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US 2014/0338336 A1Published application
Gas turbine engine combustor with integrated combustor vane
AssigneeUnited Technologies Corporation
InventorsFrank J. Cunha, Nurhak Erbas-Sen
Life of this patent
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Abstract
A combustor section for a gas turbine engine includes a combustor vane which extends at least partially into a combustion chamber.
Claims21
A combustor section for a gas turbine engine comprising:
- a combustion chamber;
- and
- a combustor vane which extends at least partially into said combustion chamber.
A swirler for a combustion vane in a combustor section of a gas turbine engine comprising:
- an annular inner jet compartment which defines a convergent-divergent section;
- and
- a multiple of supply air chambers in communication with said annular inner jet compartment.
A combustor section for a gas turbine engine comprising:
- a combustor section having a combustor vane having at least one dilution hole.
Dependencies are inferred from the claim text.