高温合金,Superalloy
1)Superalloy[英][,sju:p?r'?l?i][美][,sup?'?l??]高温合金
1.Trace analysis of superalloy by laser ablation inductively coupled plasma mass spectrometry with internal standard;激光剥蚀-电感耦合等离子体质谱内标定量法测定高温合金中痕量元素
2.Determination of multi-elements in superalloy by glow discharge mass spectrometry and interference correction;高温合金中多元素辉光放电质谱法测定及干扰校正
3.Morphology characterization of γ′ phase in a P/M nickel-base superalloy;镍基粉末高温合金中γ′相的形貌特征的定量表征研究
英文短句/例句

1.Types of heat-resisting superalloysGB/T14992-1994高温合金牌号
2.Research on High Temperature Fatigue Life Models of Powder Metallurgy;粉末高温合金高温疲劳寿命模型研究
3.The Research on Mechanism of GH4133B Superalloy after Fatigue at Elevated Temperature;镍基高温合金GH4133B的高温疲劳行为研究
4.High- temperature Alloys High-temperature-sensitive Mechanism of Crack高温合金高温裂纹敏感性机理的研究
5.Transverse Stress-rupture Properties of Single Crystal Superalloy DD6 at Mediate Temperature单晶高温合金DD6的中温横向持久性能
6.Wear Mechanism of Cemented Carbide Tool in High Speed Machining Iron-based Superalloy GH2132高速车削铁基高温合金硬质合金刀具磨损机理
7.Creep Rupture Behavior of a Cast Ni-base Superalloy at High Temperature一种铸造镍基高温合金的高温蠕变断裂行为
8.High Temperature Mechanical Behavior of a Cast Nickel-base Superalloy with Low Cost一种低成本镍基铸造高温合金的高温力学行为
9.Study on the High Temperature Oxidation Behaviors of NiCrAlCo Superalloy Sheet Prepared by EB-PVD;EB-PVD制备NiCrAlCo高温合金薄板高温氧化行为研究
10.Low Cycle Fatigue Fracture Mechanism at Elevated Temperature for FGH96 Nickel-base SuperalloyFGH96镍基高温合金的高温低周疲劳断裂机理研究
11.Microstructure of high Cr content cast Ni-base superalloy K4648高Cr铸造Ni基高温合金K4648的显微组织
12.RULE OF SEGREGATION OF ALLOYING ELEMENTS IN CAST Ni-BASE SUPERALLOYS镍基铸造高温合金中合金元素的偏析规律
13.Experimental Study on the Green Cutting Technology of High Temperature Alloy and Titanium Alloy;钛合金与高温合金的绿色切削技术试验研究
14.Study on the Microstructure of Nickel-based Superalloy and Titanium Alloy Surface Coating;镍基高温合金和钛合金表面涂层微观组织分析
15.Effects of Pouring Temperature on the Solidification Microstructure of Single Crystal Superalloy DD6浇注温度对DD6单晶高温合金凝固组织的影响
16.Influence of Shear Temperature on Chip Formation of Turning GH4169剪切温度对车削加工GH4169镍基高温合金的影响
17.Isothermal oxidation behavior of Ni-Cr-based superalloy containing MoS_2 at 800℃含MoS_2镍基高温合金在800℃的恒温氧化行为
18.Isothermal Low-cycle Fatigue and Thermomechanical Fatigue Behavior of MCrAlY Coated and Uncoated Nickel Base Superalloy;MCrAlY涂覆的镍基高温合金及其基体合金的等温和热机械疲劳行为
相关短句/例句

high temperature alloy高温合金
1.Research of deposition feature of laser melting for forming high temperature alloy powder;激光熔积高温合金件形状特征的基础研究
2.Exchangeable search in forming quality control of high temperature alloy deformation;变形高温合金成型质量控制中的转换研究
3.Research on cutting procedure of casting high temperature alloy K423A;铸造高温合金K423A的切削加工性能研究
3)Superalloys高温合金
1.Relative density and gas content in spray formed superalloys;喷射成形高温合金沉积坯致密度与气体含量
2.Spray forming technology of high temperature materials and spray depositied superalloys;结构材料喷射成形技术与雾化沉积高温合金
3.Determination of High-Content Fe in Ni-Base Superalloys by FAAS;FAAS法测定镍基高温合金中高含量铁
4)high-temperature alloy高温合金
1.Numerical simulation and experimental analysis on microstructural changes during heading of high-temperature alloy bolt;高温合金螺栓镦挤过程的微观组织演变模拟及试验研究
2.On the Processing methods of high-temperature alloy by CNC Lathe如何在数控车床上加工高温合金
3.The present method has been used for the particle size determination of carbides and metal precipitates in microalloyed steel,middle-alloy steel and high-temperature alloys.该方法被广泛应用于各种高温合金、中低合金钢、微合金化钢中碳化物、金属间化合物的粒度尺寸分布的测定。
5)super alloy高温合金
1.Microstructure and properties of nano ceramic and micro super alloy composite coating;纳米陶瓷微米高温合金复合涂层组织与性能
2.Microstructure of directly formed super alloy by plasma fused-deposition;等离子熔积直接成形高温合金件组织结构研究
3.Numerical Simulation of Vacuum Heat Treatment and Hot Bulge Forming Process of Super Alloy and Titanium Alloy;高温合金和钛合金真空热处理及热胀形过程数值模拟
6)superalloy 740高温合金740
延伸阅读

高温合金高温合金superalloy600~1200℃温度下能承受一定应力并具有抗氧化和抗腐蚀能力的合金。其典型组织是奥氏体(碳溶于γ铁中形成的固溶体)基体,在基体上弥散分布着碳化物、金属间化合物等强化相。高温合金的主要合金元素有铬、钴、铝、钛、镍、钼、钨等。合金元素起稳定奥氏体基体组织,形成强化相,增加合金的抗氧化和抗腐蚀能力的作用。常用的高温合金有铁基、镍基和钴基3种。铁基高温合金除含铁外,还含有一定量的铬和镍等元素,在600~800℃条件下具有一定的强度和抗氧化、抗燃气腐蚀能力。中温(低于800℃)力学性能和热加工塑性好,可用于制造航空发动机和工业燃气轮机的零部件。镍基高温合金可溶解较多的合金元素,如铬、钨、钼、钴等,在650~1000℃下有较高的强度和良好的抗氧化、抗燃气腐蚀能力,是应用最广的一种高温合金。用于制造航天器、火箭发动机、核反应堆的零部件。钴基高温合金的碳含量和镍、铬等合金元素含量较高,主要靠碳化物强化,在730~1100℃下,具有一定的高温强度、良好的抗热腐蚀和抗氧化能力。用于制作工业燃气轮机、舰船燃气轮机的导向叶片等。