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Acta Metall Sin  2019, Vol. 55 Issue (5): 619-626    DOI: 10.11900/0412.1961.2018.00426
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Dendrite Growth and Orientation Evolution in the Platform of Simplified Turbine Blade for Nickel-Based Single Crystal Superalloys
Dejian SUN,Lin LIU(),Taiwen HUANG,Jiachen ZHANG,Kaili CAO,Jun ZHANG,Haijun SU,Hengzhi FU
1. State Key Laborotory of Solidification Processing, Northwestern Polytechnical University, Xi'an 710072, China
Cite this article: 

Dejian SUN,Lin LIU,Taiwen HUANG,Jiachen ZHANG,Kaili CAO,Jun ZHANG,Haijun SU,Hengzhi FU. Dendrite Growth and Orientation Evolution in the Platform of Simplified Turbine Blade for Nickel-Based Single Crystal Superalloys. Acta Metall Sin, 2019, 55(5): 619-626.

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Abstract  

Ni-based single crystal (SX) superalloys are widely used in key hot section parts of advanced aero engine and industrial gas turbines (IGTs) because of their superior mechanical performance at high temperature. During directional solidification process of SX blades, high angle grain boundaries that degrade the creep and fatigue properties significantly might be highly likely to occur in the platform region, thus the analysis of multi-influencing factors, such as platform dimension, withdrawal rate and seed orientation, need to be studied. However, most of these works are conducted from the perspective of heterogeneous nucleation induced by the extreme concave shape of liquid-solid interface, and there is rare report concerning that whether dendrite deformation could also induce the high angle grain boundaries. Therefore, in the present work, the SX castings with three platforms were directionally solidified in a Bridgman-furnace, to investigate dendrite growth and the associated orientation evolution. It was observed that the whole platform consisted of three types of regions: blade body, secondary dendrite spread zone, and the "circuit-like" dendrite growth zone. The convergent boundaries of dendrite arms (CBDAs) were formed between secondary dendrite spread zone and the "circuit-like" dendrite growth zone. With increasing withdrawal rate, the area of "circuit-like" dendrite growth zone was increased, and the area of secondary dendrite spread zone was reduced. Moreover, the monotonically increased misorientation angle along CBDAs as a result of the dendrite deformation around platform edge was identified. As withdrawal rate increased, the misorientation angle along CBDAs was increased, and thus the tendency of high angle grain boundary formation on the CBDAs was enhanced. Unlike the nearly constant misorientation angle of the high angle grain boundary between grains and the low angle grain boundary between subgrains, the misorientation angle of the high angle grain boundary and low angle grain boundary formed on the CBDAs varied regularly.

Key words:  single crystal superalloy      dendrite growth      dendrite deformation      orientation evolution      high angle grain boundary     
Received:  10 September 2018     
ZTFLH:  TG21  
Fund: National Natural Science Foundation of China(51331005);National Natural Science Foundation of China(51631008);National Natural Science Foundation of China(51690163);National Natural Science Foundation of China(51771148);National Key Research and Development Program of China(2016YFB0701400);National Key Research and Development Program of China(2017YFB0702900)

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https://www.ams.org.cn/EN/10.11900/0412.1961.2018.00426     OR     https://www.ams.org.cn/EN/Y2019/V55/I5/619

Fig.1  Geometric model of simplified turbine blade (a) and the configuration and dimension of platform 3 (b)
Fig.2  Dendritic morphologies within the platform base of platform 3 (a) and magnified images of positions 1~6 in Fig.2a (b~g) with the withdrawal rate of 9 mm/min (LSDA—long secondary dendrite arm, LTDA—long tertiary dendrite arm, CBDA—convergent boundary of dendrite arms, SDZ—secondary dendrite spread zone, CZ—"circuit-like" dendrite growth zone. 2A, 3A, 4A—secondary, tertiary and quaternary dendrite arms, respectively. The yellow dotted line represents the boundaries between blade body zone and platform zone)Color online
Fig.3  Dendritic morphologies within one half of the platform base of platform 3 when the withdrawal rates are 6 mm/min (a), 3 mm/min (b) and 1.2 mm/min (c) (The yellow dotted lines represent the boundaries between blade body zone and platform zone)Color online
Fig.4  Evolution of thermal profile within one half of the platform base of platform 3 when the withdrawal rates are 9 mm/min (a~c), 6 mm/min (d), 3 mm/min (e) and 1.2 mm/min (f) (T—temperature, Tliq—liquidus temperature, Tsol—solidus temperature)Color online
Fig.5  Misorientation evolutions along CBDA within the platform base of platform 3 when the withdrawal rate is 9 mm/min (Orientations of dendrite arms located in the upside of CBDA are given in blue circles and those in the downside of CBDA are given in red circles)Color online
Fig.6  Dendritic morphologies of regions 1~3 in Fig.3b (a~c) and corresponding misorientation evolutions (d) along CBDA within the platform base of platform 3 when the withdrawal rate is 3 mm/min (The black dashed lines represent CBDA. Orientations of dendrite arms located in the upside of CBDA are given in blue circles and those in the downside of CBDA are given in red circles)Color online
Fig.7  Schematic of the evolution of misorientation angle (φ1~φ4) along CBDA and its relation between the dendrite deformation of LSDA and LTDAColor online
Fig.8  Temperature (a) and displacement (d) (b) contours within the platform base at a given instant of time (1301 s) when the withdrawal rate is 9 mm/minColor online
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