Numerical Simulation of Void Closure Process at DD15/SC-4 Superalloys Interface during Hot Isostatic Pressing Diffusion Bonding

WAN Xin, TANG Tianxiang, LIU Jian, WANG Xuqing, PENG Zicao, CHEN Gaoqiang

Journal of Netshape Forming Engineering ›› 2026, Vol. 18 ›› Issue (7) : 1-10.

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Journal of Netshape Forming Engineering ›› 2026, Vol. 18 ›› Issue (7) : 1-10. DOI: 10.3969/j.issn.1674-6457.2026.07.001
Key Technologies for Precision Forming of High-end Energy and Aerospace Equipment Components

Numerical Simulation of Void Closure Process at DD15/SC-4 Superalloys Interface during Hot Isostatic Pressing Diffusion Bonding

  • WAN Xin1, TANG Tianxiang1, LIU Jian2, WANG Xuqing2, PENG Zicao2, CHEN Gaoqiang1,*
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Abstract

The work aims to analyze the effects of interface roughness, pressure, and temperature on the morphological evolution, as well as the stress and strain processes, of the diffusion bonding interface between dissimilar superalloys during hot isostatic pressing (HIP). With DD15 and SC-4 nickel-based superalloys as research objects, a series of 2D thermo-mechanical coupled finite element models featuring three distinct surface roughness characteristics (rough turning, finish turning, and finish turning & polishing) were established. The effects of roughness on interface evolution were analyzed. Furthermore, the effects of pressure (100 MPa and 40 MPa) and temperature (1 160, 1 180, and 1 200 ℃) on the bonding process and strain distribution were investigated. Validation against experimental data showed that the relative error in predicting the interface recrystallization width was only 8%, confirming the accuracy of the proposed model. At 1 180 ℃ and 100 MPa, all three roughness models achieved complete void closure. As the applied pressure decreased, varying degrees of residual voids appeared in all models; specifically, the peak stress on the DD15 side dropped from 30 MPa (at 100 MPa) to 15 MPa (at 40 MPa), representing a 50% reduction. When the temperature increased from 1 160 ℃ to 1 200 ℃, the peak equivalent plastic strain remained consistently at approximately 0.3. As the interface roughness decreases from rough turning to finish turning, the maximum equivalent plastic strain required for complete void closure decreases from 1.1 to 0.18. Under insufficient pressure, the limited extent of the plastic deformation zone causes material extrusion to be confined to the local contact areas of asperities, failing to effectively fill the residual gaps and resulting in residual voids of different degrees to three roughness models. While increasing the temperature reduces the deformation resistance of the materials and accelerates the interface closure process, the equivalent plastic strain distribution required for void closure remains nearly independent of temperature variations, provided the initial roughness is constant.

Key words

DD15 superalloys / SC-4 superalloys / hot isostatic pressing diffusion bonding / interface void closure / numerical simulation

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WAN Xin, TANG Tianxiang, LIU Jian, WANG Xuqing, PENG Zicao, CHEN Gaoqiang. Numerical Simulation of Void Closure Process at DD15/SC-4 Superalloys Interface during Hot Isostatic Pressing Diffusion Bonding[J]. Journal of Netshape Forming Engineering. 2026, 18(7): 1-10 https://doi.org/10.3969/j.issn.1674-6457.2026.07.001

