractor is first caused to pass through a diffuser which slows the velocity of the air stream and then the air stream is cause to flow along a curved duct section toward the extractor wheel causing the solid materials to flow to the outside of the curved duct section and into the extractor wheel to facilitate extraction.

Growing community of inventors

Los Altos, CA, United States of America

Frederick E Moreno