MICROCIRCUIT COOLING FOR GAS TURBINE ENGINE COMBUSTOR
First Claim
Patent Images
1. A combustor component of a gas turbine engine comprising:
- a heat shield panel with a refractory metal core (RMC) microcircuit.
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Abstract
A combustor component of a gas turbine engine includes a refractory metal core (RMC) microcircuit.
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Citations
20 Claims
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1. A combustor component of a gas turbine engine comprising:
a heat shield panel with a refractory metal core (RMC) microcircuit. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15)
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16. A method of cooling a combustor of a gas turbine engine comprising:
communicating a cooling flow through a refractory metal core (RMC) microcircuit. - View Dependent Claims (17, 18, 19, 20)
Specification