Abstract: An internal combustion engine having an annular port and valve arranged to direct flow from dual inner and outer portions of the port in cylinder flow patterns having radially oppositely directed flow components. Various embodiments providing cylinder charge stratification or dual inlet and exhaust valve functions are disclosed.

Abstract: A low emission combustor assembly particularly suited for an automotive gas turbine engine has an inlet plenum supplied with regenerated compressor discharge, an exhaust plenum, a diffusion flame combustion chamber disposed between the inlet and exhaust plenums, and a catalytic combustion chamber also disposed between the inlet and exhaust plenums so that parallel flow paths are established between the inlet and exhaust plenums. During engine start-up, fuel is supplied only to the diffusion flame combustion chamber and regenerated compressor discharge simultaneously flowing through the catalytic combustion chamber heats the catalyst to operating temperature and cools and dilutes exhaust from the diffusion flame combustion chamber.

Abstract: A dry coal fuel supply system for a gas turbine engine includes a continuous loop conveyor pump having a plurality of positive displacement pistons connected by a cable and driven by a variable speed motor with respect to an atmospheric reservoir filled with powdered coal and the continuous loop includes a dual stage coal pick-up for assuring coal fill of the conveyor system to accurately meter coal therefrom in accordance with the speed of the variable drive motor for driving the conveyor and wherein the system includes an improved sealed discharge manifold means for directing a controlled amount of the compressor discharge air of the gas turbine engine to a plurality of air jets for blasting high pressure air across the coal pump pistons to direct a fluidized powdered coal mixture into a downstream, closely associated fuel nozzle system for a gas turbine engine combustor.

Abstract: An improved coal/air dispersion nozzle introduces fuel into the combustion chamber of a gas turbine engine as a finely atomized, dispersed spray for a uniform combustion. The nozzle has an inlet that receives finely powdered coal from a coal transport or coal/air fluidizer system and a scroll swirl generator is included within the nozzle to swirl a fluidized coal/air mixture supplied to the inlet of the nozzle. The scroll is in the form of a thin, flat metal sheet insert, twisted along its length, and configured to prevent build-up of coal particles within the nozzle prior to ejection from its outlet. Airblast air jets are included along the length of the nozzle body to assist in the discharge of the fluidized coal from the nozzle outlet and an angular pintle tip overlies the outlet to redirect coal/air mixture through a desired fluidized coal spray angle.