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High-Temperature Thermomechanical Design & Microstructure ...
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High-Temperature Thermomechanical Design & Microstructure-based Models of Nickel-Based Superalloys
ARPA-E HITEMMP annual meeting, 10/21/2020
Arian Ghazari & Nasr GhoniemDepartment of Mechanical and Aerospace Engineering, University of California Los Angeles
Giacomo PoDepartment of Mechanical and Aerospace Engineering, University of Miami
Presentation Outline
Design Approaches: (1) linear elastic (strength-based), (2) non-linear elasto-visco-plastic (strain-based), (3) microstructure-basedASME BPV strength-based design rules and safety factorsNon-linear strain-based design: creep, creep-fatigue, ductility exhaustion, fracture, and ratcheting.
Example of HX header thermomechanical analysis.Microstructure-Based Creep Model for Haynes 282 Database; Material processing effects on the microstructure Mechanisms General model with micro-mechanics parameters Dislocation Dynamics of nickel-based superalloys.
Design-By-Analysis (DBA) Methodology
Linear-Elastic
Non-linear Elasto-
viscoplastic
Microstructure-Elasto-
viscoplastic
Analysis Type Failure Basis Difficulty
Exceed Strength Limits
Microstructure Damage (microcracks
& cavities)
Exceed Strain / Fracture Limits
Common
Specialized
Under Development
Material Selection & ASME allowable stress for creep High creep strength at 700-800 OC Oxidation resistance at elevated temperatures
ASME BPV Strength-Based Safety Factors through Path 1 & 2
Supporting Path1 Supporting Path2
Supporting Paths for Stress Linearization
Path 1 Path 2
Necking & Plastic Instability Limit๐ท๐ท๐๐ < ๐บ๐บ๐๐ 1.78 1.74
๐ท๐ท๐๐ + ๐ท๐ท๐๐ โค ๐๐.๐๐๐บ๐บ๐๐ 2.09 2.04
Combined Total Primary & Secondary Stress ๐ท๐ท + ๐ธ๐ธ โค ๐๐๐บ๐บ๐๐ 0.95 1.72
Plastic Flow Localization Limit ๐ท๐ท๐๐ + ๐ธ๐ธ๐๐ โค ๐บ๐บ๐๐ 0.49 1.09
Ductility Exhaustion Limit ๐ท๐ท๐๐ + ๐ท๐ท๐๐ + ๐ธ๐ธ โค ๐บ๐บ๐ ๐ 0.63 1.07
Non-linear Elastoviscoplastic Strain-Based Design
Damage Fractions Based on Strain
Strain Amplitude for Fatigue (Manson-Coffin)
What is the optimum grain size, dislocation density, precipitatedensity & size, stacking fault energy, composition, and gโ structure?
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Material Processing
Microstructure Optimized Properties
Microstructure-Based Creep Model
Objective: Develop a phenomenological model for creep & fatigue thatreflects the microstructure, consistent with transient & steady-state data.
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Microstructure-Based Model for Transient Plasticity (Creep & Fatigue Damage)
Diffusion controlled creep mechanismsNeal D. Evans
Kocks Model
Phenomenological Creep Model
11/4/2020 MAE 296B Lecture 12.1 13
Viscous glide velocity
Climb velocity
Mean-free paths Back (threshold) stress
Glide (fast) dislocation density evolution
Climb (slow) dislocation density evolution
Phenomenological Creep Model
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elastic Viscous glide Lattice diffusion
Climb-controlled glide
oxidationcorrosion
๐พ๐พโ solvus
creepstrength
๐พ๐พโ formingelements
GB carbides
Haynes 282: empirical design principlesโข Haynes 282 is a gamma-prime (๐พ๐พโ) precipitation-strengthened Ni-based superalloy for high-T applications.โข Designed as a wrought alloy with balanced fabricability and mechanical properties.
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๐พ๐พโ content
Sims et al. 1987
better formability/weldability better mechanical properties
L. Pike, Superalloys, 2008.
Haynes 282: from processing to microstructure
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T [โ]
1010โ, 2h
788โ, 8h
WQ
solution annealing+
components fabrication
solutionannealing
two-step aging
1121โ1149โ
1000๐พ๐พโ solvus
1032M23C6 solvus
1377Haynes 282 liquidus
L. Pike, Superalloys, 2008.J. Caron, Proceedings of the 8th International Symposium on Superalloy 718 and Derivatives, 2014.Kruger, K. L. Woodhead Publishing, 2017.
(Ti-Mo)-richMC carbides
Cr-rich M23C6โblockyโ carbides
at GBs
ASTM 3-9 (144-18 ๐๐๐๐)grain size
๐พ๐พโ precipitates in the ๐พ๐พ matrix (spherical D~20nm, ~20% v.f, unimodal)
t [h]
Creep lifetime estimationโข Creep lifetime estimation is typically performed
with stress-LMP curves.
