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1

Yamamoto, Masato, and Takashi Ogata. "Microscopic Damage Mechanism of Nickel-Based Superalloy Inconel 738LC Under Creep-Fatigue Conditions." Journal of Engineering Materials and Technology 122, no. 3 (2000): 315–20. http://dx.doi.org/10.1115/1.482803.

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Creep-fatigue damage in Inconel 738LC was clarified by in-situ observation and a new creep-fatigue life prediction model was proposed based on the mechanism identified. Creep-fatigue tests on standard specimens show that the tensile hold creep-fatigue lives were reduced to 60 to 80 percent and those in the compressive hold condition were reduced to 20 to 40 percent of the fatigue life of the same total strain condition. In-situ creep-fatigue tests on miniature specimens show that grain boundary sliding could be observed under the compressive strain hold condition and under the tensile strain h
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2

Alinaghian, H., A. Farzadi, P. Marashi, and M. Pouranvari. "Wide Gap Brazing of Inconel 738LC Nickel-Based Superalloy: Metallurgical and Mechanical Characteristics." Metallurgical and Materials Transactions A 51, no. 12 (2020): 6283–93. http://dx.doi.org/10.1007/s11661-020-06027-1.

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3

Ojo, O. A., N. L. Richards, and M. C. Chaturvedi. "Microstructural study of weld fusion zone of TIG welded IN 738LC nickel-based superalloy." Scripta Materialia 51, no. 7 (2004): 683–88. http://dx.doi.org/10.1016/j.scriptamat.2004.06.013.

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4

Dobrovská, Jana, Simona Dočekalová, Věra Dobrovská, and Karel Stránský. "Effect of Cooling Rate on Structural and Chemical Microheterogeneity of IN 738LC Nickel Based Superalloy." Solid State Phenomena 138 (March 2008): 201–8. http://dx.doi.org/10.4028/www.scientific.net/ssp.138.201.

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The paper deals with the effect of cooling rate on solidification behavior of IN 738LC nickel based superalloy and on resulting structural and chemical microheterogeneity of this alloy. Samples taken from as-received state were heated with controlled ramp rates (1, 5, 10 and 20 °C min-1). Immediately after melting they were cooled with the same controlled ramp rate with the help of the laboratory experimental system SETARAM SETSYS 18TM TG/DTA/TMA. Then the microanalysis of minority phases was conducted with use of X-ray spectroscopy and microstructure of the individual samples was documented b
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5

IBUCHI, Hiroaki, Hirofumi KIMURA, Masao SAKANE, Masateru OHNAMI, Masamitsu MURAMATSU, and Kazushige FUJIYAMA. "Damage evaluation of Inconel 738LC nickel-base superalloy in creep-fatigue." Journal of the Society of Materials Science, Japan 39, no. 440 (1990): 522–28. http://dx.doi.org/10.2472/jsms.39.522.

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6

Khathem, S., M. Mohammed, and F. Hashim. "The Effect of Brazing Temperature on Shear Strength of Nickel Based Superalloy (Inconel 738LC) Joints." Acta Physica Polonica A 135, no. 5 (2019): 919–21. http://dx.doi.org/10.12693/aphyspola.135.919.

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7

Su, C. Y., C. P. Chou, B. C. Wu, and W. C. Lih. "Plasma transferred arc repair welding of the nickel-base superalloy IN-738LC." Journal of Materials Engineering and Performance 6, no. 5 (1997): 619–27. http://dx.doi.org/10.1007/s11665-997-0055-7.

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8

Juliš, Martin, Karel Obrtlík, Simona Hutařová, Tomáš Podrábský, and Jaroslav Polák. "Influence of Al-Si Diffusion Coating on Low Cycle Fatigue Properties of Cast Superalloy Inconel 738LC at 800 °C." Key Engineering Materials 488-489 (September 2011): 307–10. http://dx.doi.org/10.4028/www.scientific.net/kem.488-489.307.

