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US 8,534,041 B2Granted
Apparatus and assembly for a spark igniter having tangential embedded pins
AssigneeUnison Industries, LLC
InventorsBrendon Francis Mee, Randal Parker Bold
Life of this patent
Estimating the term…
Abstract
An apparatus and assembly for an igniter is provided. The igniter includes a shell comprising a base, a tip surface, and a sidewall extending therebetween wherein the sidewall surrounds a cavity within the shell. The igniter also includes a shell bore extending from the tip surface to the cavity and a pin embedded into the tip surface extending substantially tangentially with respect to the bore.
Claims18
An igniter comprising:
- a shell comprising a tip surface, and a sidewall extending away from said tip surface, said sidewall surrounding a cavity within the shell;
- a shell bore extending from said tip surface to said cavity;
- an electrode positioned within said shell, said electrode comprising a distal firing end positioned proximate said shell bore;
- and
- at least three pins having a first end embedded within said shell at a location between said tip surface and said distal firing end and extending parallel to a line that is substantially tangentially aligned with respect to said bore, wherein said at least three pins extend from the first end along the line such that a second end terminates embedded within said shell.
2 more elements
An igniter assembly comprising:
- a substantially cylindrical shell comprising a tip surface, and a sidewall extending away from said tip surface, said sidewall surrounding a cavity within the shell, said shell having a longitudinal axis extending parallel to said sidewall and orthogonally with respect to said tip surface;
- a shell bore extending from said tip surface to said cavity, said shell bore concentric with the longitudinal axis;
- an electrode positioned within said shell, said electrode comprising a distal firing end positioned proximate said shell bore;
- and
- at least three erosion-resistant pins having a first end embedded within said substantially cylindrical shell at a location between said tip surface and said distal firing end and extending parallel to a line in a substantially tangential orientation with respect to said bore, wherein said at least three erosion-resistant pins extend from the first end along the line such that a second end terminates embedded within said shell.
2 more elements
A gas turbine engine comprising:
- a combustor comprising a sidewall enclosing a combustion chamber;
- and
- an igniter assembly extending at least partially through said sidewall such that a tip of said igniter assembly is in flow communication with said combustion chamber, said igniter assembly comprising:
- a shell surrounding a cavity;
- a shell bore extending from said tip to said cavity;
- and
- at least three erosion-resistant pins having a first end embedded within said shell at a location between said cavity and said tip and extending parallel to a line in a substantially tangential orientation with respect to said bore, wherein said at least three erosion-resistant pins extend from the first end along the line such that a second end terminates embedded within said shell.
4 more elements
Dependencies are inferred from the claim text.