Abstract:
Operation of unthrottled internal combustion engines is improved by providing the combustion chambers with an electrically heated glow plug having a catalyst surface layer on the ignition element. The catalyst is heated to and maintained at a temperature high enough to be effective for vaporization of fuel drops and ignition of vaporized fuel by controlled electrical heating. In operation of the engine air is compressed in a combustion chamber and at least a portion of the fuel is injected during the latter portion of the compression stroke and the injected fuel ignited by contact of fuel with the hot catalytic surface of the glow plug resulting in a combustion pressure wave in the immediate vicinity of top dead center.
Abstract:
Disclosed is a method of operating a catalytic ignition internal combustion engine wherein the fuel is injected into a combustion chamber at a time near maximum compression such that at least a part of the fuel impinges upon an oxidation catalyst surface comprising a portion of the wall of said combustion chamber, said catalytic surface being insulated from the surroundings external to the combustion chamber by a low thermal conductivity material, said catalytic surface preferably comprising platinum. Also disclosed are combustion chambers constructed specially for the use of this method and the methods of constructing them.
Abstract:
There is disclosed a method for conducting catalytic reactions, particularly hydrogenation or oxidation of vaporous, carbonaceous materials, utilizing a plurality of thin catalyst bodies in a spaced-apart relationship.
Abstract:
A system and process for forming a catalytic bed in which the active catalytic material is formed with an enhanced surface area and secure adhesion onto a support structure. The system is formed by a process in which a liquid solution of a salt which is decomposable into a refractory oxide is applied to a support structure. The solution is dried to remove the solvent and, following decomposition of said salt, an active catalytic material is impregnated by applying onto the surface a soluble compound comprised of a noble metal or a catalytic oxide-forming metal. The structure is calcined to activate the catalytic material.
Abstract:
Methanol is passed over a catalyst at an elevated temperature and pressure to produce a fuel gas containing a high proportion of methane in a one-step catalytic conversion process. Removal of water and carbon dioxide from the fuel gas produces a synthetic natural gas. For example, methanol with water is passed over a precious metal catalyst such as ruthenium on alumina at a temperature in the range of about 350.degree. C. to 500.degree. C. and a pressure in the range of about 800 to 2500 psig to produce a gaseous mixture comprising methane, carbon dioxide, minor amounts of hydrogen and essentially no carbon monoxide. Upon condensing the water vapor and scrubbing out the carbon dioxide, synthetic natural gas is obtained having a methane content above 90% by volume.
Abstract:
Synthetic natural gas and high octane motor fuel blending stock is produced by catalytically reforming naphtha at low severity to maximize production of aromatics and minimize hydrocracking, and then converting the remaining paraffins to methane in a methanation zone. The effluent from the methanation zone is separated into synthetic natural gas and motor fuel blending stock.
Abstract:
An internal combustion piston engine utilizing a catalyst to promote combustion and not requiring spark ignition. A catalyst member is provided within the engine cylinder. Air is supplied to the cylinder and is compressed by a piston. At or near the point of maximum compression, fuel is contacted with the catalyst, preferably from the side of the catalyst opposite the piston. The fuel and air mix to initiate combustion and the air-fuel mixture passes through the catalyst member, completing the combustion. The operation can result in relatively complete combustion of the fuel at a relatively low temperature of about 1800.degree. to 3300.degree. or 3500.degree. F. so that little or no undesirable components are present in the engine exhaust, especially the exhaust may have a low content of nitrogen oxides.
Abstract:
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.
Abstract:
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.
Abstract:
A method for operating a hydrogen-fueled gas turbine is provided wherein a supply of fuel is passed to a gas turbine combustor, and a supply of nitrogen and sufficient air to provide at least sufficient compressed air to the gas turbine for fuel combustion is passed to a compressor. A sufficient portion of the compressor discharge flow is passed to a combustor for fuel rich combustion of the fuel flow to the combustor and the fuel is combusted to produce hot combustion gases that are, in turn, passed to a turbine.