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US 12,680,505 B1Granted
Carbide torch igniter
AssigneeRtx Corporation
InventorWilliam Joseph Beeson
Life of this patent
Estimating the term…
Abstract
A start mechanism ignitor for a propulsion system combustor including a nozzle comprising a nozzle wall forming a nozzle interior; and a torch ignitor attached to the nozzle wall and fluidly coupled with the nozzle interior.
Claims18
A start mechanism ignitor for a propulsion system combustor comprising:
- a nozzle comprising a nozzle wall forming a nozzle interior;
- and
- a torch ignitor attached to the nozzle wall and fluidly coupled with the nozzle interior;
- a torch mixing zone fluidly coupled with a reaction source container upstream of the torch mixing zone;
- the torch mixing zone fluidly coupled with a torch outlet downstream of the torch mixing zone, the torch outlet fluidly coupled with the nozzle interior;
- wherein the torch ignitor comprises a chemical source material within the torch mixing zone and a reaction source material within the reaction source container, wherein the chemical source material is a calcium carbide and the reaction source material is water.
3 more elements
A gas turbine engine having a start mechanism ignitor comprising:
- a case supporting a combustion section having a combustor;
- a nozzle attached to a combustor casing, the nozzle fluidly coupled to a fuel injector upstream from the nozzle;
- a nozzle wall defining a nozzle interior;
- and
- a torch ignitor attached to the nozzle wall and fluidly coupled with the nozzle interior;
- wherein the torch ignitor comprises a torch mixing zone fluidly coupled with a reaction source container upstream of the torch mixing zone;
- the torch mixing zone fluidly coupled with a torch outlet downstream of the torch mixing zone, the torch outlet fluidly coupled with the nozzle interior;
- wherein the torch ignitor comprises a chemical source material within the torch mixing zone and a reaction source material within the reaction source container, wherein the chemical source material is a calcium carbide and the reaction source material is water.
5 more elements
A process of forming a gas turbine engine having a start mechanism ignitor comprising:
- forming a case supporting a combustion section having a combustor with a combustor casing;
- attaching a nozzle to the combustor casing;
- fluidly coupling the nozzle to a fuel injector upstream from the nozzle;
- forming a nozzle wall defining a nozzle interior;
- and
- attaching a torch ignitor to the nozzle wall;
- fluidly coupling the torch ignitor with the nozzle interior;
- fluidly coupling a torch mixing zone with a reaction source container upstream of the torch mixing zone;
- fluidly coupling the torch mixing zone with a torch outlet downstream of the torch mixing zone;
- fluidly coupling the torch outlet with the nozzle interior;
- locating a chemical source material within the torch mixing zone;
- and
- locating a reaction source material within the reaction source container, wherein the chemical source material is a calcium carbide and the reaction source material is water.
10 more elements
Dependencies are inferred from the claim text.