Directionally solidified (DS) nickel-base superalloys are widely used for turbine blades in aircraft engines and industrial gas turbines. The surface recrystallization, detrimental to mechanical properties of DS superalloys, is an influencing factor in the engineering failures. [1][2][3][4] For conventional polycrystalline metals, recrystallization is an effective approach to optimizing microstructure and thus to improving mechanical property, such as grain refining and strength improving. Industrially, the static recrystallization temperature is at which the metal with 70 % cold deformation mostly accomplishs its recrystallization course in one hour. The dynamic recrystallization refers to the recrystallization process during the hot working operation which temperature is higher than the static recrystallization one. [4] However, for DS superalloy, aim of recrystallization researches is to provide effective measures to reduce or even supress surface recrystallization of DS components. When DS components are deformed by the improper operations such as severe grit-blating or polisihing and subsequently heated above the static recrystallization temperature, the static recrystallization occurs. [5][6][7][8] The static recrystallization temperature of DS nickel-base superalloy, dominated by the solution behavior of gamma prime (c′), is close to the dissolution temperature of c′ and about 0.8 ∼ 0.9 times the absolute melting temperature. [9][10] In addition, DS components may be dynamically recrystallized because of the rigorous service conditions even if the operation temperature is slightly lower than that of the static recrystallization.Little information has been available in the open literature on the dynamic recrystallization of DS superalloys, especially on the dynamic recrystallization mechanism. [11][12][13][14] This paper investigates the dynamic recrystallization behavior of a DS nickel-base superalloy. The main purpose is to find out the dynamic recrystallization mechanism and thus to provide measures against the dynamic recrystallization of DS components.
Experimental Details
MaterialThe alloy investigated was produced by directional solidification and the longitudinal axis was in the [001] direction with not more than 10°deviation. The nominal chemical composition in weight percentage was as follows: C 0.14, Cr 9.5, Co 6.0, W 5.3, Mo 3.8, Al 6.0, Ti 1.8, B 0.02, and balance Ni. The DS nickel-base superalloy was treated by solution (1220°C/4 h, air cool) and subsequent aging (870°C/32 h, air cool). In the heattreated state, the superalloy had a uniform fine cuboidal c′ precipitate, typically 0.1 lm ∼ 0.15 lm in size and approximately 0.6 vol. fraction. The static recrystallization temperature of this superalloy is above 1000°C. [15] Testing ProcedureFull size creep specimens with the gage portion of 52 mm in length and 10 mm in diameter were machined from the DS superalloy. Tensile creep tests were carried out using the single lever type creep machine at three temperatures, i.e. 800°C, 850°C and 900°C und...