References

[1] 史振宇, 刘晓文, 宋来聪, 等. 航空发动机应用领域粉末高温合金的研究进展[J]. 中国粉体技术, 2025, 31(1): 46-60.
SHI Z Y, LIU X W, SONG L C, et al.Research Progress of Powder Metallurgy Superalloy in Aero Engine Applications[J]. China Powder Science and Technology, 2025, 31(1): 46-60.
[2] 罗学军, 王珏, 赵巍, 等. FGH91粉末高温合金与K418B铸造叶环热等静压扩散连接研究[J]. 粉末冶金技术, 2021, 39(4): 291-296.
LUO X J, WANG J, ZHAO W, et al.Research on Diffusion Bonding of FGH91 Powder Metallurgy Superalloy and K418B Castedblade by Hot Isostatic Pressing[J]. Powder Metallurgy Technology, 2021, 39(4): 291-296.
[3] 吴雨萌, 姚志浩, 董建新. GH4169高温合金铸锭开坯锻造的组织模拟预测研究[J]. 精密成形工程, 2025, 17(8): 136-149.
WU Y M, YAO Z H, DONG J X.Microstructure Simulation and Prediction of Forging Process for GH4169 Superalloy Ingots[J]. Journal of Netshape Forming Engineering, 2025, 17(8): 136-149.
[4] TSUDA O, KANAMARU N, FURUTA S, et al.PM Nickel-Base Superalloy Dual-Property Disks Produced by Superplastic Forging[J]. Metal Powder Report, 1991, 46(3): 31-35.
[5] 于晶, 张琴, 欧阳志高. 航空发动机双合金涡轮整体叶盘结构分析及参数选取[J]. 装备制造技术, 2020(6): 53-56.
YU J, ZHANG Q, OUYANG Z G.Structural Analysis and Parameter Selection of Double-Alloy Turbine Blisk[J]. Equipment Manufacturing Technology, 2020(6): 53-56.
[6] SHI J M, LIU J T, JIN F, et al.Diffusion Bonding of FGH98 Superalloy and DD5 Single Crystal Using Pure Ni Interlayer[J]. Materials Today Communications, 2023, 37: 107003.
[7] 高峻, 罗皎, 李淼泉. 航空发动机双性能盘制造技术与机理的研究进展[J]. 航空材料学报, 2012, 32(6): 37-43.
GAO J, LUO J, LI M Q.Advance in Manufacture Technology and Mechanism of Aero-Engine Dual Property Disk[J]. Journal of Aeronautical Materials, 2012, 32(6): 37-43.
[8] 刘砚飞, 钟燕, 陶稀鹏, 等. 镍基单晶高温合金/热障涂层体系的应用研究进展[J]. 材料工程, 2025, 53(9): 1-10.
LIU Y F, ZHONG Y, TAO X P, et al.Research Progress in Application of Nickel-Based Single Crystal Superalloy/Thermal Barrier Coating System[J]. Journal of Materials Engineering, 2025, 53(9): 1-10.
[9] MA S J, CAO L, WANG X Z, et al.Influence of Heat Process on Microstructure and Mechanical Properties of DD5 Single Crystal Superalloy during Manufacturing[J]. Journal of Materials Engineering and Performance, 2025, 34(6): 5339-5346.
[10] NIU H Y, LIU Z Z, WANG H, et al.Effects of Hot Isostatic Pressing on the Micron-Scale Residual Stress of Nickel-Based Single-Crystal Superalloys[J]. Journal of Materials Science & Technology, 2025, 221: 102-116.
[11] ATKINSON H V, DAVIES S.Fundamental Aspects of Hot Isostatic Pressing: An Overview[J]. Metallurgical and Materials Transactions A, 2000, 31(12): 2981-3000.
[12] 周相, 李培跃, 王晓南, 等. 镍基合金扩散焊研究进展[J]. 焊接技术, 2023, 52(9): 5-11.
ZHOU X, LI P Y, WANG X N, et al.Research Process of Nickel Based Alloy Diffusion Welding[J]. Welding Technology, 2023, 52(9): 5-11.
[13] YAN R G, ZHU L N, LIU A, et al.Evaluation of Small Fatigue Crack Growth Rates in HIP FGH96 Superalloy under Microstructural Influences[J]. Fatigue & Fracture of Engineering Materials & Structures, 2025, 48(6): 2495-2505.
[14] 贾建, 陶宇, 张义文. 异种镍基高温合金热等静压扩散连接性研究[J]. 钢铁研究学报, 2011, 23(S2): 510-513.
JIA J, TAO Y, ZHANG Y W.Feasibility Study of Diffusion Bonding Dissimilar Ni-Based Superalloys by HIP[J]. Journal of Iron and Steel Research, 2011, 23(S2): 510-513.
[15] YANG J, LIU S Z, WANG X F, et al. HIP Diffusion Bonding of FGH96-DD6 Dual Alloys[J]. Materials Research Innovations, 2014, 18(sup4): S4-429-S4-434.
