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US 2016/0102861 A1Published application
Gas turbine engine combustor liner panel
AssigneeUnited Technologies Corporation
InventorsFrank J. Cunha, Stanislav Kostka, JR.
Life of this patent
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Abstract
A liner panel for a combustor of a gas turbine engine includes a multiple of heat transfer augmentors which extend from a cold side thereof. At least one of the multiple of heat transfer augmentors includes a first heat transfer augmentation feature with a second heat transfer augmentation feature stacked thereon.
Claims18
A liner panel for a combustor of a gas turbine engine, the liner panel comprising:
- a first heat transfer augmentation feature with a second heat transfer augmentation feature stacked thereon.
A combustor of a gas turbine engine, the combustor comprising:
- a shell;
- and
- a liner panel mounted to said shell, said liner panel includes a multiple of heat transfer augmentors which extend from a cold side thereof to extend toward said shell, at least one of said multiple of heat transfer augmentors includes a first heat transfer augmentation feature with a second heat transfer augmentation feature stacked thereon.
Dependencies are inferred from the claim text.