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High temperature low cycle fatigue behaviour of cast nickel-based superalloy Inconel 738LC in as-received condition and coated with an Al-Si diffusion layer was studied. The Al-Si protective layer was deposited on the gauge section of cylindrical specimens using the slurry technique. Fatigue tests were performed on cylindrical specimens under total strain control in symmetrical cycle at 800 °C in air. The coating has a beneficial effect on fatigue life in the low amplitude domain. The stress response of the coated material is higher for high amplitudes in comparison with the uncoated one. Frac
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9

Jalilvand, V., H. Omidvar, M. R. Rahimipour, and H. R. Shakeri. "Influence of bonding variables on transient liquid phase bonding behavior of nickel based superalloy IN-738LC." Materials & Design (1980-2015) 52 (December 2013): 36–46. http://dx.doi.org/10.1016/j.matdes.2013.05.042.

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10

Obrtlík, Karel, Alice Chlupová, Martin Petrenec, and Jaroslav Polák. "Low Cycle Fatigue of Cast Superalloy Inconel 738LC at High Temperature." Key Engineering Materials 385-387 (July 2008): 581–84. http://dx.doi.org/10.4028/www.scientific.net/kem.385-387.581.

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Cylindrical specimens of cast polycrystalline nickel base superalloy Inconel 738LC were cyclically strained under total strain control at 23 and 800 °C to fracture. Cyclic hardening/softening curves, cyclic stress-strain curves, and fatigue life curves were obtained at both temperatures. Surface relief was studied in specimens fatigued to failure using scanning electron microscopy. Cyclic hardening/softening behaviour depends both on temperature and strain amplitude. Low amplitude straining was characterized by saturation of the stress amplitude. In high amplitude straining a pronounced harden
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11

Saghafi, AliAkbar, JamshidAghazade Mohandesi, and Hamid RezaAlizade Attar. "Characterization of Gamma Prime Phase in Hafnium Doped IN-738LC Nickel Base Superalloy." Journal of Engineering and Technology 4, no. 2 (2014): 121. http://dx.doi.org/10.4103/0976-8580.141200.

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12

Park, Jung Hong, M. S. Ku, Jeong Suk Kim, K. H. Lee, Y. S. Song, and Myung Chang Kang. "The High Temperature Fatigue Behavior of Inconel-738LC Material Deposited Thermal Barrier Coating." Advanced Materials Research 264-265 (June 2011): 1409–14. http://dx.doi.org/10.4028/www.scientific.net/amr.264-265.1409.

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This work investigated the thermal fatigue behavior of Inconel-738LC material deposited thermal barrier coating by Vacuum Plasma Spray(VPS). The Inconel-738LC material which is widely used as a turbine parts is a CoNi-based superalloy with CoNiCrAlY bond coating and ZrO2-8wt%Y2O3 ceramic top coating. The microstructure of coating layer was analyzed by SEM/EDS and XRD. Thermal fatigue tests were performed using compact tension specimens at 550°C, 750°C, 950°C with the load frequency of 10Hz. The fatigue crack growth behavior was characterized depending on number of cycles. The crack growth rate
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13

Vilanova, Mireia, Rubén Escribano-García, Teresa Guraya, and Maria San Sebastian. "Optimizing Laser Powder Bed Fusion Parameters for IN-738LC by Response Surface Method." Materials 13, no. 21 (2020): 4879. http://dx.doi.org/10.3390/ma13214879.

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A method to find the optimum process parameters for manufacturing nickel-based superalloy Inconel 738LC by laser powder bed fusion (LPBF) technology is presented. This material is known to form cracks during its processing by LPBF technology; thus, process parameters have to be optimized to get a high quality product. In this work, the objective of the optimization was to obtain samples with fewer pores and cracks. A design of experiments (DoE) technique was implemented to define the reduced set of samples. Each sample was manufactured by LPBF with a specific combination of laser power, laser
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14

Gradzik, Andrzej, Jacek Nawrocki, Grażyna Mrówka-Nowotnik, and Jan Sieniawski. "Laser Surfacing of Superalloy Inconel 738LC-Based Alloy Stellite 694 – Overlay Weld Imperfections." Biuletyn Instytutu Spawalnictwa 2017, no. 4 (2017): 25–31. http://dx.doi.org/10.17729/ebis.2017.4/3.