[16] 闫来成, 燕平, 赵京晨. 镍基高温合金HIP扩散连接的组织和性能[J]. 钢铁研究学报, 2012, 24(1): 48-53.
YAN L C, YAN P, ZHAO J C.Microstructure and Properties of Diffusion Couple of Superalloy Bonded by HIP[J]. Journal of Iron and Steel Research, 2012, 24(1): 48-53.
[17] 闫来成, 燕平, 赵京晨. 镍基双合金扩散偶的拉伸性能研究[J]. 粉末冶金工业, 2012, 22(1): 21-27.
YAN L C, YAN P, ZHAO J C.The Tensile Properties of Diffusion Couple of nickle-Base dual-Superalloy[J]. Powder Metallurgy Industry, 2012, 22(1): 21-27.
[18] GUO W, XIN J R, HAO D, et al.Diffusion Bonding of Nickel-Based Powder Metallurgy Superalloy FGH98 with Pure Nickel Interlayer[J]. Journal of Materials Research and Technology, 2024, 30: 267-282.
[19] ZHU F H, LI X F, PENG H L, et al.Analytical Approaches to Describe Diffusion Bonding of Similar and Dissimilar Materials[J]. Science and Technology of Welding and Joining, 2020, 25(8): 661-668.
[20] YUAN L, XIONG J T, PENG Y, et al.Modeling Void Closure in Solid-State Diffusion Bonding of TC4 Alloy[J]. Vacuum, 2020, 173: 109120.
[21] PENG Y, LI Z X, GUO W, et al.Modeling of Interfacial Void Closure and Prediction of Bonding Time in Solid-State Diffusion Bonding[J]. Journal of Materials Processing Technology, 2024, 324: 118267.
[22] CHANG R J, GUO Q Y, MA Z Q, et al.Kinetics of Voids Evolution during Diffusion Bonding of Dissimilar Metals on Consideration of the Realistic Surface Morphology: Modeling and Experiments[J]. Acta Materialia, 2024, 276: 120121.
[23] 刘浩铭, 丁方政, 蒋康河, 等. DD15/SC-4双合金热等静压扩散连接接头微观组织[J]. 材料工程, 2026, 54(2): 222-233.
LIU H M, DING F Z, JIANG K H, et al.Microstructure of DD15/SC-4 Dual-Alloy Hot Isostatic Pressure Diffusion Bonding Joint[J]. Journal of Materials Engineering, 2026, 54(2): 222-233.
[24] 《航空发动机设计用材料数据手册》编委会. 航空发动机设计用材料数据手册[M]. 北京: 航空工业出版社, 2010: 349-366.
Editorial Committee of Materials Data Handbook for Aero Engine Design. Materials Data Handbook for Aero Engine Design[M]. Beijing: Aviation Industry Press, 2010: 349-366.
[25] 《中国航空材料手册》编辑委员会. 中国航空材料手册. 第2卷,变形高温合金、铸造高温合金[M]. 北京: 中国标准出版社, 2001: 812-818.
Editorial Committee of China Aeronautical Materials Handbook. China Aeronautical Materials Handbook, Volume 2: Wrought Superalloys and Cast Superalloys[M]. Beijing: China Standards Press, 2001: 812-818.
[26] 王文泽. 镍基高温合金DD6力学性能及切削残余应力仿真研究[D]. 绵阳: 西南科技大学, 2024: 29-40.
WANG W Z.Study on the Mechanical Properties and Cutting Residual Stress Simulation of Nickel-Based Superalloy DD6[D]. Mianyang: Southwest University of Science and Technology, 2024: 29-40.
[27] 杨金龙. 镍基粉末高温合金FGH4113A热变形工艺及组织性能研究[D]. 长沙: 中南大学, 2024: 52-67.
YANG J L. Hot Deformation Process, Microstructure and Mechanical Properties of Ni-Based Powder Metallurgy Superalloy FGH4113A[D]. Changsha: Central South University, 2024: 52-67.
[28] LIU Y H, NING Y Q, YAO Z K, et al.Plastic Deformation and Dynamic Recrystallization of a Powder Metallurgical Nickel-Based Superalloy[J]. Journal of Alloys and Compounds, 2016, 675: 73-80.

Funding

Independent Innovation Special Fund of Aero Engine Corporation of China; The National Natural Science Foundation of China (52175334); Tsinghua University Initiative Scientific Research Program
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