FGH95-DZ22双合金的热等静压复合工艺

研究了采用热等静压扩散连接工艺实现FGH95高温合金粉末和DZ22定向合金之间可靠连接的可行性.研究内容包括热等静压复合工艺对FGH95-DZ22复合界面的成分扩散、界面组织以及叶片材料本身组织和性能的影响.研究表明,通过合理地选择与改进工艺,可以在保证对偶材料性能满足要求的前提下实现界面的良好扩散与结合.     

镍基双合金扩散偶的拉伸性能研究

采用热等静压(HIP)扩散连接工艺,获得了镍基单晶高温合金与粉末高温合金的扩散偶。研究了热等静压和热处理工艺对扩散偶的组织和拉伸性能的影响。结果表明,不同温度热等静压的扩散偶均实现了冶金结合,瞬时拉伸断口位置处于DD402侧,断裂面为{111}滑移面。随着HIP温度升高,DD402母材的γ′相粒子粗化,FGH95粉末合金母材的再结晶晶粒长大;1 166℃HIP扩散偶热处理后,FGH95粉末合金的γ′相由晶界大尺寸γ′相、晶粒内中等尺寸的和细小的γ′相组成。扩散偶试样的650℃抗拉强度受HIP温度影响小,而屈服强度随着HIP温度升高而降低。     

镍基高温合金HIP扩散连接的组织和性能

 采用热等静压扩散连接工艺,获得了DD402单晶合金与FGH95合金的扩散偶。研究了热等静压温度对扩散偶的持久性能、组织结构的影响。结果表明,不同温度热等静压的扩散偶均实现了冶金结合;结合界面区形成了一个组织过渡区,DD402单晶合金中的γ′ 相粒子在HIP过程中发生了筏形化;热处理后结合界面区的γ′ 相形貌和尺寸未发生明显变化。1166℃热等静压扩散偶的650℃持久性能偏低,断口在DD402单晶合金侧,断裂面从结合界面区的大尺寸γ′ 相起始,沿{111}滑移面向筏形γ′ 相区扩展。     

FGH95镍基粉末高温合金热等静压工艺的研究和发展

在借鉴国外相关研究成果的基础上,对FGH95合金的热等静压工艺参数进行了具体的实验研究,分析了FGH95合金热等静压工艺中存在的问题,研究了不同成形工艺对合金力学性能的影响,指出了FGH95合金热等静压工艺研究的发展方向.     

硬质合金与铁基复合材料热等静压扩散连接

以烧结结态硬质合金和粉末态铁基复合材料为连接对象，研究了两种材料的热等静压扩攻连接工艺，获得了直接连接接头和加镍作中间过渡层的间接连接接头，考察了接头的结合界面形貌，界面的元素扩散和界面结合强度。     

热等静压烧结—连接法制取硬质合金／钢复合材料初探

用热等静压烧结－连接法获得了ＹＧ１５Ｃ与４５＃钢的复合接头，考察了接头的界面复合特征，界面上元素扩散及接头的结合强度，分析了ＹＧ１５Ｃ与４５＃钢的热等静压烧结－连接机制。     

金属材料的热等静压扩散连接

简单介绍了热等静压扩散连接的概念及工艺,以及某些材料,例如钢与钛、钼与钛、钨与钼、钼与钼、FGH95与FGH95以及不锈钢薄片之间的热等静压连接。并用金相、电子探针、扫描电镜能谱分析以及显微硬度等初步地评价了试验结果。     

硬质合金与球墨铸铁热等静压扩散连接的研究

用热等静压扩散连接法获得了硬质合金与球墨铸铁的直接连接接头和以镍箔为中间夹层的间接连接接头。采用金相、扫描电镜、显微硬度及电子探针显微分析等手段对结合界面区域的组织结构、显微硬度变化及元素扩散进行了研究。对直接连接和间接连接接头的接合强度进行了评估,并对接头断裂特性进行了分析。     