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15

Sajjadi, S. A., A. Chaichi, H. R. Ezatpour, A. Maghsoudlou, and M. A. Kalaie. "Hot Deformation Processing Map and Microstructural Evaluation of the Ni-Based Superalloy IN-738LC." Journal of Materials Engineering and Performance 25, no. 4 (2016): 1269–75. http://dx.doi.org/10.1007/s11665-016-1967-x.

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16

Baghlani, V., P. Mehbudi, J. Akbari, Erfan Zal Nezhad, Ahmed A. D. Sarhan, and A. M. S. Hamouda. "An optimization technique on ultrasonic and cutting parameters for drilling and deep drilling of nickel-based high-strength Inconel 738LC superalloy with deeper and higher hole quality." International Journal of Advanced Manufacturing Technology 82, no. 5-8 (2015): 877–88. http://dx.doi.org/10.1007/s00170-015-7414-6.

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17

朱, 静., null Re同Cr和Co元素共偏聚于尖端区域, and null HUANG Ming & ZHU Jing. "nickel-based single crystal superalloy." SCIENTIA SINICA Technologica 46, no. 1 (2015): 54–60. http://dx.doi.org/10.1360/n092015-00173.

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18

Erdeniz, Dinc, Tobias A. Schaedler, and David C. Dunand. "Deposition-based synthesis of nickel-based superalloy microlattices." Scripta Materialia 138 (September 2017): 28–31. http://dx.doi.org/10.1016/j.scriptamat.2017.05.027.

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19

Monteiro, Waldemar A., and Ingrid A. Dos Santos. "Microstructural evolution of a nickel-based superalloy." Proceedings, annual meeting, Electron Microscopy Society of America 48, no. 4 (1990): 936–37. http://dx.doi.org/10.1017/s0424820100177817.

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Superalloys are indispensable for the superior perfomance and efficien of jet engine turbine disks,turbine blades,combustors,roket shells and many other devices and components used in various industries, in Cluding nuclear, space and aeronautics.Over the last thirty years,nickel-base superalloys has undergone more structural studies than any other superalloy as a result of attempts to correlate its properties to microstructure and heat treatment. To avoid contradictory or inconsistent findings, it is also necessary a carefully microstructural observation of the employed starting materials. In
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20

Wu, Bao Hai, Cheng Yu Zheng, Ming Luo, and Xiao Dong He. "Investigation of Trochoidal Milling Nickel-Based Superalloy." Materials Science Forum 723 (June 2012): 332–36. http://dx.doi.org/10.4028/www.scientific.net/msf.723.332.

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Nickel-based superalloy is a relatively new class of materials that exhibit high mechanical strength, ductility, creep resistance at high operating temperatures and stress levels. It is widely used in aero engine parts such as blade and blisk. Due to its high hardness and high strength at high temperature, it’s difficult to machine nickel-based alloy. In order to reduce tool wear, trochoidal milling strategy is studied in this paper. With trochoidal tool path strategy, tool load can be reduced and the tool has enough time to be cooled under high cutting temperature. Tool immersion angle in tro
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21

Podany, Pavel, Zbysek Novy, and Jaromir Dlouhy. "Recrystallization behaviour of a nickel-based superalloy." Materiali in tehnologije 50, no. 2 (2016): 199–205. http://dx.doi.org/10.17222/mit.2014.163.

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22

Ma, Peili, and Jing Zhu. "Magnesium distribution in a nickel-based superalloy." Metallography 19, no. 1 (1986): 115–18. http://dx.doi.org/10.1016/0026-0800(86)90011-x.

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23

Kim, Kyomin, and Woochul Kim. "Thermophysical Properties of Nickel-based Superalloy CM247LC." Transactions of the Korean Society of Mechanical Engineers - B 44, no. 10 (2020): 619–25. http://dx.doi.org/10.3795/ksme-b.2020.44.10.619.

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24

Zhang, Bing, Chun-hu Tao, Xin Lu, Chang-kui Liu, Chun-yan Hu, and Ming-yuan Bai. "Recrystallization of single crystal nickel-based superalloy." Journal of Iron and Steel Research International 16, no. 6 (2009): 75–79. http://dx.doi.org/10.1016/s1006-706x(10)60031-3.

