SBIR-STTR Award

P/M Near-Net-Shape Formed Superalloy Turbine Wheels
Award last edited on: 11/1/2005

Sponsored Program
SBIR
Awarding Agency
DOD : DARPA
Total Award Amount
$827,053
Award Phase
2
Solicitation Topic Code
DARPA93-004
Principal Investigator
Gunes Ecer

Company Information

Globix

PO Box 4025
Thousand Oaks, CA 91359
   (805) 529-9038
   N/A
   N/A
Location: Single
Congr. District: 26
County: Ventura

Phase I

Contract Number: ----------
Start Date: ----    Completed: ----
Phase I year
1994
Phase I Amount
$77,722
An improvement to a power metallurgy near-net-shape consolidation process, Radially Constricted Consolidation (RCC) process, is proposed. Program objective is to develop complex shaped ceramic containers (shells) for soft die hot pressing of powders using the RCC process. Shells to be developed are intended for consolidation of copper alloys, iron, iron base alloys, and stainless steels. Taguchi methods will be used to design and execute the experimental study. Experiments will involve design factors such as shell chemistry, time and temperature of drying, particle size, etc. If successful, the results will allow commercialization of the RCC process for small and medium sized P/M parts. Phase II work will scale-up the shell size, provide scientific understanding of successful shell compositions, and produce prototype parts, and test them. The RCC process has the potential of becoming a major P/M process which can expand markets served by the P/M industry into larger and more complex shaped parts. Anticipated

Benefits:
The proposed research and development effort will allow the potential of the RCC process to be realized. Manufacture of small and medium sized complex shaped parts, up to now impossible to manufacture by any other P/M process, will be possible. Many castings and welded assemblies, including those used in aero-space applications, may be replaced by RCC products with better properties and lower cost.

Phase II

Contract Number: ----------
Start Date: ----    Completed: ----
Phase II year
1996
Phase II Amount
$749,331
Development of powder metallurgy (P/M) near-net-shape consolidation of superalloy turbine wheels using the Radially Constricted Consolidated (RCC) process, is proposed. Program objective is to demonstrate commercial worthiness of the RCC process. A process for making robust ceramic molds (shells) for RCC processing of metals ws developed in Phase I. In Phase II, shell size and complexity will be scaled up, and small quantities of a nickel base superalloy turbine wheel will be produced and evaluated. The whell is a 8lbs (3.6 kg) highly stressed component of T-40-8 jet fuel starter used on F-16 aircraft. A finite element model of the RCC densification process will be developed as a predictive tool. Tensile, high cycle fatigue, stress-rupture tests, chemical analyses, and dimensional conformity tests will be utilized to assess the experimental wheels. Thermal-mechanical fluidized bed tests will compare the RCC produced wheels to presently used cast wheels. If successful, the Phase II will allow the RCC process to become a major new force in the P/M near-net-shape processing field. Anticipated

Benefits:
The proposed research and development effort will allow the potential of the RCC process to be realized. Manufacture of small and medium sized complex shaped parts, up to now impossible to manufacture by any other P/M process, will be possible. Many castings and welded assemblies, including those used in aero-space applications, may be replaced by RCC products with better properties and lower cost.