Precision Combustion, Inc.

General Energy Recovery, Inc.

Benjamin D Baird

Richard Mastanduno

Bruce Crowder

Sandeep Alavandi

Subir Roychoudhury

Chester Ledlie Sandberg

Curtis Morgan

Brian Kay

J Kevin Burns

William C Pfefferle

Shahrokh Etemad

Jeffrey G Weissman

Codruta Maria Zoican-Loebick

Paul Fazzino

Richard T Maastanduno

Kevin J Burns

A process of removing at least one metal contaminant, such as copper, from a fluid hydrocarbon, for example, crude oil or a liquid hydrocarbon fuel, such as an aviation fuel. The process involves contacting the metal-contaminated fluid hydrocarbon with a sorbent selected from graphene oxide or a functionalized graphene oxide. The process removes greater than 99 percent of the metal contaminant without reducing concentrations of advantageous additives, such as, antioxidants, icing inhibitors and corrosion inhibitors. Also disclosed are a purified fluid hydrocarbon composition and a metal contaminant filter system.

Process of removing a metal from a fluid hydrocarbon

A system and method of producing oil is provided. The system includes a support module that provides air, water and fuel to a well. A steam generator is fluidly coupled to the support module to receive the air, water and fuel. The steam generator includes an injector having a plurality of tubes. The tubes have an outer surface with an oxidation catalyst thereon. The steam generator is configured to divide the supplied air and direct a first portion through the tubes. A second portion of the supplied air is mixed with supplied fuel and directed over the outside of the tubes. The air and fuel is burned in a combustor and water is sprayed on the combustion gases to produce steam. The steam and combustion gases are directed in the direction of the oil reservoir.

System and method of producing oil

A flameless cooking apparatus for use with liquid fuels and for indoor or outdoor use under field operations. The burner exhibits low CO and hydrocarbon emissions and meets standards for burner thermal efficiency when used with JP-8 fuel. The apparatus employs a catalytic burner having among its parts (i) a combustion catalyst; (ii) a conductive surface, e.g., cooking surface; and (iii) in between the catalyst and the conductive surface and in direct physical contact with both surfaces, a heat spreader for conductively transferring heat of combustion from the catalyst to the conductive surface. Also claimed are a method of heat flux and a method of cooking.

Flameless cooking appliance

A system and method of producing steam is provided. The system includes a support module and a steam module. The support module is configured to supply air, water and fuel. The steam module includes a casing defining a hollow interior that is fluidly coupled to receive water from the support module. An interface module is provided having a first conduit made from flexible tubing that is fluidly coupled to receive fuel from the support module. The interface module further having a second conduit being made from flexible tubing that is fluidly coupled to receive air from the support module. A combustor is coupled to and spaced apart from the interface portion, the combustor being fluidly coupled to receive fuel from the first conduit and air from the second conduit. A steam generator is coupled to an end of the combustor.

A method for low NOx combustion, without premixing of fuel and air prior to passage to a combustor, is provided wherein a fuel is injected into a reaction zone via an eductor thereby inducing an air flow and producing a fuel-rich mixture. The fuel-rich mixture is reacted and produces partial reaction products plus heat. A portion of the heat is to transferred to a cooling air stream and the cooled partial reaction products are brought into contact with the heated cooling air stream for combustion. Increased injection of the fuel results in an increased induction of the air flow.

Direct injection method and apparatus for low NOx combustion of high hydrogen fuels

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.

Two stage combustor with reformer

The invention provides an apparatus for generating heat and transferring the heat to a heater head of an external combustion engine, preferably, a Stirling engine. Fuel and air are introduced into a combustion chamber and mixed to form an air/fuel mixture. The air/fuel mixture is combusted over a combustion catalyst positioned in physical contact with a heat spreader, which itself is positioned in physical contact with a heat acceptor surface. The heat acceptor surface is secured in thermal communication with the heater head. Depending upon the design of the heater head, heat flux from the heat acceptor surface into the heater head may occur radially or non-radially.

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Rocky Hill, CT, United States of America

Benjamin D Baird