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1.
应力腐蚀门限值δSCC的恒载荷多试样测定法   总被引:2,自引:0,他引:2  
为评定金属材料在弹塑性状态下的δSCC敏感性,以现行国家标准为基础,提出了弹塑性状态下应力腐蚀断裂韧性门限值δSCC的概念和恒载荷多试样测定法.实验中的裂纹起裂时间由挠度-时间曲线的转折点确定,避开了直接观测的困难.所得结果与用其他方法得到的基本一致.  相似文献   

2.
研究了ZG06Cr16Ni5Mo 铸钢中δ铁素体形态和分布对铸钢塑性、韧性和弯曲性能的影响; 探讨了δ铁素体的分布在材料弯曲变形时的作用; 同时提出了改善δ铁素体形态和分布的措施。  相似文献   

3.
不锈钢焊缝金的氢脆   总被引:4,自引:0,他引:4  
用慢应变速率拉伸方法研究了不稳定型奥氏体不锈钢焊缝金属(308L和 347L)以及母材(304L)的氢脆敏感性,分别研究了原子氢以及氢致马氏体对氢致塑性损失的贡献,结果表明,当可扩散的氢浓度C0大于临界值(约 25×10-6-30×10-6)后三种不锈钢均会出现氢致马氏体(ε+α’),其含量 M随 C0升高而升高,即 M(ε+α’)=54.2-25 exp(-C0/153).氢致马氏体引起的塑性损失Iδ(M)随马氏体含量线性升高,即 Iδ(M)=045M=24.4-11.3 exp(-C0/153)100%马氏体引起的最大塑性损失约为 45%,动态充氢引起的塑性损失几减去充氢除气试样的塑性损失就是原子氢引起的塑性损失Iδ(H),它随 C0升高而升高,但当 C0>10-4后,Iδ(H)趋于最大值(对应 ε=5 × 10-6/s),即 Iδ(H)max=44%(308L),Iδ(H)max=45%(347L)以及 Iδ(H)max=40%(304L).随应变速率ε升高,Iδ(H)逐渐下降,直至为零(对应 ε=0.018/s—0.032/s);即 Iδ(H)=-16.4—10.6 igε(308L),Iδ(H)=-20.9—12.1  相似文献   

4.
测定了含Ce0.06wt%及0.15wt%的1420合金板材的时效硬化曲线及室温力学性能,分析了Ce对1420合金时效过程的影响。结果表明:Ce含量在0.15wt%范围内的1420合金时效的组织与不含Ce的1420合金类似,主要强化相为δ'及δ'/β'复合相。微量Ce在1420合金中可以减缓固溶处理时的再结晶过程及细化再结晶晶粒,并促进δ'相在时效过程中的弥散析出。添加0.06Wt%Ce时有利于提高合金塑性,而添加0.15wt%Ce时则有利于提高合金强度。采用465℃固溶,2%预拉伸变形及170℃/6h时效,可使含微量Ce的1420合金板材获得较好的综合力学性能。  相似文献   

5.
张瑛洁  赵芳欣 《铸造》1999,(11):15-17
研究了ZG06Cr16Ni5Mo铸钢中δ铁素体形态和分布对铸钢塑性,韧性和弯曲性能的影响;探讨了δ铁素体的分布在材料弯曲变形时的作用;同时提出了改善δ铁素体形态和分布的措施。  相似文献   

6.
PROCESSCHARACTERISTICSOFHoBa_2Cu_3O_(7-δ)ANDEFFECTOFMAGNETICFIELDONSUPERCONDUCTIVITYOFREBa_2Cu_3O_(7-δ)(RE=Y,Ho)¥Yi,Jianhong;Pen...  相似文献   

7.
QuantumChemicalCalculationonPreparationofYBa_2Cu_3O_(7-δ)PowdersbyHydrolysisofMetalAlkoxidesYinZhoulan;LiXinhai;ZhaoQinsheng;...  相似文献   

8.
激光熔覆WC—Ni复合涂层的结构和性能   总被引:2,自引:0,他引:2  
研究了两种激光熔覆WC-Ni涂层,均满足柴油机飞轮的技术要求。给出了两种WC-Ni涂层的金相组织、显微硬度及X光相分析结果。WC-Ni涂层的硬化相是δ-WC、β-W2C、M^C、M12C及少量r-WC。  相似文献   

9.
ElectronMicroscopyStudiesofMagnetronSputteredYBa_2Cu_3O_(7-δ)ThinFilmsShaWei沙维(DepartmentofMaterials,ImperialCollege,PrinceCo...  相似文献   

