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Acta Metall Sin  2026, Vol. 62 Issue (2): 309-327    DOI: 10.11900/0412.1961.2025.00109
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Review of the Formation Mechanism and Control Technology for Freckle Defects in Directionally Solidified Superalloys
JIA Yuliang1,2, ZHANG Yongjia3, SHI Zekai4, SHEN Xu4, YIN Yajun4, SHI Changkun2, ZHOU Jianxin4(), LYU Zhigang1()
1 Department of Mechanical Engineering, Tsinghua University, Beijing 100084, China
2 Anhui Yingliu Hangyuan Power Technology Co. Ltd., Huoshan 237200, China
3 School of Energy and Mechanical Engineering, Jiangxi University of Science and Technology, Nanchang 330013, China
4 State Key Laboratory of Materials Processing and Die & Mould Technology, Huazhong University of Science and Technology, Wuhan 430074, China
Cite this article: 

JIA Yuliang, ZHANG Yongjia, SHI Zekai, SHEN Xu, YIN Yajun, SHI Changkun, ZHOU Jianxin, LYU Zhigang. Review of the Formation Mechanism and Control Technology for Freckle Defects in Directionally Solidified Superalloys. Acta Metall Sin, 2026, 62(2): 309-327.

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Abstract  

Freckles severely degrade the crystalline integrity and high-temperature mechanical properties of superalloy blades, posing a critical barrier to the fabrication of large-sized directionally solidified blades for heavy-duty gas turbines. This paper reviews the research progress on freckles over the past several decades, both domestically and internationally. It summarizes investigations of elemental segregation, thermo-solutal convection, and dendrite arm fragmentation during freckle formation using techniques such as atom probe tomography, synchrotron radiation, and numerical simulation. Freckle formation criteria based on temperature fields or mushy-zone density have been described, and the influences of blade geometry and solidification parameters on freckle distribution have been elucidated. Moreover, freckle control techniques and methods are comprehensively reviewed. At present, most studies on freckles focus on cases involving “small-sized specimens, low withdrawal rates (≤ 1.5 mm/min), and alloys with high W/Re contents”, which exhibit relatively significant differences from the freckle solidification conditions and occurrence patterns of “large blades, high withdrawal rates (≥ 2.0 mm/min), and alloys with low W/Re content” in the engineering practice of heavy-duty gas turbines. Therefore, developing rapid freckle prediction methods and effective control technologies specifically suited to the solidification conditions of large blades in heavy-duty gas turbines has become a critical need and a key research direction for the present and future.

Key words:  large-scale blade      directional solidification      superalloy      freckle      numerical modeling     
Received:  14 April 2025     
ZTFLH:  TG245  
Fund: National Key Research and Development Program of China(2024YFB3713805);Basic Research Program(JCKY-C102)
Corresponding Authors:  LYU Zhigang, professor, Tel: 13701333592, E-mail: lvzg@tsinghua.edu.cn;
ZHOU Jianxin, professor, Tel: 13871482400, E-mail: zhoujianxin@hust.edu.cn

URL: 

https://www.ams.org.cn/EN/10.11900/0412.1961.2025.00109     OR     https://www.ams.org.cn/EN/Y2026/V62/I2/309

