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US 2020/0080530 A1Published application
Igniter for gas turbine engine
AssigneePratt & Whitney Canada Corp.
InventorsRichard Freer, Kian McCaldon, Tin-Cheung John Hu, Michel Bousquet, André Fortin
Life of this patent
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Abstract
There is disclosed an igniter for a gas turbine engine including: a base; a glow plug heater rod extending from the base along an axis and terminating in a rod end; and a fuel receiver adjacent the heater rod, the fuel receiver including a portion located closest to the heater rod, the rod end protruding axially relative to the axis from the fuel receiver portion located closest to the heater rod.
Claims20
An igniter for a gas turbine engine comprising:
- a base;
- a glow plug heater rod extending from the base along an axis and terminating in a rod end;
- and a fuel receiver adjacent the heater rod, the fuel receiver including a portion located closest to the heater rod, the rod end protruding axially relative to the axis from the fuel receiver portion located closest to the heater rod.
Dependencies are inferred from the claim text.