crystal plasticity modeling of ni-based superalloys

1
PD Dr.-Ing. habil. B. Eidel Heisenberg-Fellow (DFG) Chair of Computational Mechanics Department of Mechanical Engineering B. Eidel University of Siegen, Chair of Computational Mechanics University of Duisburg-Essen, Institute of Mechanics Crystal Plasticity Modeling of Ni-Based Superalloys – Numerical Analysis and Experimental Validation Motivation For their high creep resistance at high temperatures Ni-based superalloys are used for single-crystalline blades in gas (air- craft/stationary) turbines. The composition of Ni-based su- peralloy is two-phase, one with semicoherent, ordered Ni 3 Al precipitates of L1 2 type (γ 0 -phase) embedded in a Ni-matrix of fcc structure (γ-phase). Size of a single precipitate: d p 0.4– 0.5 μm. Indentation with indenters of spherical as well as pyramidal shape are used to investigate the material’s plastic behavior. The key questions in the present, combined experimental and simulation analyses are: 1. Which continuum constitutive model is adequate for the two-phase material at room-temperature? 2. How does the indenter’s geometrically non-isotropic, pyramidal shape influence the elastoplastic deformations of the single crystal? How does the indenter’s azimuthal orientation influence the results? Will it break the symmetries of the crystal leading to pile-up pattern different from spherical indentation? 3. Which role plays the anisotropy in the elasticity law for the formation of anisotropic pile-up pattern? Aspects of modelling CMSX-4 at room temperature 1. Since the two phases each exhibit single-crystalline, fcc composition, an fcc crystal plasticity model is chosen assuming purely octahedral slip. 2. Since the length scale of the material is much smaller than the characteristic length scale of the experiment, the two-phase composition can be neglected and mod- elled as a ”homogenized” material. Crystal plasticity constitutive model Multiplicative decomposition F = F e F p Plastic velocity gradient L p = ˙ F p F p-1 = N X α=1 ˙ γ α S α 0 Schmidt Matrix S α 0 = s α 0 n α 0 Resolved shear stress τ α = S α 0 : σ Shear rate ˙ γ α = ˙ γ 0 τ α τ α r 1/m sgn(τ α ) Accumulated shear γ = N X α=1 Z t 0 | ˙ γ α | dt Hardening rate ˙ τ α r = N X β=1 h αβ |γ β | Hardening coefficients h αβ = h[q + (1 - q)δ αβ ] h = h 0 sech 2 h 0 γ τ s - τ 0 Fig. 1. : Spherical indentation into (001) CMSX-4. Left: Mi- crograph from experiment. Right: Perspective view on the in- dentation crater in experiment (left part) and simulation (right part), where pile-up hillocks emerge in <110> directions. X Y Z u_z: -1.00 -0.74 -0.47 -0.21 0.06 0.32 0.58 0.85 1.11 1.37 1.59 X Y Z u_z: -1.00 -0.75 -0.49 -0.24 0.01 0.27 0.52 0.77 1.03 1.28 1.49 X Y Z u_z: -0.70 -0.52 -0.35 -0.17 0.00 0.18 0.36 0.53 0.71 0.88 1.07 Fig. 2. : Pyramidal indentation into (001) CMSX-4. 1st row: experiment (SEM) for azimuthal orientation angle φ =0 , 22.5 , 45 . 2nd row: Corresponding pile-up in simulations, u z [μm]. Conclusions (I) The pyramidal indents constantly reflect the material’s cu- bic symmetry. Pile-up patterns invariantly emerge in <110> directions for different azimuthal orientations. The curved boundaries of the indent’s rim stem from a local adaption of the indenter to the pile-up. (II) Experiment and simulation show that pile-up is induced by glide on {111}<110> slip systems. It is mainly the geom- etry of the slip systems in the (001) oriented crystal which governs pile-up. Stress concentrations introduced by (i) dif- ferent indenter shapes, by (ii) the azimuthal orientation of a pyramidal indenter and also by (iii) the type of the elasticity law, have minor influence. (III) The ”homogenized” modeling of the heterogeneous 2- phase material is adequate since accurate; it correctly predicts in FEA the pile-up pattern formation. References [1] Y. Wang, D. Raabe, D., C. Kl¨ uber, F. Roters, Acta Mater. 52 (2004). [2] B. Eidel, PhD Thesis TU Darmstadt (Shaker, Aachen, 2005). [3] B. Eidel, F. Gruttmann, Comp. Mat. Sci. 39 (2007). [4] B. Eidel, Acta Mater. 59 (2011).

