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High Temperature Materials 21 Project:
The Present Status

10 Nov.1999

National Research Institute for Metals, Japan
(1999-2004)


1.Materials Design Team

Computer simulations of microstructures and properties. Both theoretical and empirical approaches are being made mainly with Ni-base superalloys and Ir-base refractory superalloys.

(1) Statistical Thermodynamics
Cluster Variation and Monte Carlo simulations for multi- component superalloys containing Re, Ir, etc.

(2)Thermodynamics
An equilibrium calculation model for multi-component Ni-base superalloys, containing platinum group metals, etc.

(3)Empirical approach
Databese and regression analysis: Alloy Design Program.

etc.

2.Microstructure Analysis Team

Microstructure evolution during process and service is being analised on different scales by using some equipments.

(1)APFIM
Phase equilibrium, site occupation, composition profile at phase interface, etc.in multi-component Ni-base superalloys.

(2)TEM
A TEM equipped with high temperature tensile holder is to be installed for in-situ observations of microstructure evolution and dislocation motion during creep.

(3)High Temp. X-ray Diffractometry
An X-ray Diffractometer with a hot stage (up to 1200C) is being used for misfit and lattice distortion measurements in coherent structures.

(4)Elastic moduli measurement
Elastic moduli measurement is being made with a new equipment up to 1100C.

(5)Creep analysis
Creep behaviour of SC/DS superalloys, e.g., 3rd generation alloys,is being analysed in connection with the micro- structural parameters above.

etc.

3.Ni-base Superalloy Team

Single crystal (SC) and directionally solidified (DS) superalloys are being developed under collaborations with private companies.

(1)Large gas turbines for combined cycle power plants Development of new SC superalloys and its application to actual gas turbines. An NRIM 3 rd generation SC superalloy (TMS-75) and a newly developed SC superalloy (TMS-82)are going to be tested in a gas turbine in 2000 year.

(2)Small gas turbines for co-generations, etc.
Development of new SC/DS superalloys with higher temperature capabilities as well as better hot corrosion resistance is conducted.

(3)Jet engines
Development of 4th genaration superalloys is being carried out.

etc.

4.Ceramics Team

Si3N4 with controlled grain boundary is being investigated. A Yb addition with some other ceramics to crystalise the glass phase is successfully applied.

5.Refractory Superalloy Team

Ultra-high temperature alloys with fcc/L12 coherent structures are being developed.

(1)Ir/Rh-base refractory superalloys
Ir/Rh-X (X= Nb,Hf,Zr, etc) binary alloys. Effects of L12 volume fraction, lattice misfit, morphology, etc on mechanical properties, deformation mechanisms, etc.

(2)Ductilisation of the refractory superalloys
Additions of minor elements including B, C, etc. as well as major additions of Ni etc.for ductilisation.

(3)Mixing Ir-base and Ni-base superalloys
Balancing cost performance, specific weight, etc is being tried by mixing the two superalloys in a different fractions.

etc.

6.Virtual Turbine Team

A virtual gas turbine system is being constructed in a computer by combining CFD, heat transfer analysis, and stress analysis programs with materials simulation programs.

Project Director: Hiroshi Harada (HARADA.Hiroshi@nims.go.jp)


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Last modified: Mon Apr 02 12:42:35 2001