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25

Lone, Shafaq Ashraf, and Atikur Rahman. "Electroless nanoceria films on nickel-based superalloy." Surface Engineering 36, no. 9 (2019): 936–43. http://dx.doi.org/10.1080/02670844.2019.1662225.

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26

Kim, T. K., Jin Yu, and J. Y. Jeon. "Creep rupture in a nickel-based superalloy." Metallurgical Transactions A 23, no. 9 (1992): 2581–87. http://dx.doi.org/10.1007/bf02658061.

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27

Hou, Xue Qin, Yu Huai He, and Tao Jiang. "Study on Fracture Morphologies of Nickel Based P/M Superalloy." Materials Science Forum 788 (April 2014): 531–37. http://dx.doi.org/10.4028/www.scientific.net/msf.788.531.

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Fracture morphology analysis is an important way to understand material fracture process, find the reason of fracture and improve its performance. Nickel based powder metallurgy (P/M) superalloy is an important material which is widely used in the modern aeronautic and astronautic industry. In order to determine the fracture characteristic morpholgies and mechanisms of the P/M superalloy fractured at different conditions, the fracture surfaces of the high temperature low cycle fatigue,high cycle fatigue, high-low cycle complex fatigue, tension and creep specimens from the P/M superalloy were s
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28

Xiong, Jiangtao, Lin Yuan, Yuan Zhu, Hao Zhang, and Jinglong Li. "Diffusion bonding of nickel-based superalloy GH4099 with pure nickel interlayer." Journal of Materials Science 54, no. 8 (2019): 6552–64. http://dx.doi.org/10.1007/s10853-018-03274-x.

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29

Xiao, Gui Jian, Yun Huang, Gui Lin Chen, Zhi Wu Liu, and Xiu Mei Liu. "Investigations on Belt Grinding of GH4169 Nickel-Based Superalloy." Advanced Materials Research 1017 (September 2014): 15–20. http://dx.doi.org/10.4028/www.scientific.net/amr.1017.15.

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The majority of aero-engine components are designed and manufactured with nickel-based superalloy GH4169 in mind. There is little information available in the literature related to belt grinding processes of aero-engine components. Up to now, limited research has been reported in the use of belt for grinding aero-engine components made of nickel-based superalloy GH4169. A case study of an abrasive belt grinding performance applied on nickel-based superalloy GH4169 in manufacturing processes is presented, aiming to investigate the possibility of using belt grinding as a operation for components
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30

Yamaguchi, Yoshiya, Hiromu Hisazawa, and Yoshihiro Terada. "Microstructure Quantification in Nickel-Based Superalloy Udimet 720Li." MATERIALS TRANSACTIONS 60, no. 4 (2019): 593–601. http://dx.doi.org/10.2320/matertrans.m2018389.

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31

Petronić, Sanja, Dubravka Milovanović, Anđelka Milosavljević, Željko Radovanović, Olivera Erić-Cekić, and Radomir Jovičić. "Laser treatments of Nimonic 263 nickel-based superalloy." Zastita materijala 60, no. 1 (2019): 26–43. http://dx.doi.org/10.5937/zasmat1901026p.

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32

ZHANG, Bing, Xue-gang CAO, De-lin LIU, and Xin-ling LIU. "Surface recrystallization of single crystal nickel-based superalloy." Transactions of Nonferrous Metals Society of China 23, no. 5 (2013): 1286–92. http://dx.doi.org/10.1016/s1003-6326(13)62595-9.

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33

ZHANG, Bing, Chang-kui LIU, Jin-yi ZHOU, and Chun-hu TAO. "Dynamic recrystallization of single-crystal nickel-based superalloy." Transactions of Nonferrous Metals Society of China 24, no. 6 (2014): 1744–49. http://dx.doi.org/10.1016/s1003-6326(14)63248-9.

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34

Qu, Jing-long, Zhong-nan Bi, Jin-hui Du, Min-qing Wang, Qing-zeng Wang, and Ji Zhang. "Hot Deformation Behavior of Nickel-Based Superalloy GH4720Li." Journal of Iron and Steel Research International 18, no. 10 (2011): 59–65. http://dx.doi.org/10.1016/s1006-706x(12)60023-5.

