铌对镍基合金蠕变性能的影响

研究了Nb对Ni基合金高温蠕变性能的影响，认为Nb主要是通过增强第二组γ’相沉淀强化，γ相固溶强化，晶界M23C6呈链状分布，而使Ni基合金抗蠕变性能提高。     

锰对ZA27合金压蠕变行为的影响

采用自制的实验装置研究了锰对 ZA2 7合金在常温及高温时的压蠕变行为的影响。研究表明 ,在所试验的温度为 2 0℃到 16 0℃和压应力为 5 0 MPa到 137.5 MPa的范围内 ,加入锰的合金 ZA2 7- Mn和未加锰的 ZA2 7合金的压蠕变量均随着温度和应力的升高而增大 ,ZA2 7- Mn合金的压蠕变速率小于 ZA2 7合金的压蠕变速率。加入锰后 ,合金在压蠕变过程中的负蠕变量及出现负蠕变的温度和应力范围增大。两种合金的稳态蠕变速率均符合于半经验公式 εs=Aσnexp(- Qa/RT)。但在不同的温度 ,ZA2 7- Mn合金的应力指数 n和表观激活能 Qa 均大于 ZA2 7合金的应力指数和表观激活能 ,而 ZA2 7- Mn合金的材料结构常数 A为 1.5 4× 10 - 4,低于 ZA2 7合金的材料结构常数 A(0 .0 0 2 )。两种合金的稳态蠕变速率均是由锌的点阵自扩散和位错的攀移所控制。     

热带粗轧机组立轧稳定轧制变形规律的实验研究和有限元分析

本文采用铅作为模拟材料，对热带粗轧机组平辊立轧变形规律进行了实验研究，得到了表征立轧稳定轧制阶段时轧件断面特征的四个参量与侧压量、立辊直径、板坯来料厚度及宽度之间的关系。并首次提出用超薄单元近似处理奇异点的新方法，采用全三维刚塑性可压缩有限元法对立轧稳态过程进行了理论解析，所得结果和实验结果符合较好。     

Mechanical properties and potential applications of magnesium alloys

1　INTRODUCTIONDuringthefirsthalfofthetwentiethcentury ,magnesiumalloyswereusedextensivelyincivilianandmilitaryaircraftcomponents.TheneglectofmagnesiumalloysafterworldwarⅡwasrepresentedbytheslumpoftheproductionfrom 2 2 8.8kt/ain194 4to 10kt/aafterWorldWarⅡ .Themostsig nificantapplicationofmagnesiumalloysinthesecondhalfofthetwentiethcenturywasinproductionofair cooledenginesandgearboxesforVolkswagenBeetle ,whichledtheautomobileindustrytomakeavolun tarycommitmenttoachieve 30 %CO2 emissio…     

Development of design principles for a creep-limited alloy for turbine blades

Recent advancements in turbine-blade materials engineering are reviewed in light of general superalloy research and the author’s work on a new powder metallurgy IN-792 creep-limited alloy for application in blades of gas-turbine engines. The developed set of principles presented in this paper incorporates all the factors that must be taken into consideration in selecting and designing an alloy for turbine blades.     

A kinetics formulation for low-temperature plasticity

The mechanism of low-temperature plastic deformation is controlled by thermally activated dislocation movements. An evolutionary constitutive law based on the principles of deformation kinetics is described in this article. The constitutive law is expressed with a sinh function designed for computational efficiency. It is derived from rigorously defined kinetics principles. The approximation involved in the sinh function is defined so that in applications an exact evaluation can be made of the validity limits. The system of the constitutive law and the external constraints lead to the operational equations. Applications are developed for constant strain-rate loading, constant stress-rate loading, stress relaxation, creep, and ratchetting processes. The analysis provides a unified treatment for low-temperature plastic deformation.     

RELATIONSHIP BETWEEN CREEP PROPERTIES AND STRUCTURE OF STEEL 20Cr11MoVNbNB

Studies were made of the creep properties and structure change of steet 20Cr11MoVNbNB at550-650℃.It is found that at 550℃ when creep stress>180 MPa there exists linear rela-tion with two different slopes β_1 and β-2 between transitional creep strain ε_β and creeptime t~(1/3),and β_1(in initiol period)>β_2(in later period).The Creep rate of stable stage at550℃ can be expressed by =Aσ exp(-Q_ /RT),where,n=4.7.A exp(-Q_ /RT)=5.37×10~(-16).Apparent creep activation energy Q_ =430 kJ/mol at 550-650℃,which ismuch higher than the self-diffusion activation energy of atoms for matrix Fe.In creepprocess,as the creep stress and time increase,the total weight of precipitated phases and rela-tive weight of Cr,Mo and V increase,but those of Fe and Nb decrease in precipitated phases,     

某航空发动机第三级涡轮叶片失效分析

本文对某型号航空发动机GH4033第三级涡轮叶片榫头裂纹及断裂失效进行了分析,确定了失效模式为两类,第一类为蠕变疲劳裂纹,第二类为起始应力较大的高低周复合疲劳断裂.研究发现GH4033合金屈服强度偏低、晶界强化能力不足是叶片发生蠕变疲劳开裂的主要原因.而叶片的高低周复合疲劳断裂则主要与个别相邻叶片的叶冠间隙偏大引发的高振动弯曲应力及R处加工刀痕引发的应力集中有关.最后提出了预防叶片发生该类失效的措施.     

Evaluation of high- temperature behavior of CMSX4 + yttrium single- crystal nickel- base superalloy

CMSX4 + Y, a highly strengthened rhenium-containing second-generation single-crystal nickel-base su-peralloy, has been studied by creep, low-cycle, and thermomechanical fatigue in the temperature range 500 to 1100 °C. The alloy exhibits good high-temperature mechanical properties that are superior or com-parable to other single-crystal superalloys. Thermomechanical fatigue resistance is equivalent to low-cy-cle fatigue and is cycle-shape dependent. High-temperature mechanical properties have been studied using life prediction relationships that are frequently used for creep and low-cycle fatigue data evalu-ation. Examination of fracture surfaces revealed that fracture induced by creep damage is internal and starts from pore-initiated cracks; however, fatigue damage starts on the external surface and propagates inward in stage II mode.