Pratt & Whitney Rocketdyne, Inc.

The Boeing Company

Rockwell International Corporation

General Electric Company

United Technologies Corporation

Gas Technology Institute

Aerojet Rocketdyne of De, Inc.

Kenneth Michael Sprouse

David R Matthews

Shahram Farhangi

Albert E Stewart

Robert M Saxelby

John Saunders Stevenson

Alan V Von Arx

Constantin Bugescu

Robert J Jensen

Chandrashekhar Sonwane

Robert Michael Zirin

Raymond Douglas Steele

Mark David Horn

Steven P Fusselman

Bryan William McEnerney

Stephen Yows

Roger Ma

John D Winter

Jeffrey A Mays

Michael P Moriarty

Gregory A Johnson

Ganesan Subbaraman

James R Lobitz

James A Hartung

Stephen Arthur Yows

Merlin D Schuman

L Paul Combs

George M O'Connor

Terry Langowski

Allan Von Arx

Luis A Rosales

Adon Delgado, Jr

James D Navratil

Bryan William Mcenerney

An injector mixer for a gasification reactor system that utilizes reactants includes an injector body that extends between a first face and a second face. The injector body includes a first passage that extends between the first face and the second face and has a first central axis. At least one second, impinging passage extends between the first face and second face and has an associated second central axis that has an angle with the first axis. The angle satisfies mixing efficiency Equation (I) disclosed herein.

Injector mixer for a compact gasification reactor system

A tight-shale oil production tool includes a combustor operable to generate an aqueous-phase nitric acid, combustion products.

Tight-shale oil production tool

A pump system includes a particulate consolidator pump that has a pump outlet. A duct is coupled to the pump outlet. The duct has a wall that is coupled with an oscillator. The oscillator is operable to oscillate the wall at a controlled frequency. The controlled frequency is selected with respect to breaking static bridging of particulate in the duct due, at least in part, to consolidation of the particulate from a downstream check valve.

Duct having oscillatory side wall

A slag agglomerator includes an inlet, an outlet and a plurality of obstacles. The inlet receives a flow of gas and slag droplets and the outlet allows the flow of gas and slag droplets to exit the agglomerator. The obstacles are oblique or perpendicular to the flow of gas and slag droplets and have an exterior surface containing a ceramic matrix composite.

Agglomerator with ceramic matrix composite obstacles

A biomass torrefaction system includes a mill which receives a raw biomass feedstock and operates at temperatures above 400 F (204 C) to generate a dusty flue gas which contains a milled biomass product.

Biomass torrefaction mill

A method of assembling an injection device for use in a reactor injector feed assembly includes extending the injection device at least partially into a cavity. The injection device includes a plurality of substantially concentric conduits coupled to a modular tip that includes a plurality of cooling channels and a plurality of substantially annular nozzles defined therein. The method also includes coupling at least one coolant distribution device in flow communication with the plurality of cooling channels to facilitate removing heat from an outer surface of the injection device.

Apparatus for removing heat from injection devices and method of assembling same

An annular injector is described. The injector includes a first bayonet assembly and a second bayonet assembly each including a terminal end and a tip end. The second bayonet assembly is configured to be concentrically coupled at least partially about the first bayonet assembly. An outer diameter of the first bayonet assembly and an inner diameter of the second bayonet assembly vary at the tip end to define a first substantially annular nozzle. The first bayonet assembly includes a maximum outer diameter that is greater than a minimum inner diameter of the second bayonet assembly and at least a portion of at least one of the first bayonet assembly and the second bayonet assembly extends from the tip end to the terminal end. The injector includes a third bayonet assembly configured to be concentrically coupled at least partially about the second bayonet assembly to define a second substantially annular nozzle.

Annular injector assembly and methods of assembling same

A flow splitter is operable to divide flow of a fuel mixture. The flow splitter includes a first tube having an outlet end and a plurality of second tubes that are coupled at the outlet end to divide flow from the first tube. Each of the plurality of second tubes has a respective inside diameter that satisfies Equation (I) and Equation (II) disclosed herein.

Flow splitter for a compact gasification reactor system

A pump system includes a pump that includes a first belt and a second belt that are spaced apart from each other to provide generally straight sides of a passage there between. There is an inlet at one end of the passage and an outlet at an opposite end of the passage, with a passage length that extends between the inlet and the outlet. The passage defines a gap distance in a width direction between the straight sides at the passage inlet. A hopper includes an interior space that terminates at a mouth at the passage inlet. At least one screw is located within the interior space of the hopper and includes a screw diameter in the width direction that is less than or equal to the gap distance.

Screw-fed pump system

A power plant includes a closed loop, supercritical carbon dioxide system (CLS-COsystem). The CLS-COsystem includes a turbine-generator and a high temperature recuperator (HTR) that is arranged to receive expanded carbon dioxide from the turbine-generator. The HTR includes a plurality of heat exchangers that define respective heat exchange areas. At least two of the heat exchangers have different heat exchange areas.

Recuperative supercritical carbon dioxide cycle

A method of assembling a gasification reactor includes extending an injection device at least partially into the gasification reactor. The injection device includes a plurality of substantially concentric conduits coupled to a modular tip and at least one outer surface. The modular tip includes a plurality of cooling channels and a plurality of substantially annular nozzles defined therein. The method further includes forming at least one layer of insulation about at least a portion of the at least one outer surface to facilitate insulating at least a portion of the injection device from heat within the gasification reactor.

Method and apparatus for assembling injection devices

A method of assembling an injection device for use in a reactor injector feed assembly includes coupling a plurality of substantially concentric conduits to a modular tip. The method also includes coupling a first conduit of the reactor injector feed assembly to a modular tip and coupling a second conduit of the reactor injector feed assembly to the modular tip. The modular tip includes a first substantially annular nozzle and a second substantially annular nozzle defined therein. The first conduit and the first substantially annular nozzle are centered about an injection device centerline.

Modular tip injection devices and method of assembling same

A method of producing a synthetic gas (syngas) includes injecting a plurality of reactant streams into a gasification reactor via at least one injection device having a plurality of injection annuli, an inner portion that extends annularly about a centerline extending through the at least one injection device, and an outer portion extending substantially annularly about the inner portion. At least a portion of the outer portion is oriented obliquely with respect to the at least one injection device centerline. The method also includes mixing at least a portion of each of the streams together such that a plurality of recirculation zones is defined by the streams. The method further includes producing a syngas within the recirculation zones via mixing at least a portion of each of the streams. The injection device includes an inner portion that extends annularly about a centerline extending through the injection device. The device also includes an outer portion extending substantially annularly about the inner portion that includes at least one of at least one carbonaceous reactant injection port oriented obliquely with respect to the injection device centerline and at least one outer face oriented obliquely with respect to the injection device centerline.

Method and apparatus to produce synthetic gas

A reactor vessel liner system includes a liner having an inner wall, an outer wall, and a plurality of passages extending between the inner wall and the outer wall. An attachment member extends outwards from the outer wall for securing the liner.

Reactor vessel and liner

Annular injector assembly and methods of assembling the same

Growing community of inventors

Northridge, CA, United States of America

Kenneth Michael Sprouse