机械工程学报
機械工程學報
궤계공정학보
Journal of Mechanical Engineering
2015年
18期
71-82
,共12页
赵荣国%刘亚风%蒋永洲%李其棒%言怡%刘学晖
趙榮國%劉亞風%蔣永洲%李其棒%言怡%劉學暉
조영국%류아풍%장영주%리기봉%언이%류학휘
涡轮盘%疲劳裂纹扩展%寿命预测%概率%应力比
渦輪盤%疲勞裂紋擴展%壽命預測%概率%應力比
와륜반%피로렬문확전%수명예측%개솔%응력비
turbine disk%fatigue crack propagation%life prediction%probability%stress ratio
镍基高温合金的概率寿命预测要求模拟多种复杂随机现象。针对室温下航空发动机涡轮盘用GH4133B 合金的疲劳裂纹扩展试验数据,采用Paris公式和含门槛值?Kth的修正Paris公式,对不同应力比下的疲劳裂纹扩展速率进行概率预测。基于Paris公式和修正Paris公式的积分式计算不同存活概率P下的理论疲劳剩余寿命Nfp,并与试验疲劳剩余寿命Nft对比。结果表明,当P=50%时,基于修正Paris公式的Nfp与Nft吻合;当P=90%时,基于Paris公式和修正Paris公式的Nfp均与Nft吻合;当P=99%时,基于修正Paris公式的Nfp具有高可靠度。基于疲劳寿命试验数据的非线性回归分析绘制Nf-Fp,m-Fp,a曲面,引入参量γ表征平均载荷Fp,m和载荷幅值Fp,a对疲劳寿命Nf的影响,结果表明,在所研究的应力比范围内Fp,m对Nf影响大。
鎳基高溫閤金的概率壽命預測要求模擬多種複雜隨機現象。針對室溫下航空髮動機渦輪盤用GH4133B 閤金的疲勞裂紋擴展試驗數據,採用Paris公式和含門檻值?Kth的脩正Paris公式,對不同應力比下的疲勞裂紋擴展速率進行概率預測。基于Paris公式和脩正Paris公式的積分式計算不同存活概率P下的理論疲勞剩餘壽命Nfp,併與試驗疲勞剩餘壽命Nft對比。結果錶明,噹P=50%時,基于脩正Paris公式的Nfp與Nft吻閤;噹P=90%時,基于Paris公式和脩正Paris公式的Nfp均與Nft吻閤;噹P=99%時,基于脩正Paris公式的Nfp具有高可靠度。基于疲勞壽命試驗數據的非線性迴歸分析繪製Nf-Fp,m-Fp,a麯麵,引入參量γ錶徵平均載荷Fp,m和載荷幅值Fp,a對疲勞壽命Nf的影響,結果錶明,在所研究的應力比範圍內Fp,m對Nf影響大。
얼기고온합금적개솔수명예측요구모의다충복잡수궤현상。침대실온하항공발동궤와륜반용GH4133B 합금적피로렬문확전시험수거,채용Paris공식화함문함치?Kth적수정Paris공식,대불동응력비하적피로렬문확전속솔진행개솔예측。기우Paris공식화수정Paris공식적적분식계산불동존활개솔P하적이론피로잉여수명Nfp,병여시험피로잉여수명Nft대비。결과표명,당P=50%시,기우수정Paris공식적Nfp여Nft문합;당P=90%시,기우Paris공식화수정Paris공식적Nfp균여Nft문합;당P=99%시,기우수정Paris공식적Nfp구유고가고도。기우피로수명시험수거적비선성회귀분석회제Nf-Fp,m-Fp,a곡면,인입삼량γ표정평균재하Fp,m화재하폭치Fp,a대피로수명Nf적영향,결과표명,재소연구적응력비범위내Fp,m대Nf영향대。
Probabilistic life prediction of nickel-base superalloy requires the modelling multiple complex random phenomena. The fatigue crack growth rates at various stress ratios are probabilistically predicted using the Paris formula and the modified Paris formula with threshold value?Kth for fatigue crack growth test data of GH4133B superalloy used in turbine disk of aero-engine at room temperature. The theoretic fatigue crack growth livesNfp at various survival probabilitiesP predicted by integral based on the Paris formula and the modified Paris formula are calculated and compared with the test onesNft. It is shown thatNfp obtained by integral based on the modified Paris formula is well fitted withNft atP=50%, while bothNfp obtained by integral based on the Paris formula and that obtained by integral based on the modified Paris formula are all well fitted withNft atP=90%, andNfp obtained by integral based on the modified Paris formula possesses a high reliability atP=99%. A 3DNf-Fp,m-Fp,a fatigue life surface are plotted based on the nonlinear regression analysis of fatigue life test data, and a parameterγ is introduced to characterize the effect of mean loadFp,m and load amplitudeFp,a on fatigue lifeNf. It is suggested that the effect ofFp,m on Nf is larger than that ofFp,a on Nf.