Accession Number : ADA043688


Title :   Development of Hot Isostatically Pressed Rene 95 Turbine Parts


Descriptive Note : Final rept. Jul 1973-Jul 1976


Corporate Author : GENERAL ELECTRIC CO LYNN MA AIRCRAFT ENGINE BUSINESS GROUP


Personal Author(s) : Mathur, P S ; Bartos, J L


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a043688.pdf


Report Date : May 1977


Pagination or Media Count : 313


Abstract : To arrest the increasing cost of materials and fabrication techniques for high-strength gas turbine components, a contract was awarded to the General Electric Company to develop a reliable, low-cost, reproducible powder metallurgy production process for manufacturing premium quality HIP Rene 95 T700 gas generator turbine disks and cooling plates. The work to accomplish this objective was subdivided into four tasks.


Descriptors :   *ISOSTATIC PRESSING , *TURBINE COMPONENTS , *SUPERALLOYS , *GAS TURBINES , COOLING , PLATES , NICKEL ALLOYS , POWDER METALLURGY , DISKS , HELICOPTER ENGINES , HIGH TEMPERATURE , TURBOSHAFT ENGINES , POWDER ALLOYS , MECHANICAL PROPERTIES , MANUFACTURING


Subject Categories : Metallurgy and Metallography
      Fabrication Metallurgy
      Jet and Gas Turbine Engines


Distribution Statement : APPROVED FOR PUBLIC RELEASE