昆明理工大学学报(自然科学版)
昆明理工大學學報(自然科學版)
곤명리공대학학보(자연과학판)
JOURNAL OF KUNMING UNIVERSITY OF SCIENCE AND TECHNOLOGY(SCIENCE AND TECHNOLOGY)
2013年
6期
43-47
,共5页
伍曾%李洁青%黄伟%陶忠
伍曾%李潔青%黃偉%陶忠
오증%리길청%황위%도충
扣件%弹条%非线性接触理论%微动磨损%疲劳%断裂
釦件%彈條%非線性接觸理論%微動磨損%疲勞%斷裂
구건%탄조%비선성접촉이론%미동마손%피로%단렬
fastener%elastic bar%non-linear contact theory%fretting wear%fatigue%fracture
弹条是实现弹条II型扣件功能的主要元件,传统的疲劳分析方法主要从弹条的应力、应变入手,这并不能反映真实情况,因为弹条在工作中与其它构件接触面表面之间存在微小的相互移动,即微动。应用非线性接触理论,采用库仑摩擦模型模拟弹条与周围接触元件之间的摩擦接触情况,计算出弹条各点的剪切应力τ、相对位移δ及二者乘积τ·δ的值;并采用离散裂缝模型来模拟扣件裂纹的生成及扩展。理论分析表明,若微动磨损在弹条疲劳断裂过程中起主要作用,则断口处应位于弹条中τ·δ值最大的点附件。扣件疲劳试验表明,弹条断口处位于弹条尾部与轨距挡板接触处,处于τ及τ·δ最大的点之间且更靠近τ·δ值最大的点。弹条尾部与轨距挡板之间由于微动磨损产生裂纹,形成污染源,反复作用下,裂纹扩展,最终导致弹条断裂。试验证明了弹条微动磨损理论分析的正确性,为改进弹条设计,提高其疲劳寿命提供科学依据。
彈條是實現彈條II型釦件功能的主要元件,傳統的疲勞分析方法主要從彈條的應力、應變入手,這併不能反映真實情況,因為彈條在工作中與其它構件接觸麵錶麵之間存在微小的相互移動,即微動。應用非線性接觸理論,採用庫崙摩抆模型模擬彈條與週圍接觸元件之間的摩抆接觸情況,計算齣彈條各點的剪切應力τ、相對位移δ及二者乘積τ·δ的值;併採用離散裂縫模型來模擬釦件裂紋的生成及擴展。理論分析錶明,若微動磨損在彈條疲勞斷裂過程中起主要作用,則斷口處應位于彈條中τ·δ值最大的點附件。釦件疲勞試驗錶明,彈條斷口處位于彈條尾部與軌距擋闆接觸處,處于τ及τ·δ最大的點之間且更靠近τ·δ值最大的點。彈條尾部與軌距擋闆之間由于微動磨損產生裂紋,形成汙染源,反複作用下,裂紋擴展,最終導緻彈條斷裂。試驗證明瞭彈條微動磨損理論分析的正確性,為改進彈條設計,提高其疲勞壽命提供科學依據。
탄조시실현탄조II형구건공능적주요원건,전통적피로분석방법주요종탄조적응력、응변입수,저병불능반영진실정황,인위탄조재공작중여기타구건접촉면표면지간존재미소적상호이동,즉미동。응용비선성접촉이론,채용고륜마찰모형모의탄조여주위접촉원건지간적마찰접촉정황,계산출탄조각점적전절응력τ、상대위이δ급이자승적τ·δ적치;병채용리산렬봉모형래모의구건렬문적생성급확전。이론분석표명,약미동마손재탄조피로단렬과정중기주요작용,칙단구처응위우탄조중τ·δ치최대적점부건。구건피로시험표명,탄조단구처위우탄조미부여궤거당판접촉처,처우τ급τ·δ최대적점지간차경고근τ·δ치최대적점。탄조미부여궤거당판지간유우미동마손산생렬문,형성오염원,반복작용하,렬문확전,최종도치탄조단렬。시험증명료탄조미동마손이론분석적정학성,위개진탄조설계,제고기피로수명제공과학의거。
The function of type II fastener is mainly achieved by the elastic bar.The traditional methods for the study of fatigue dealing with stress or strain do not reflect the true situation because the contact surface between the elastic bar at work and other with other components leads to tiny mutual movement,namely fretting.The shear stress(τ),relative displacement(δ)and the product of them(τ·δ)of the elastic bar are calculated by application of the nonlinear contact theory and the Coulomb friction model.A discrete crack model is then used to simulate the fastener crack generation and propagation.It is shown through theoretical analysis that the fatigue fracture should be located in a section close to the maximum value of the τ·δif the fretting wear plays a major role.Fastener fatigue tests indicate that,a fracture is found at the tail of elastic bar and baffle contact,which is between points of theτvalue and the maximumτ·δvalue,while being a little closer to the latter one.The fret-ting wear between the tail elastic bar and baffle results in cracks,which are then propagated repeatedly and leads to the eventual fracture.The correctness of the fretting wear theory is proved by the experiment,which provides scientific basis for improving the fastener design and enhancing its wearability.