K497与FGH741合金的热等静压扩散连接

采用热等静压（ＨＩＰ）固－固扩散连接工艺,研究了Ｋ４９７与ＦＧＨ７４１合金ＨＩＰ连接及热处理后的组织变化、结合界面的组织、力学性能及界面区元素的扩散规律。结果表明,在ＨＩＰ和热处理阶段,ＦＧＨ７４１合金未发生再结晶,其晶粒度与母材基本相同,均为ＡＳＴＭ５～６级,Ｋ４９７合金的粗大枝晶组织和共晶相经热处理后基本消除。结合界面冶金结合良好,形成了一个由亚晶和再结晶晶粒组成的界面区且无有害相析出。结合试     

热等静压及其加锻造和热挤压粉末高温合金FGH95的组织和性能

本工作的目的在于研究不同成型工艺对粉末高温合金FGH95组织和性能的影响,以确定合适的成型工艺。采用了氩气雾化的FGH95合金粉,用热等静压(HIP)、及其加锻造和热挤压三种工艺使之致密化。对各种压坯的显微组织和机械性能进行了研究。扫描电镜和透射电镜的研究结果说明,经过锻造或挤压的合金,其显微组织有明显的改善。热等静压合金的断口是沿粉末颗粒间断裂的,这是由于显微组织中存在着原始颗粒边界(PPB),降低了合金的力学性能。在热等静压加锻造或热挤压的合金中,由于消除了原始颗粒边界,断口是穿晶断裂的,因而改善了合金的强度和塑性。采用热挤压或热等静压加锻造成型工艺比较有效。     

Ti6Al4V和Al2A12的扩散连接界面组织及力学性能

采用热等静压(HIP)工艺连接Al12A12和Ti6Al4V两种不同的航空航天用材料.利用扫描电镜、能谱仪和X射线衍射仪观察连接过渡区的微观组织和组成的演化,并测试其主要的力学性能.结果表明:采用热等静压制备这两种材料的界面连接好;Ti/Al反应层界面处形成了不同的金属间化合物,例如,Al₃ Ti、TiAl₂和TiAl;连接接头处硬度为163 HV,界面连接处剪切强度达到了23 MPa,比只添加镀层而无中间层的连接强度提高了约17.9%,但低于带有中间层的连接强度.由于过烧和孔隙的形成使得断裂方式是脆性断裂.由此可知,在热等静压成形过程中异种材料的元素发生了相互扩散,在扩散连接处形成了不同的金属间化合物,这些金属间化合物影响连接处的力学性能.      

FGH96合金固相扩散连接界面组织与失效机制

对原始状态分别为锻态、固溶态和半时效态的FGH96合金固相扩散连接界面显微组织进行表征,并对连接界面的拉伸性能进行测试,对失效行为进行研究。结果表明,锻态、固溶态和半时效态试样经固相扩散连接后界面均实现了良好的冶金结合,连接界面无孔洞和缝隙等缺陷。锻态试样界面扩散更为充分,组织过渡更为平缓;固溶态和半时效态试样界面存在明显的连接影响区。锻态试样经固相扩散连接和标准热处理后,二次γ?相细小、均匀且呈典型椭球状;固溶态和半时效态试样因固相扩散连接热循环的作用导致γ?相发生长大和分化。二次γ?相尺寸及形貌的不同决定了界面区域性能水平的差异。电子背散射衍射测试结果表明,连接界面处大晶粒的择优取向为{100},距离固相扩散连接界面越近,晶粒的择优取向越明显。拉伸试验结果表明,锻态试样经固相扩散连接和标准热处理后,连接界面处的强度达到基体强度的99%以上。拉伸裂纹主要萌生于连接界面大晶粒及γ?相粗化聚集区域,体现为穿晶的韧窝型断裂。     

Effect of Operation Parameters on Diffusion Bonded AA5083, AA6082 and AA7075 Aluminum Alloys

Rolled plates of 5 mm thick AA5083, AA6082 and AA7075 aluminum alloys Joints were fabricated by diffusion bonding at different temperatures. The microstructure evolution of AA5083, AA6082 and AA7075 aluminium alloys were characterized by transmission electron microscopy. Metallurgical investigations and mechanical tests were also performed to correlate the microstructural investigations with the mechanical properties of the produced diffusion bonded joints. It was observed that the bonding and shear strength increased with the increase in bonding temperature due to the diffusion of micro-constituents in the interface. Higher temperature enhanced the uniform distribution of secondary phase particles, which further improved the reduction in pores/defects in the bonded joints.     