โข Lifetime varies significantly depending on:1. sample dimensions (sheet vs plate)2. microstructure (grain size and
precipitates)
โข Lifetime prediction is inaccurate for1. Non-standard materials processing2. Rafting microstructures3. Heat-affected zones (HAZ)
โข Conservative design has significant impact on costs.
28x lifetime
72h 2016h
K. Vattappara, 2019.
Physics-based creep modelingโข Assuming Class II solid solution alloy behavior:
1. Nabarro-Herring creep (self diffusion of vacancies)2. Dislocation creep (glide + diffusion-assisted climb)3. Q = Ni self-diffusion coefficient
โข Creep rate:๐๐๐๐๐ท๐ท๐ฟ๐ฟ๐บ๐บ๐บ๐บ
๐๐ = ๐ด๐ด๐๐๐๐๐บ๐บ๐๐
2 ๐๐๐บ๐บ +๐ด๐ด๐๐
๐๐๐บ๐บ
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๐ท๐ท๐ฟ๐ฟ = ๐ท๐ท0๐๐๐๐๐๐ โ๐๐๐ ๐ ๐๐
โข Steady-state creep data is collected from the literature as a function of stress, temperature, and grain size.
โข We want to explain this data based on simple physics-based models.
Physics-based creep modelingโข ๐พ๐พโฒ precipitates cause a โthresholdโ stress:
๐๐๐๐๐ท๐ท๐ฟ๐ฟ๐บ๐บ๐บ๐บ
๐๐ = ๐ด๐ด๐๐๐๐๐บ๐บ๐๐
2 ๐๐๐บ๐บ
+ ๐ด๐ด๐๐๐๐๐บ๐บ
3+ ๐ด๐ด๐๐
๐๐ โ ๐๐๐ก๐ก๐ก๐บ๐บ
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โข The threshold stress is determined from micromechanical simulations, assuming that its major contribution is due to the dislocation-precipitates bypass stress.
โข ๐๐๐ก๐ก๐ก was estimated to be approximately 70MPa for Haynes 282.
โข Haynes 282 has high Mo content. Mo causes large lattice misfit.โข Assuming Class I solid solution alloy behavior:
1. Nabarro-Herring creep (self diffusion of vacancies)2. Dislocation creep (viscous glide + diffusion-assisted
climb)3. Q = Mo self-diffusion coefficient
โข Creep rate:๐๐๐๐๐ท๐ท๐ฟ๐ฟ๐บ๐บ๐บ๐บ
๐๐ = ๐ด๐ด๐๐๐๐๐บ๐บ๐๐
2 ๐๐๐บ๐บ + ๐ด๐ด๐๐
๐๐๐บ๐บ
3+ ๐ด๐ด๐๐
๐๐๐บ๐บ
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Micromechanical modeling of the threshold stress
๐พ๐พโฒ โ GSFE
๐พ๐พ โ GSFE
โข Discrete Dislocation Dynamics (DDD) simulations were used to estimate the threshold stress for dislocations-precipitates bypass as a function of
1. Precipitates size2. Precipitates volume fraction3. ๐พ๐พ/๐พ๐พโ lattice misfit
โข Three possible bypass mechanisms
Haynes 282
AB
C
Lattice misfit and Mo effects
Haynes 282 ~15% stronger
L. Pike, Superalloys, 2008.
E. Artz et al., Progress in Mat. Sci. 2001.
M. Santella, 24th Annual Conference on Fossil Energy Materials, 2010
โข Misfit stresses pin dislocations and increase the threshold stress.
Possible misfit effects:โข Misfit ~0 reduces the ๐พ๐พ/๐พ๐พโ
surface energy and reduces precipitates coarsening kinetics
โข Affects self-diffusionโข Alters stress in matrix and
precipitates โข Affects dislocations-
precipitates interaction
Linear elastic analysis coupled with strength-based limits give conservative MTBF because it is based on minimum properties and non-specific datasets.Non-linear elasto-viscoplastic analysis coupled with strain damage fraction rules is less
conservative and more relevant to operational transients. Conservatism must still be built in if exact microstructure information is not included.A microstructure-based creep model has been implemented to predict transient and
cyclic creep.Main creep mechanisms: viscous glide, climb, and diffusion. Slowest rate is due to
molybdenum. Some uncertainties exist regarding the effects of grain size and sample thickness. The model will be refined to address those with additional experiemnts.ฮณโ misfit stresses and dislocation-precipitate interaction have been implemented in our
Dislocation Dynamics Code (MODELIB) to predict fatigue and creep.
Conclusions