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35

Zhang, Dayi, Fabrizio Scarpa, Yanhong Ma, Katarzyna Boba, Jie Hong, and Hongwei Lu. "Compression mechanics of nickel-based superalloy metal rubber." Materials Science and Engineering: A 580 (September 2013): 305–12. http://dx.doi.org/10.1016/j.msea.2013.05.064.

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36

Meyer, A., E. Daenicke, K. Horke, et al. "Metal injection moulding of nickel-based superalloy CM247LC*." Powder Metallurgy 59, no. 1 (2016): 51–56. http://dx.doi.org/10.1080/00325899.2016.1142058.

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37

Amulele, G. M., and A. G. Every. "Wave propagation in an anisotropic nickel-based superalloy." Ultrasonics 38, no. 1-8 (2000): 252–55. http://dx.doi.org/10.1016/s0041-624x(99)00140-7.

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38

Rakoczy, Łukasz, Lechosław Tuz, and Krzysztof Pańcikiewicz. "HOT CRACKING OF NICKEL-BASED SUPERALLOY TURBINE BLADE." Metallurgy and Foundry Engineering 41, no. 4 (2015): 181. http://dx.doi.org/10.7494/mafe.2015.41.4.181.

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39

Rahim, Erween Abdul, and Hiroyuki Sasahara. "Surface Integrity in MQL Drilling Nickel-Based Superalloy." Key Engineering Materials 447-448 (September 2010): 811–15. http://dx.doi.org/10.4028/www.scientific.net/kem.447-448.811.

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Nickel-based superalloys remain the most widely used of all materials in aerospace industry, contributed over 50 % of the weight of a jet engine. In machining of any jet engine components, it is necessary to satisfy the surface quality or surface integrity requirements to facilitate high reliability components. In the present study, surface integrity of Inconel 718 was studied when drilling under different lubricants. The holes were drilled individually using indexable AlTiN coated carbide drill under minimum quantity of lubricant (MQL) conditions. The results demonstrated that the machining c
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40

Hayashi, M., A. Jakobsson, T. Tanaka, and S. Seetharaman. "Surface tension of nickel based superalloy CMSX-4." High Temperatures-High Pressures 35/36, no. 4 (2003): 441–45. http://dx.doi.org/10.1068/htjr123.

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41

Semaltianos, N. G., W. Perrie, J. Cheng, et al. "Picosecond laser ablation of nickel-based superalloy C263." Applied Physics A 98, no. 2 (2009): 345–55. http://dx.doi.org/10.1007/s00339-009-5399-4.

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42

Terashima, H., Y. Ohta та Y. G. Nakagawa. "β-Ni4W phase precipitation in nickel-based superalloy". Materials Science and Engineering 89 (травень 1987): L15—L18. http://dx.doi.org/10.1016/0025-5416(87)90266-7.

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43

Rafiei, Mohsen, Hamed Mirzadeh, Mehdi Malekan, and Mohammad Javad Sohrabi. "Homogenization kinetics of a typical nickel-based superalloy." Journal of Alloys and Compounds 793 (July 2019): 277–82. http://dx.doi.org/10.1016/j.jallcom.2019.04.147.

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44

Yagi, Ryohei, and Toru H. Okabe. "Recovery of Nickel from Nickel-Based Superalloy Scraps by Utilizing Molten Zinc." Metallurgical and Materials Transactions B 48, no. 1 (2016): 335–45. http://dx.doi.org/10.1007/s11663-016-0854-z.

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45

Zagula-Yavorska, Maryana. "Rhodium influence on the microstructure and oxidation behaviour of aluminide coatings deposited on pure nickel and nickel based superalloy." High Temperature Materials and Processes 38, no. 2019 (2019): 621–27. http://dx.doi.org/10.1515/htmp-2019-0008.

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AbstractThe rhodium 0,5 μm thick layer was deposited on pure nickel and CMSX 4 Ni-based superalloy using the electroplating method. The rhodium coated substrates were aluminized by the CVD method. Oxidation resistance of nonmodified and rhodium modified coatings deposited both on nickel and CMSX 4 superalloy was compared. The triple-layer structure of rhodium modified coatings deposited on pure nickel was found. The β-(Ni,Rh)Al, rhodium doped γ'-Ni3Al and rhodium doped γ-Ni(Al) phases were the main components of the coatings on pure nickel. Two layers – additive and interdiffusion ones were id
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46

Tian, Su Gui, Xian Lin Meng, Ning Tian, and Hui Chen Yu. "Microstructure and Creep Property of DZ125 Nickel-Based Superalloy." Materials Science Forum 747-748 (February 2013): 697–702. http://dx.doi.org/10.4028/www.scientific.net/msf.747-748.697.

