Torch igniters
AssigneeThe Secretary of State for Defence in Her Britannic Majesty's Government of the United Kingdom of Great Britain and Northern Ireland
InventorJohn R. Tilston
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AssigneeThe Secretary of State for Defence in Her Britannic Majesty's Government of the United Kingdom of Great Britain and Northern Ireland
InventorJohn R. Tilston
Estimating the term…
A torch igniter intended particularly for gas turbine engine applications comprises an integral assembly of a flame lighter and a fuel atomizer of the pre-filming air blast type. The fuel atomizer is configured so as to encircle the tip of the flame lighter and this atomizer comprises fuel and air inlets, a fuel/air passage defined between a body portion of the flame lighter and a sleeve this fuel air passage extending from the inlets to an exit mouth around the electrodes at the tip of the flame lighter, and an atomizer lip at the mouth of the fuel/air passage. A secondary passage can be included to aid in atomization of the fuel and in direction of the spray of atomized fuel this secondary passage having an exit annulus encircling the mouth of the fuel/air passage. A further passage can be included which is exposed to heat exchange with exterior air to pre-cool compressor delivery air before supply to the atomizer. This torch igniter is intended to be resistant to sprayer blockage and therefore suitable for use in a mode in which the fuel supply to the atomizer is cut off once the main burner is lighted.
A torch igniter for a gas turbine engine, said engine including a means for supplying compressor bleed air, said igniter comprising:
In a liquid fueled gas turbine engine, including at least one combustion chamber consisting of a flame casing, a pressure casing encompassing said flame casing in a spaced apart relationship therewith and defining therebetween an air passage, means for supplying compressor bleed air to said air passage, said pressure casing being situated in said engine such that at least a part of its surface abuts a bypass duct and is exposed to cool air in said bypass duct, an improved torch igniter comprising:
In a liquid fueled gas turbine engine, including at least one combustion chamber consisting of a flame casing, a pressure casing encompassing said flame casing in a spaced apart relationship therewith and defining therebetween an air passage, and a means for supplying compressor bleed air to said passage, said pressure casing being situated in said engine such that at least a part of its surface abuts a bypass duct and is exposed to cool air in said bypass duct, an improved torch igniter comprising:
Dependencies are inferred from the claim text.