Evaporatively cooled rotor for a gas turbine engine
AssigneeAerodyne Research, Inc.
InventorsDavid B. Stickler, Jack L. Kerrebrock
Life of this patent
Estimating the term…
Loading patent…
AssigneeAerodyne Research, Inc.
InventorsDavid B. Stickler, Jack L. Kerrebrock
Estimating the term…
An evaporatively cooled rotor for a gas turbine engine. Each rotor defines an internal cavity which includes a vaporization section that corresponds generally to the blade section of the rotor and a condensing section that corresponds generally to the hub section of the rotor. A radial array of circumferentially disposed capture shelves is provided in the vaporization section for capturing cooling fluid contained within the internal cavity and flowing radially outward under the centrifugal field generated during rotation of the rotor. A barrier disposed along the inner surface of the rotor wall in the condensing section slows or temporarily stops the flow of cooling fluid prior to reaching the vaporization section and a perforated baffle attached to the capture shelves prevents cooling fluid from splashing out of the shelves.
An evaporatively cooled rotor adapted for rotation about an axis and having an internal cavity defining an inner surface and including a vaporization section disposed radially outwardly with respect to the rotational axis from a condensing section, the rotor further comprising:
An evaporatively cooled rotor adapted for rotation about an axis and having an internal cavity defining an inner surface and including a vaporization section disposed radially outwardly with respect to the rotational axis from a condensing section, the rotor further comprising:
An evaporatively cooled rotor adapted for rotation about an axis and having an internal cavity including a vaporization section disposed radially outwardly with respect to the rotational axis from a condensing section, the rotor further comprising:
An evaporatively cooled rotor adapted for rotation about an axis and having a rotor wall defining an internal cavity including a vaporization section disposed radially outwardly with respect to the rotational axis from a condensing section, the rotor further comprising:
Dependencies are inferred from the claim text.