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By means of creep property measurement and microstructure observation, an investigation has been made into the creep behaviors of DZ125 superalloy at high temperature and low stress. Results showed that the superalloy under the applied stress of 137MPa at 1293 K displayed a better creep resistance, and the apparent creep activation energy of the alloy during steady state creep was measured to be Q = 325.57 kJ/mol. The various microstructures were displayed in different regions of the sample, thereinto, the rafted γ phase was uniformly distributed in the regions far away from the fracture, but
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47

Yang, Chang Yong, Yu Can Fu, Da Shun Huang, Jiu Hua Xu, Neng Ge Yang, and Wen Yan. "Surface Roughness and Topography of Honed Nickel-Based Superalloy." Advanced Materials Research 1136 (January 2016): 478–83. http://dx.doi.org/10.4028/www.scientific.net/amr.1136.478.

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Honing experiments were carried out for nickel-based superalloy Inconel718 bore. The significance analysis of the four honing parameters: spindle speed, stroke speed, wedge feed per stroke cycle and grain size on the surface roughness, was studied with the orthogonal design method. And the significant degree under the rated conditions was determined. The results showed that: wedge feed per stroke cycle and grain size have a significant influence on surface roughness while spindle speed and stroke speed had no significant effect. Also, there was a positive correlation between surface roughness
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48

Peng, Rui Tao, Fang Lu, Xin Zi Tang, and Yuan Qiang Tan. "Residual Stresses in Prestressed Turning of Nickel-Based Superalloy." Applied Mechanics and Materials 271-272 (December 2012): 242–46. http://dx.doi.org/10.4028/www.scientific.net/amm.271-272.242.

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Aiming to get appropriate residual compressive stress distribution on machined surface just in the machining process, the technique of prestressed cutting is applied for nickel-based superalloy shafts. This article studies theoretically and experimentally the effect of prestress on the residual stress in the machined surface layer. Prestressed turning tests under the conditions of different prestress, cutting speed, depth of cut and feed rate were carried out, residual stresses were determined via an X-ray diffraction technique. Theoretical result demonstrates that higher prestress leads to mo
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49

Nowotnik, Andrzej, Paweł Rokicki, Paweł Pędrak, Slawomir Kotowski, Jan Sieniawski, and Grazyna Mrówka-Nowotnik. "Mechanical Aspects of Plastic Deformation of Nickel Based Superalloy." Key Engineering Materials 592-593 (November 2013): 724–27. http://dx.doi.org/10.4028/www.scientific.net/kem.592-593.724.

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Variations of a true stress vs. true strain illustrate behaviour of materials during plastic deformation. Stress-strain relationship is generally evaluated by a torsion, compression and tensile tests. Results of these tests provide crucial information pertaining to the stress values which are necessary to run deformation process at specified temperature and cooling rate. Uniaxial compression tests at temperatures below the γ solvus were conducted on nickel based superalloy CMSX-4, to study the effect of temperature and strain rate on its flow stress. On the basis of received flow stress values
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50

Ahn, Kwanghyun, and Hoon Huh. "Dynamic Hardening Equation of Nickel-Based Superalloy Inconel 718." Key Engineering Materials 535-536 (January 2013): 129–32. http://dx.doi.org/10.4028/www.scientific.net/kem.535-536.129.

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The dynamic response of the turbine blade materials is indispensable for analysis of erosions of turbine blades as a result of impulsive loading associated with gas flow. This paper is concerned with the dynamic hardening equation of the Nickel-based superalloy Inconel 718 which is widely used in the high speed turbine blade. Reported representative dynamic hardening equations have been constructed and evaluated using the dynamic hardening characteristics of the Inconel 718. Dynamic hardening characteristics of the Inconel 718 have been obtained by uniaxial tensile tests and SHPB tests. Uniaxi
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