Effect of Hf and Zr Contents on Stress-rupture and Fatigue Crack Growth Rate Performances in FGH96PM Superalloy

Four experimental FGH96alloys with various contents of Hf and Zr(0and 0.04%,0.3% and 0.04%,0.6% and 0.04%,0.3%and 0.06%,respectively)were produced using PREP(plasma rotating electrode process)+HIP(hot isostatic pressing)route.The unnotched and notched stress-rupture properties and fatigue crack growth rate(FCGR)of all the experimental alloys were investigated to study the effect of Hf and Zr.Relevant fracture morphology and microstructure were observed by scanning electron microscopy and transmission electron microscopy.The results revealed that appropriate content of Hf could lengthen stress-rupture life,eliminate notch sensitivity and slower FCGR.Microstructure analysis showed that the amount ofγ′phase should be increased or decreased by adjusting Hf and Zr contents,and MC carbide and oxide coupled growth should be increased by adding Hf content,which caused oxycarbide to precipitate along grain boundary and strengthen the alloy.It was found that excessive Zr in Hfcontaining FGH96alloy had certain deleterious effects on stress-rupture property because there was strong Zr segregation at prior particle boundary,leaving a long chain of large-size oxides along the boundary.The optimal content of Hf and Zr in FGH96alloy was 0.6%and 0.04%,respectively.     

热轧7075/AZ31B复合板的显微组织及结合性能

为了研究热轧铝/镁复合板结合强度的变化规律,本文综合考虑压下率、轧制温度和轧制速度等多种轧制参数,单道次热轧制备了7075 Al/AZ31B Mg复合板。结果表明:在复合板轧制过程中由于热和强变形作用组织发生了动态再结晶,且增大轧制速度有助于镁基体产生完全动态再结晶。在相同轧制温度下,铝镁复合板结合强度均随压下率增加先升高后降低;强度升高是由于界面元素扩散宽度的增大和镁合金近界面晶粒组织的细化所致,强度降低是由于大变形导致镁基体近界面处产生裂缝,以及塑性功产生热量过多使得镁基体温度升高导致的镁侧晶粒长大所致。对复合板进行拉剪实验,铝镁结合界面剪切强度较低时,断裂发生在复合界面处且成脆性断裂特征,强度较高时断口形貌呈韧性断裂特征,断裂发生在镁基体侧。      

The Effects of Borides on the Mechanical Properties of TLPB Repaired Inconel 738 Superalloy

The transient liquid phase diffusion bonding (TLPB) method was used to repair an artificial crack in Inconel 738, which was notched by a femtosecond laser. Mixed ratios of BNi-1a:DF-4B were investigated at the bonding temperature of 1373 K (1100 °C) for 2 to 36 hours. The effect of borides on the mechanical properties of TLPB repaired joints was studied through analysis of the microstructure, fracture path, and morphology observations. The borides formation, morphology, distribution, and joints strength were studied in detail. The results showed that the diffusion of B can either increase or decrease the joint strength, depending on its distribution and morphology. The amount of large blocky Ni-B compounds in the precipitate zone were reduced with increasing holding time, which resulted in an increase in joint strength. Nevertheless, further increasing the holding time led to a decrease in joint strength because of the formation of continuous acicular borides in the diffusion-affected zone. The fracture modes of TLPB joints were also discussed on the basis of the microstructure and fractography.     

稀土元素铈对镁合金AZ91D显微组织和力学性能的影响

利用光学显微镜、X射线衍射和扫描电镜等分析研究含铈镁合金AZ91D（0．25％Ce、0．7％Ce、0．95％Ce）的显微组织,并对其力学性能进行了测试,同时与不含铈镁合金AZ91D进行了比较。结果表明,加入一定量Ce后的镁合金AZ91D形成杆状化合物Al4Ce,被推移到生长界面,阻碍枝晶的自由生长,从而细化合金显微组织;Ce能提高镁合金AZ91D抗拉强度和硬度,而对其屈服强度和延伸率影响不大;加入0．7％Ce的AZ91D镁合金晶粒细化效果和综合力学性能比较理想。