Coolable airfoil assembly
AssigneeGeneral Electric Company
InventorsRonald Scott Bunker, James William Bartos, Nicholas Damlis, Mark Eugene Noe, Steven Douglas Ward
Life of this patent
Estimating the term…
Loading patent…
AssigneeGeneral Electric Company
InventorsRonald Scott Bunker, James William Bartos, Nicholas Damlis, Mark Eugene Noe, Steven Douglas Ward
Estimating the term…
An apparatus and method including a closed-circuit coolable airfoil assembly for use and exposure in a hot fluid flow of a machine portion. The assembly includes a first flange configured to be connected with a casing of the machine portion. A second flange is configured to be connected with the casing. An airfoil is connected with and between the first flange and the second flange, the airfoil including a peripheral portion surrounding a medial portion. At least one channel is disposed in the peripheral portion, the channel extending between the first flange and the second flange and being in flow communication with each. A closed flow path is formed from the casing and through the first flange, the second flange and the channel in which a coolant fluid can pass to cool the airfoil assembly.
A closed-circuit coolable airfoil assembly for use and exposure in a hot fluid flow of a machine portion, comprising:
A process for closed-circuit cooling of an airfoil assembly, comprising:
A closed-circuit coolable airfoil assembly for use and exposure in a hot fluid flow of a machine portion, comprising:
Dependencies are inferred from the claim text.