10.
研究了热处理对Cr17Ni2钢组织和硬度的影响。结果表明,随淬火温度由950℃升高到1100℃,组织中δ铁素体略有增加,而硬度持续增加,回火对δ铁素体数量没有影响,研究还发现该钢的硬度是基体和δ铁素体的综合贡献,存在如下近似关系式HV=HVM(1-fF)+HVFfF。  相似文献   

11.
Mo2C is normally added to improve the wettability between Ti(C,N) and Ni in Ti(C,N)-based cermets. Due to the increasing price of Mo2C, much attention has been paid to Ti(C,N)-based cermets with WC addition. In this paper, effect of WC content on the microstructure and properties of Ti(C0.7N0.3)-xWC-15wt.%Ni cermets free of Mo2C was studied. The experimental results show that the microstructure is refined obviously with the increase of WC content. The fracture toughness decreases with the increase of WC content when WC content is 10-25 wt.%, and increases when WC content varies from 25 wt.% to 30 wt.%.  相似文献   

12.
Three Laves phase-based alloys with nominal compositions of Cr2Nb–x Ti(x = 20,30,40,in at%) have been prepared through vacuum non-consumable arc melting.The results show that the microstructures of Cr2Nb-(20,30) Ti alloys are composed of the primary Laves phase C15–Cr2(Nb,Ti) and bcc solid solution phase,while the microstructure of Cr2Nb–40Ti alloy is developed with the eutectic phases C15–Cr2(Nb,Ti)/bcc solid solution.The measured fracture toughness of ternary Laves phase C15–Cr2(Nb,Ti) is about 3.0 MPa m1/2,much larger than 1.4 MPa m1/2for binary Laves phase Cr2 Nb.Meanwhile,the fracture toughness of Cr2Nb–x Ti(x = 20,30,40) alloys increases with increasing Ti content and reaches 10.6 MPa m1/2in Cr2Nb–40Ti alloy.The eutectic microstructure and addition of Ti in Cr2 Nb are found to be effective in toughening Laves phase-based alloys.  相似文献   

13.
High-temperature fracture strength and compressive creep of an electrodischarge-machinable composite, Al2O3-30.9 vol.% SiC whiskers-23 vol.% TiC particles have been studied to 1200 °C and 1450 °C, respectively, in inert atmosphere. Microstructures of fractured and deformed specimens were examined using scanning and transmission electron microscopy. Fast fracture occurred at T ≤ 1200 °C. Steady-state creep was achieved for T > 1350 °C at stresses < 80 MPa, with the rate-controlling mechanism being partially unaccommodated grain-boundary sliding, with a stress exponent of ≈ 1 and an activation energy of≈ 470 kJ/mol.  相似文献   

14.
Effect of Mo and Mo2 C on the microstructure and properties of Ti(C,N)-based cermets was investigated in this article. The results have indicated that the weight percentage of Mo from 5 to 10 can reduce Ti(C,N) grain diameter and thickness of the rim, and Ti(C,N) grain can be wetted by Ni-Cu-Mo liquid so as to get small contiguity of Ti(C,N) grain. In that way, the transverse rupture strength of Ti(C,N)-based cermets has reached 1800-1900 MPa; the fracture toughness has been due to 16-18 MPa.m1/2. But 15 wt pct Mo was not more effective on Ti(C,N)-based cermets, because the thickness of the rim becomes larger. In the circumstance of Mo2 C, 5 wt pct Mo2 C was good for microstructure and properties of Ti(C,N)-based cermets, but 11 wt pct Mo2C has resulted in larger contiguity of Ti(C,N) grain and big Ti(C,N) grain diameter so as to reduce transverse rupture strength and fracture toughness. So that, the effect of Mo on Ti(C,N)-based cermets is better than Mo2C.  相似文献   

15.
The paper presents a new approach for the prediction of ductile fracture occurrence in multi-stage cold forging process chains. The approach combines the fracture criterion proposed by Xue and Wierzbicky with a linear damage accumulation law. Thanks to this feature, the approach is capable of predicting both the location where the failure events occur under the action of external loading and the time they take to be generated. An application to the multi-stage cold forging of a C35 Torx-type socket screw carried out on a double-blow header is presented and results of predictions are compared with experimental observations.  相似文献   

