Composite turbine wheel and process for making same
AssigneeSpecial Metals Corporation
InventorsDon M. Weaver, Steven H. Reichman
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AssigneeSpecial Metals Corporation
InventorsDon M. Weaver, Steven H. Reichman
Estimating the term…
A process for making a composite integral turbine wheel and the like, consisting of a plurality of blade elements of an airfoil shape connected at their inner ends to the periphery of a sintered rotor or hub and metallurgically bonded thereto. In accordance with the practice of the process, a plurality of identical blade elements in a final machined condition are inserted in a mold at accurate circumferentially-spaced intervals therearound and are disposed such that the inner root sections thereof extend inwardly of a mold cavity defining the rotor profile. The mold cavity is filled with metal powder composed of a high-strength, temperature-resistant alloy, and sintered into a coherent mass in a manner to effect a metallurgical bonding of the sintered rotor section to the individual blade elements. The resultant integral assembly is thereafter isostatically pressed at an elevated temperature for a period of time to effect a further densification of the sintered rotor section to a density approaching 100 percent theoretical density.
A process for making a composite turbine wheel or the like comprising a plurality of blades connected to the periphery of a hub which comprises the steps of forming a plurality of blade elements composed of a high temperature strength and fatigue resistant material including a blade section having an integrally-connected root section extending axially of the base of said blade section, finishing said blade elements to accurate final dimensions, positioning said blade elements in a mold in radially-oriented accurately-spaced circumferential relationship with said root sections thereof extending inwardly of a mold cavity defining the profile of the hub of said turbine wheel, filling said mold cavity with a superalloy metal powder of a particle size less than about 100 mesh and an oxygen content of less than about 200 ppm in a manner to achieve a loose powder packing density of at least about 60 percent of theoretical 100 percent density and effecting an embedment of said root sections in said metal powder, heating said mold and the assembled said blade elements and said metal powder in vacuum to an elevated temperature to effect a sintering of said metal powder into a coherent mass and a bonding thereof to said root sections, continuing said heating and sintering until the sintered said powder attains a density of at least about 90 of 100 percent theoretical density and to form a metallurgical diffusion bond between said root sections and the sintered said metal powder forming an integral assembly, and thereafter hot isostatically pressing said integral assembly at an elevated temperature under sufficient pressure for a period of time to effect a further densification of the sintered said powder defining the hub to a density approaching 100 percent of theoretical density.
A process for making a composite turbine wheel or the like comprising a plurality of blades connected to the periphery of a hub, which comprises the steps of forming a plurality of blade elements composed of a high temperature strength and fatigue resistant material, including a blade section having an integrally-connected root section extending axially of the base of said blade section, finishing said blade elements to accurately final dimensions, forming a hub section by placing a superalloy metal powder of a particle size less than about 100 mesh and an oxygen content of less than about 200 ppm in a mold cavity defining the profile of said hub section and formed with a plurality of accurately spaced notches around the periphery of said hub section, heating said metal powder to an elevated temperature in vacuum to effect a sintering thereof into a coherent mass of at least about 85 percent theoretical density producing a preform, removing said preform from said mold and positioning said blade elements with said root sections thereof in coacting relationship within said notches of said hub section and in radially oriented accurately circumferentially spaced relationship, heating the preliminarily assembled hub and blade sections in vacuum to an elevated temperature until the sintered said hub section attains a density of at least 90 percent of theoretical density and for a period of time to form a metallurgical diffusion bond between said root sections and said hub section forming an integral assembly, and thereafter hot isostatically pressing said integral assembly at an elevated temperature under sufficient pressure for a period of time to effect a further densification of the sintered said hub section to a density approaching 100 percent of theoretical density.
Dependencies are inferred from the claim text.