Turbine rotor fabrication
AssigneeGeneral Motors Corporation
InventorKenneth R. Cross
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AssigneeGeneral Motors Corporation
InventorKenneth R. Cross
Estimating the term…
A method for manufacturing a hybrid, dual property turbine wheel assembly comprising the steps of preforming a blade element and separate support ring of a supperalloy material and locating the blades in support slots in the outer diameter of the support ring and radially outwardly of a preformed inner diameter underlying base tangs on each blade element; vacuum braze sealing each of the base tangs within a support slot and thereafter machining the inside diameter of the ring to expose the base tangs; thereafter joining the ring and undercut base tangs thereon to the outside diameter of a preformed disc element and vacuum braze sealing the hub disc and ring blade assemblies to produce a sealed interface region between the outside diameter of the hub element and the inside diameter of the ring and base tangs; and thereafter directly hot isostatically pressing the joined parts to form a direct diffusion bond between the tangs, ring and disc.
A method for fabricating a hybrid dual property wheel assembly comprising:
A method for fabricating a hybrid dual property wheel assembly comprising:
A method for fabricating a hybrid, dual property wheel assembly comprising:
A method for fabricating a hybrid, dual property wheel assembly comprising the steps of preforming a blade of a first predetermined high alloy material having a preformed wedge shaped base thereon, preforming a support ring for said blade element including a slot thereon including sloped walls to accept the wedge shaped base of said blade pressing each of said blade bases into one of said slots and tack welding each of the blades to the ring thereby to locate each blade on the ring, vacuum seal brazing each of the exposed joints between the blade base and the tapered walls of the slots on said ring, hot isostatically pressing each of said blades with respect to the support ring to diffusion bond across the interfaces of the slotted ring slot and wedge surfaces of individual blades, thereafter machining the inside diameter of the ring to a radius to expose a portion of the base of each of the blades, preforming a powdered metal disc, shrink fitting the ring and blade assembly to the outer diameter of the disc, vacuum braze sealing all exposed joint lines between the outer diameter of the disc and the inside diameter of the ring, and thereafter hot isostatically pressing the joined ring assembly and disc to produce a diffusion bond between the inside diameter of the ring, the exposed bottoms of the base of each of the blade elements and the disc.
Dependencies are inferred from the claim text.