航空科学技术
航空科學技術
항공과학기술
AERONAUTICAL SCIENCE AND TECHNOLOGY
2014年
7期
68-72
,共5页
赵凯%何玉怀%刘新灵%陶春虎
趙凱%何玉懷%劉新靈%陶春虎
조개%하옥부%류신령%도춘호
50CrVA弹簧钢%比例加载%冲击载荷%多轴疲劳
50CrVA彈簧鋼%比例加載%遲擊載荷%多軸疲勞
50CrVA탄황강%비례가재%충격재하%다축피로
50CrVA spring steel%proportional loading%impact load%multiaxial fatigue
本文用MTS 809拉-扭电液伺服材料试验机研究了50CrVA弹簧钢标准试样在冲击载荷下的多轴疲劳寿命,对试样的断口进行了宏微观观察。研究结果表明:冲击载荷会明显降低试样的寿命;试样的寿命随轴向拉力的增大而减小;宏观损伤方面,试样整个断口可见稳定扩展区、快速扩展区和瞬断区;稳定扩展区面积较小,快速扩展区磨损严重;与源区对侧存在一台阶,台阶与源区正对的位置存在一偏转角;台阶附近区域未出现明显的磨损,为瞬断区;微观损伤方面,裂纹源萌生于试样表面,稳定扩展区疲劳条带不明显,快速扩展区以剪切拉长韧窝和磨损形貌为主。
本文用MTS 809拉-扭電液伺服材料試驗機研究瞭50CrVA彈簧鋼標準試樣在遲擊載荷下的多軸疲勞壽命,對試樣的斷口進行瞭宏微觀觀察。研究結果錶明:遲擊載荷會明顯降低試樣的壽命;試樣的壽命隨軸嚮拉力的增大而減小;宏觀損傷方麵,試樣整箇斷口可見穩定擴展區、快速擴展區和瞬斷區;穩定擴展區麵積較小,快速擴展區磨損嚴重;與源區對側存在一檯階,檯階與源區正對的位置存在一偏轉角;檯階附近區域未齣現明顯的磨損,為瞬斷區;微觀損傷方麵,裂紋源萌生于試樣錶麵,穩定擴展區疲勞條帶不明顯,快速擴展區以剪切拉長韌窩和磨損形貌為主。
본문용MTS 809랍-뉴전액사복재료시험궤연구료50CrVA탄황강표준시양재충격재하하적다축피로수명,대시양적단구진행료굉미관관찰。연구결과표명:충격재하회명현강저시양적수명;시양적수명수축향랍력적증대이감소;굉관손상방면,시양정개단구가견은정확전구、쾌속확전구화순단구;은정확전구면적교소,쾌속확전구마손엄중;여원구대측존재일태계,태계여원구정대적위치존재일편전각;태계부근구역미출현명현적마손,위순단구;미관손상방면,렬문원맹생우시양표면,은정확전구피로조대불명현,쾌속확전구이전절랍장인와화마손형모위주。
Multiaxial fatigue life of 50CrVA spring steel standard specimens under impact loading was studied with MTS 809 tension-torsion electro-hydraulic servo tester. The results show that impact loading can obviously reduce the specimens’ life. Specimens’ life decreases with the increasing of axial tension. In macroscopic damage aspect, slow, fast propagation and ifnal fracture zone can be observed throughout the specimen’s fracture. The area of slow propagation zone was small and fast propagation zone was worn badly. A step exits opposite the source, which is the ifnal fracture zone. There is a one-sided corner between step and the opposition of the source region. In microscopic damage aspect, fatigue sources initiate at the surface and fatigue stripes can’t be found easily on the slow propagation zone. Elongated dimples and wear are the main characteristics for the fast propagation zone.