Fig.1  Freckle defects and its formation mechanism of the large-sized industrial gas turbine blade[16] (a-c) freckle chains (showed by arrows) (a), dendritic crystal (b), and orientation images (c) of freckle chains (IPF—inverse pole figure) (d) schematic of formation mechanism of freckle defects
Fig.2  Freckle defects: microstructure in electron microscopy and composition obtained by atom probe tomography (APT)[12]
(a) SEM image displaying the four regions of interest (ROIs): the dendritic cores in the single crystal (SC-DC) and in the freckles (F-DC); the inter-dendritic regions in the SC (SC-ID) and in the freckles (F-ID)
(b-e) 3D APT reconstructions of samples lifted-out from the four ROIs
(f, g) Al, Cr, Co, Mo, Ta, W, and Re element concentrations in four ROIs
Fig.3  Distributions of freckle chains on blades with different alloy compositions[18]
(a) UCSX6 (b) UCSX7 (On the basis of UCSX6, add 1.5%Cr and 3.0%Mo, mass fraction)
(c) UCSX8 (On the basis of UCSX7, add 2% Ta, and reduce 2%W and 0.8%Re, mass fraction)
Fig.4  Experimental observation of channel segregation (a1, a2) upward jet flow parallel to gravity direction in NH4Cl solution (a1) and jet flow on the top side (a2)[11] (b1, b2) segregation channels (indicated by arrows) in Pb-2%Sb alloy (mass fraction, the same below) in different sections[21] (c1, c2) solute plumes during directional solidification of CMSX-4 alloy[13] (R—cooling rate, white arrows show the dendrite tips)
Fig.5  Simulation results of channel segregation during directional solidification
(a1, a2) velocity field (a1) and normalized concentration field (a2) of Ti element in CMSX2 alloy[23] (Cmix—mixture concentration, Cin—initial concentration)
(b1, b2) isosurfaces of liquid volume fraction (Color of streamtraces indicates mixture concentration of Sn, with corresponding levels shown in the upper color bar) (b1) and segregation channels of Sn (b2) during directional solidification of Pb-10%Sn[14]
(c1, c2) velocity field and segregation channels[30] (fs—solid volume fraction, ul—velocity of the melt, t—time, Teut—eutectic temperature)
Fig.6  Convection velocity near the convergence grain boundary by cellular automation simulation[36] (a1, a2) experimental results (Fig.6a2 is the corresponding magnified view) (b) simulation result
Fig.7  Phase field simulation results of dendrite morphology and solute concentration distribution during directional solidification of CMSX-4 alloy[46]
(a) dendrite deflection (G—temperature gradient, acrystal growth direction)
(b) dendrite remelt and protrude (c) dendrite branch and overgrowth
Fig.8  Isolated dendrites near solidification front
(a1, a2) convergence grain boundary (a1) and fractured dendrites (a2) in NH4Cl solution[11] (White arrow indicates the direction of the convective jet eroding the mushy zone)
(b1, b2) occurrence of isolated grains at time of 115 s (b1) and 135 s (b2) during directional solidification of Ga-25%In alloy by synchrotron radiation observation[52] (Numbers 1 and 2 represent grains)
Fig.9  Freckle formation map of CMSX-4 alloy with different temperature gradients and solidification rates[56]
Fig.10  Mushy zones and velocity fields for René N4 alloy (a1, a2) and Ni-Al-W alloy (b1, b2)[64] (a1, b1) reconstructed morphologies (a2, b2) simulated velocity fields
CategoryImpact factor
TemperatureBlade designDimensionsCross-sectionCurvature
field(Abrupt change, gradual change)
PreparationMold positioningSolidification rateMold parameters
process(Withdrawal rate,(Structure and temperature)
temperature gradient)
Solute fieldAlloyW, ReAlTa
composition(Heavy elements with(Light elements with(Heavy elements with
negative segregation)positive segregation)positive segregation)
SolidificationGravityMagnetic fieldCrystal characteristics
conditions(Orientation and grain
boundaries)
Table 1  Influence factors of freckle formation
Fig.11  Freckle distributions of sample with varied cross-sections (a, b) samples with increased section (a) and decreased section (b)[58]Z indicates the incubation distance for the freckle onset after varying the specimen diameter. A, B, and C represent the freckle chains. Yellow, red, green, and blue arrows represent radiation lines) (c) freckle chains on sample with increased and decreased sections[66]
Content of W, Re, and Al in nickel-based alloys*DimensionWithdrawal rateRef.

Mar-M200: 13.2W-4.9Al...

Udimet700: 4.19Al...

ϕ101.6 mm-[9]
CMSX-4: 6W-3Re-5.6Al...Thickness: 10 mm

1, 6 mm·min-1

(Intense freckle occurs at a rate of 1 mm·min-1)

[72]
DD33: 6W-4Re-6Al...

Thickness: 0.6-10 mm

(Freckles tendency inward)

1, 3, 6 mm·min-1

(Intense freckle occurs at a rate of 1 mm·min-1)

[59]
CMSX-4: 6W-3Re-5.6Al...20 mm × 40 mm × 50 mm

1.2, 4.2 mm·min-1

(Intense freckle occurs at a rate of 1.2 mm·min-1)

[73]
CMSX-4: 6W-3Re-5.6Al...

Nearly ϕ20 mm

(Freckles tendency inward)

1 mm·min-1[58]
PW1483: 1.81W-3.63Al...

Nearly ϕ15 mm

(Freckles tendency inward)

1 mm·min-1[60]
6.52W-4.89Re-5.69Al...

60 mm × 25 mm × 150 mm

(Freckles tendency inward)

1.5 mm·min-1[30]
Table 2  Sample size, withdrawal rate, and alloy composition of sample with freckles in the literatures [9,30,58-60,72,73]
EffectDensity/segregationElement
PromoteHeavy elements/negative segregationRe, W
Light elements/positive segregationAl
InhibitHeavy elements/positive segregationTa
Light elements/negative segregation-
Table 3  Alloy elements affecting solute convection
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