Cooling apparatus for combustor transition piece
AssigneeGeneral Electric Company
InventorsRonald James Chila, David Purnell
Life of this patent
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AssigneeGeneral Electric Company
InventorsRonald James Chila, David Purnell
Estimating the term…
Disclosed is an apparatus for cooling a transition piece of a combustor includes at least one wrapper disposed at the transition piece located outboard of the transition piece. At least one support boss is located between the at least one wrapper and the transition piece. The at least one support boss, the at least one wrapper, and transition piece define at least one cooling flow channel for directing flow for cooling the transition piece. A method of cooling a transition piece of a combustor includes flowing cooling flow into at least one cooling flow channel located at the transition piece, the at least one cooling flow channel defined by the transition piece, at least one wrapper located at the transition piece and located outboard of the transition piece, and at least one support boss located between the at least one wrapper and the transition piece. The cooling flow is directed via the at least one support boss and flows across an outer surface of the transition piece thereby cooling the transition piece.
An apparatus for cooling a transition piece of a combustor comprising:
A gas turbine comprising:
A method of cooling a transition piece of a combustor comprising:
Dependencies are inferred from the claim text.