航空材料学报
航空材料學報
항공재료학보
JOURNAL OF AERONAUTICAL MATERIALS
2010年
1期
26-29
,共4页
张家锋%邹金文%康进武%柳百成
張傢鋒%鄒金文%康進武%柳百成
장가봉%추금문%강진무%류백성
粉末高温合金涡轮盘%热处理%界面换热系数%数值模拟
粉末高溫閤金渦輪盤%熱處理%界麵換熱繫數%數值模擬
분말고온합금와륜반%열처리%계면환열계수%수치모의
P/M superalloy disk%heat-treatment%surface heat transfer coefficients%numerical simulation
以试验方法研究了FGH96粉末高温合金涡轮盘在空冷、风冷和油淬等条件下的表面换热行为,进而反算求解得到了界面换热系数,并将其应用到实际盘件热处理过程的数值模拟当中.结果表明,油淬条件下的界面换热系数远大于其他两种冷却方式,其最大值约为空冷换热系数最大值的10倍.现有工艺适合文中涡轮盘的热处理,淬火应力低于材料对应温度的屈服强度.
以試驗方法研究瞭FGH96粉末高溫閤金渦輪盤在空冷、風冷和油淬等條件下的錶麵換熱行為,進而反算求解得到瞭界麵換熱繫數,併將其應用到實際盤件熱處理過程的數值模擬噹中.結果錶明,油淬條件下的界麵換熱繫數遠大于其他兩種冷卻方式,其最大值約為空冷換熱繫數最大值的10倍.現有工藝適閤文中渦輪盤的熱處理,淬火應力低于材料對應溫度的屈服彊度.
이시험방법연구료FGH96분말고온합금와륜반재공랭、풍랭화유쉬등조건하적표면환열행위,진이반산구해득도료계면환열계수,병장기응용도실제반건열처리과정적수치모의당중.결과표명,유쉬조건하적계면환열계수원대우기타량충냉각방식,기최대치약위공랭환열계수최대치적10배.현유공예괄합문중와륜반적열처리,쉬화응력저우재료대응온도적굴복강도.
Heat extraction behaviors of a FGH96 P/M superalloy disk under static air cooling, forced air cooling and oil quenching conditions were studied by experiments and the surface heat transfer coefficients were obtained by solving the inverse thermal problems. Numerical simulation of the heat-treatment process of a real disk was then carried out. The results showed that the heat extraction rates of oil quenching were much higher than those in the other two conditions, and the peak value was almost 10 times of that in the static air cooling. The heat-treatment process was appropriate as the stress generated in the quenching process was lower than the yield strength of the disk material.