Abstract: The conventional gas turbine combustor is improved by mounting a pilot flame producing torch in a wall of the combustor to project a flame into the combustor as a means of ignition. The torch preferably is a catalytic igniter which will operate over a wide range of air/fuel ratios.

Abstract: The conventional gas turbine combustor is improved by mounting a pilot flame producing torch in a wall of the combustor to project a flame into the combustor as a means of ignition. The torch preferably is a catalytic igniter which will operate over a wide range of air/fuel ratios.

Abstract: The conventional gas turbine combustor is improved by mounting a pilot flame producing torch in a wall of the combustor to project a flame into the combustor as a means of ignition. The torch preferably is a catalytic igniter which will operate over a wide range of air/fuel ratios.

Abstract: Gas phase combustion producing lower emissions in gas turbines is stabilized in a lean pre-mixed combustor, by flow of the fuel/air mixture through a catalyst which is heated by contact with recirculated, partially reacted combustion gases.

Abstract: An assembly for the catalytic ignition of atomized fuel for combustion within the combustion chamber of a turbine engine places the catalytic fuel igniter in a position to receive the atomized fuel upon entry into the combustion chamber. The igniter is heated to operating temperature so that at least a portion of the atomized fuel enters the combustion chamber in an ignited state.

Abstract: Honeycomb structure assemblies comprising walled structures which admit fluid such as air for purposes of cooling or heating the walls thereof or for other purposes. The assemblies comprise spaced inner and outer walls united by means of an internal honeycomb structure comprising aligned cells having opposed interior and exterior gaps open to adjacent cells, which causes the admitted fluid to undulate through said gaps into contact with both of the walls, such as for uniform cooling or heating. The honeycomb structure contains flanges which are secured to one or both walls for uniform strength and resistance to separation under the stress of use.