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Page 1: Crystal Plasticity Modeling of Ni-Based Superalloys

PD Dr.-Ing. habil. B. EidelHeisenberg-Fellow (DFG)Chair of Computational MechanicsDepartment of Mechanical Engineering

B. Eidel

University of Siegen, Chair of Computational Mechanics

University of Duisburg-Essen, Institute of Mechanics

Crystal Plasticity Modeling of Ni-Based Superalloys

– Numerical Analysis and Experimental Validation

• Motivation

For their high creep resistance at high temperatures Ni-based

superalloys are used for single-crystalline blades in gas (air-

craft/stationary) turbines. The composition of Ni-based su-

peralloy is two-phase, one with semicoherent, ordered Ni3Al

precipitates of L12 type (γ′-phase) embedded in a Ni-matrix

of fcc structure (γ-phase). Size of a single precipitate: dp ≈ 0.4–

0.5µm.

Indentation with indenters of spherical as well as pyramidal

shape are used to investigate the material’s plastic behavior.

The key questions in the present, combined experimental and

simulation analyses are:

1. Which continuum constitutive model is adequate for the

two-phase material at room-temperature?

2. How does the indenter’s geometrically non-isotropic,

pyramidal shape influence the elastoplastic deformations

of the single crystal? How does the indenter’s azimuthal

orientation influence the results? Will it break the

symmetries of the crystal leading to pile-up pattern

different from spherical indentation?

3. Which role plays the anisotropy in the elasticity law for

the formation of anisotropic pile-up pattern?

• Aspects of modelling CMSX-4 at room temperature

1. Since the two phases each exhibit single-crystalline, fcc

composition, an fcc crystal plasticity model is chosen

assuming purely octahedral slip.

2. Since the length scale of the material is much smaller

than the characteristic length scale of the experiment,

the two-phase composition can be neglected and mod-

elled as a ”homogenized” material.

• Crystal plasticity constitutive model

Multiplicative decomposition F = Fe Fp

Plastic velocity gradient Lp = FpFp−1 =N∑

α=1

γαSα0

Schmidt Matrix Sα0 = sα0 ⊗ nα

0

Resolved shear stress τα = Sα0 : σ

Shear rate γα = γ0

∣∣∣∣τα

ταr

∣∣∣∣1/m sgn(τα)

Accumulated shear γ =

N∑α=1

∫ t

0

|γα| dt

Hardening rate ταr =

N∑β=1

hαβ |γβ |

Hardening coefficients hαβ = h[q + (1− q)δαβ ]

h = h0 sech2

∣∣∣∣ h0 γ

τs − τ0

∣∣∣∣

Seite 1 von 1

05.01.2004file://H:\mytex\docs\Disse\TEX\pics-indentation\schick\dissertation_schick_53_0001....

Fig. 1. : Spherical indentation into (001) CMSX-4. Left: Mi-

crograph from experiment. Right: Perspective view on the in-

dentation crater in experiment (left part) and simulation (right

part), where pile-up hillocks emerge in <110> directions.

X

Y

Z

u_z: -1.00 -0.74 -0.47 -0.21 0.06 0.32 0.58 0.85 1.11 1.37 1.59

X

Y

Z

u_z: -1.00 -0.75 -0.49 -0.24 0.01 0.27 0.52 0.77 1.03 1.28 1.49

X

Y

Z

u_z: -0.70 -0.52 -0.35 -0.17 0.00 0.18 0.36 0.53 0.71 0.88 1.07

Fig. 2. : Pyramidal indentation into (001) CMSX-4. 1st row:

experiment (SEM) for azimuthal orientation angle φ = 0◦,

22.5◦, 45◦. 2nd row: Corresponding pile-up in simulations,

uz [µm].

• Conclusions

(I) The pyramidal indents constantly reflect the material’s cu-

bic symmetry. Pile-up patterns invariantly emerge in <110>

directions for different azimuthal orientations. The curved

boundaries of the indent’s rim stem from a local adaption of

the indenter to the pile-up.

(II) Experiment and simulation show that pile-up is induced

by glide on {111}<110> slip systems. It is mainly the geom-

etry of the slip systems in the (001) oriented crystal which

governs pile-up. Stress concentrations introduced by (i) dif-

ferent indenter shapes, by (ii) the azimuthal orientation of a

pyramidal indenter and also by (iii) the type of the elasticity

law, have minor influence.

(III) The ”homogenized” modeling of the heterogeneous 2-

phase material is adequate since accurate; it correctly predicts

in FEA the pile-up pattern formation.

References

[1] Y. Wang, D. Raabe, D., C. Kluber, F. Roters, Acta Mater. 52

(2004).

[2] B. Eidel, PhD Thesis TU Darmstadt (Shaker, Aachen, 2005).

[3] B. Eidel, F. Gruttmann, Comp. Mat. Sci. 39 (2007).

[4] B. Eidel, Acta Mater. 59 (2011).