16.
利用原位高温拉伸台在扫描电镜中研究了镍基铸造高温合金MAR-M247在室温、400 ℃与760 ℃拉伸过程中的动态组织演变和断裂机制。原位测试结果表明,在室温到760 ℃范围内,MAR-M247合金的屈服强度与抗拉强度随温度的升高略有下降,拉伸塑性略有提高。室温原位拉伸过程中,并没有出现滑移带;400 ℃与760 ℃的原位拉伸,只在样品断口附近存在少量的滑移带。随拉伸温度的提高,合金的断裂机制并无明显变化,均表现为韧性穿晶断裂。合金的微裂纹主要来源于变形过程中碳化物的破裂,晶内与晶界都存在因碳化物破裂而形成的微裂纹。  相似文献   

17.
In order to clarify the forming limit of magnesium alloy in cold forging, the workability of magnesium alloy AZ31B (Mg-3%Al-1%Zn) is examined by upsetting and backward extrusion. In the upsettability test, shear type fracture occurs at a small equivalent strain of about 0.15 at temperatures lower than 170 °C. At a higher temperature, the flow stress curve has a peak at an average equivalent strain of 0.2-0.3, showing a clear tendency to work soften. In cold backward extrusion with a conical punch, the local strain can reach a very large value, 3.0 or greater, without fracture. To explain the experimental results, the mechanism of fracturing is discussed on the basis of strain localization, and a fracture criterion of magnesium alloy in cold forging is suggested. The newly proposed criterion provides much better results than the existing criteria.  相似文献   

18.
An Nb-Silicide in situ composite with a nominal composition of Nb-16Si-10Ti-10Mo-5Hf (at. %) was fabricated by mechanical alloying followed by hot-pressing sintering. The microstructure consisted of an Nb solid solution, Nb5Si3 and a small amount of Nb3Si. This in-situ composite exhibited good balance of strength between ambient temperature and high temperatures; the ultimate tensile strength was 413 and 496 MPa at room temperature and 1200 °C, respectively. The tensile fracture behavior was dominated by cleavage of the Nbss and Nb5Si3 at 1200 °C and lower temperatures. However, the fracture behavior was governed by ductile rupture of Nbss at 1300 °C and higher temperature, which was ascribed to both the increased ductility of Nbss and the decreased interface strength. At 1400 °C and higher temperature, the material exhibited extensive plasticity or superplasticity; the dominant deformation mechanism was grain boundary sliding at 1400 °C and higher temperature.  相似文献   

19.
In the present investigation electroless Ni-P coatings were prepared. Structural characterizations indicated that the as-deposited coating had an amorphous structure with a P content of 23 at.%. The deformation behavior of an electrolessly amorphous Ni-P coating was investigated by using the Vickers indentation and the Tribo-indenter instrumented nano-indentation technique. The hardness of the Ni-P coating is remarkably improved after proper heat-treatment and the hardness is as high as 12.7 GPa for the coating annealed at 400 °C for 1 h. However, the cracks were observed during the indentation of the Ni-P coatings annealed at 400 °C and 500 °C for 1 h. The corresponding fracture toughness was evaluated as 2.58 MPa m0.5 and 1.33 MPa m0.5, respectively. Nanoscratching tests indicated that the wear resistance of the Ni-P coatings was improved significantly with an increasing ratio of hardness (H) to elastic modulus (E). It was observed that the friction coefficient increased from 0.083 ± 0.006 for the Ni-P coating annealed at 300 °C up to 1.337 ± 0.009 for the IF steel substrate, while the H/E simultaneously decreased from 0.084 (10.7/128) to 0.009 (1.85/200). The study revealed that the electrolessly amorphous Ni-P coating had offered better corrosion resistance than the Ni-P coatings after heat-treatment. An annealing temperature of 300 °C is preferentially suggested for the trade-off between the wear resistance property and anti-corrosion property of the Ni-P coating.  相似文献   

20.
Some existing wrought Ni-Cr-Co-based superalloys are being evaluated as the candidate materials for advanced ultra-supercritical power plant applications beyond 700 °C due to their high creep strength. But they are all prohibitively expensive due to the addition of Co, Mo and W. Here we developed a new Ni-Fe-Cr-based superalloy (named as HT700 alloy) with low cost and high strength. This paper reports the mechanical properties and fracture modes of HT700 alloy to support its high temperature applications and to understand prospective failure mechanism. Fractographic examinations indicate that the fracture modes shift with test condition change. In addition, the HT700 alloy has relatively stable microstructure at 750 °C. Compared with IN740 and GH2984 alloys, this new alloy has higher yield strength in the temperature range from room temperature to 800 °C. The creep life of this new alloy is much longer than that of the Ni-Fe-based superalloy GH2984. The results suggest that this new alloy is a promising material for advanced ultra-supercritical power plant applications beyond 700 °C.  相似文献   

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