Patent · US Expired

Method for manufacturing a dual alloy cooled turbine wheel

US4587700A · kind A · utility

53Cited by
15References
27Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 8, 1984
Grant dateMay 13, 1986
Priority date
Expiry dateJun 8, 2004

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49996
  • WIPO fieldMachine tools
  • WIPO sectorMechanical engineering

Abstract

A dual alloy cooled turbine is manufactured by casting a hollow cylinder of first nickel-base alloy material with high creep resistance to produce directionally oriented grain boundaries. A preform of a second nickel-base alloy material with high tensile strength and high low-cycle-fatigue strength is diffusion bonded into the bore of the hollow cylinder by subjecting the cylinder and preform to hot isostatic pressing. The resulting cylindrical block is cut into thin precisely flat wafers. A plurality of alignable holes for forming fluid cooling passages are photochemically etched into the individual wafers. The wafers then are laminated by vacuum diffusion bonding techniques, with the holes aligned to form fluid cooling passages. The resulting laminated block is machined to produce the turbine wheel with turbine blades through which the cooling passages extend.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.