金属学报
金屬學報
금속학보
ACTA METALLURGICA SINICA
2009年
10期
1242-1248
,共7页
Inconel 718合金%晶粒长大模型%粗轧加热%等温条件%非等温条件
Inconel 718閤金%晶粒長大模型%粗軋加熱%等溫條件%非等溫條件
Inconel 718합금%정립장대모형%조알가열%등온조건%비등온조건
Inconel 718 alloy%grain growth model%reheating prior to rough rolling%isothermal condition%non-isothermal condition
以Inconel 718合金锻坯为研究对象,在1173-1423 K的温度范围内,研究了加热温度和时间对Inconel 718合金锻坯晶粒尺寸变化的影响,推导并验证了具有普适意义的适合Inconel 718合金锻坯粗轧加热过程的晶粒长大模型.研究结果表明:随加热时间的延长,在1173 K加热时,晶粒尺寸变化不显著;1173-1323 K加热时,晶粒尺寸呈线性长大;高于1323 K加热时,晶粒尺寸呈抛物线性长大.所建立的Inconel 718合金的晶粒长大模型适用于等温条件和非等温条件下晶粒尺寸演变的计算.
以Inconel 718閤金鍛坯為研究對象,在1173-1423 K的溫度範圍內,研究瞭加熱溫度和時間對Inconel 718閤金鍛坯晶粒呎吋變化的影響,推導併驗證瞭具有普適意義的適閤Inconel 718閤金鍛坯粗軋加熱過程的晶粒長大模型.研究結果錶明:隨加熱時間的延長,在1173 K加熱時,晶粒呎吋變化不顯著;1173-1323 K加熱時,晶粒呎吋呈線性長大;高于1323 K加熱時,晶粒呎吋呈拋物線性長大.所建立的Inconel 718閤金的晶粒長大模型適用于等溫條件和非等溫條件下晶粒呎吋縯變的計算.
이Inconel 718합금단배위연구대상,재1173-1423 K적온도범위내,연구료가열온도화시간대Inconel 718합금단배정립척촌변화적영향,추도병험증료구유보괄의의적괄합Inconel 718합금단배조알가열과정적정립장대모형.연구결과표명:수가열시간적연장,재1173 K가열시,정립척촌변화불현저;1173-1323 K가열시,정립척촌정선성장대;고우1323 K가열시,정립척촌정포물선성장대.소건립적Inconel 718합금적정립장대모형괄용우등온조건화비등온조건하정립척촌연변적계산.
The Inconel 718 superalloy is extensively used to manufacture critical parts in aero-nautical, astronautical, oil and chemical industries due to its excellent mechanical, physical and anti-corrosion behavior. Usually, these parts are shaped by hot forging or rolling in open-train mills. Recently, the tandem hot rolling has been applied to form superalloy bar products. In some cases, it can replace the traditional rolling, since it has higher productivity and product quality. In order to obtain the most favorable microstructure and the best mechanical properties of Inconel 718 alloy in tandem hot rolling, it is necessary to control its microstructural evolution in every step of the whole rolling process. With the aid of computer modeling, it is possible to make such a controlling process possible. As the first step in tandem hot rolling, reheating process of a forged slab prior to rough rolling plays a predominant role in predicting the grain size change or even the microstructural evo-lution. Thus, in this study, an Inconel 718 alloy forged slab was used as the experimental material and the effects of reheating temperature and holding time on its grain growth were investigated. A universal model was developed and verified for the grain growth of Inconel 718 alloy forged slab in reheating process prior to rough rolling. With the increase of holding time, the grain size shows no remarkable change up to 1173 K. The grain growth presents a linear trend in the range from 1173 to 1323 K. A parabolic trend of grain growth can be observed when reheating temperature is higher than 1323 K. The established grain growth model of Inconel 718 alloy would be suitable to calculate the grain size evolution under the both isothermal and non-isothermal reheating conditions. This could also provide a basis in formulating the technological parameters for tandem hot rolling of Inconel 718 superalloy.