共查询到20条相似文献,搜索用时 109 毫秒
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航空用宽滞后Ni-Ti-Nb记忆合金管接头研究 总被引:1,自引:1,他引:0
一、前言 形状记忆合金第一次成功的应用是美国Raychem公司于1969年生产的Ti_(50)Ni_(47)Fe_3记忆合金管接头用于Grumman航空公司的F—14战斗机上的液压管路系统连接。至今这种记忆合金管接头在美国各种型号飞机上使用已超过150万只,尚未发现一例失效,其连接的可靠性和密封性均达到十分满意的程度,而且实际安装施工简单方便,深受工程界的欢迎。现在,美国所有新的军用飞机几乎都规定用NiTi记忆合金管接头作为液压管路连接唯一的许用系统。但由于NiTi二元合金相变滞后小,制成的记忆合金零件在安装前必须保存在液氮中,因此工程应用很不方便。1986年,美国Raychem公司发展了一种Ni-Ti-Nb宽滞后记忆合金,该合金经适当的低温变形处理后相变滞后(As—Ms)可达150℃,显著高于常用的NiTi和NiTiFe合金(通常约为30℃~50℃),用这种宽滞后记忆合金制成的管接头可在室温下运输、储存,不需保存在液氮中,利于推广应用。此后,航空用记忆合金管接头大量改为Ni_(47)Ti_(44)Nb_9合金,这种管接头只需在-60℃扩径,在常温下保存不发生形状 相似文献
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铜基形状记忆合金管接头在舰船中的应用研究 总被引:1,自引:0,他引:1
用Cu(27-35)Zn-(1.8-2.5)Al记忆合金制作管接头。研究了合金成分设计、热处理工艺对记忆效应的影响及扩管装配接管性能。该管接头已实船安装使用,效果良好。 相似文献
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研究了Ni—Ti—Nb宽滞后形状记忆合金点焊环拉伸试验的断裂行为。对形状记忆合金环的断口形貌及微区成分用扫描电镜作了分析,得出了形状记忆合金环中的(Ti,Nb)2Ni硬脆相是导致断裂的主要原因。并分析了(Ti,Nb)2Ni硬脆相形成的原因,提出了利用多次电弧炉熔炼和热变形工艺的方法来提高记忆合金冶金质量的建议。 相似文献
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简述二元NiTi合金中R相变、马氏体相变、沉淀析出相的主要研究成果以及三元窄滞后NiTiCu合金和宽滞后NiTiNb合金的相变和组织特征。 相似文献
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Ni47 Ti44 Nb9合金丝氩弧焊接头的显微组织和力学行为 总被引:2,自引:0,他引:2
系统研究了Ni47Ti44Nb9宽滞后记忆合金带氩弧焊点丝材的显微组织和力学行为.结果表明,焊后适当温度退火处理可显著改善焊点的显微组织,得到细小、均匀的等轴晶,从而提高了焊点的力学性能,室温下表现出较高的拉伸强度和延伸率.焊后未经退火处理的试样,室温拉伸断口均位于焊缝金属的熔合区内,微观断口存在明显的解理台阶,为典型脆性断裂.退火处理后,断口位于近焊缝处的热影响区内,是韧窝型断口,属塑性断裂.韧窝内镶嵌有(Ti,Nb)2Ni相,该相内部及其与基体交界处存在有明显的微裂纹.带焊点丝材经退火处理后在---60℃下变形,最大弯曲可恢复应变约为5%,表明焊点处仍具有一定的记忆效应. 相似文献
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研究了Fe-Mn-Si-Cr-Ni系形状记忆合金管接头形状记忆效应和耐腐蚀性能。结果表明,随着预变形量的增加,管接头的形状记忆效应下降,而恢复应变呈上升趋势,当预变形超过5.3%左右时,上升幅度不大;连接状态的管接头在模拟油田介质中的耐腐蚀性能比3.5%的NaCl溶液中的抗蚀性差;在模拟油田介质中,连接状态和未连接的管接头相比,由于回复应力使表面产生拉应力以及应力诱发ε马氏体的存在,使连接状态的管接头耐腐蚀性能下降;随着预变形的增大,由于回复应力、管接头裂纹以及晶体缺陷密度增加的共同作用,使连接状态的管接头耐腐蚀性能降低。 相似文献
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W. Siegert M. Mertmann K. Neuking G. Eggeler 《Materialwissenschaft und Werkstofftechnik》2000,31(9):822-824
Influence of thermomechanical treatment on a NiTiNb shape memory alloy for coupling devices The application of shape memory alloys in coupling devices depends considerably on the phase transition temperatures of the material. On the one hand it is important to achieve a high austenite start temperature. On the other hand the difference between martensitic and austenitic transition start‐temperatures should be as large as possible. The present work investigates the influence of thermomechanical treatments on the phase transition temperatures of a NiTiNb alloy. The aim is to optimize the properties of the semi‐product for later applications in coupling devices. 相似文献
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High specific strength and stiffness are characteristics desired for aircraft and launch vehicle domains to enhance the payload gain and performance. The mechanical properties of the composites can be further tailored by embedding structural components, such as shape memory alloys, into the passive composite structure. The present study is primarily focused on the nonlinear free vibration analysis of spherical and cylindrical composite shell panels embedded with shape memory alloy fibers. The nonlinear finite element governing equations based on the higher-order shear deformation plate theory and principle of virtual work with nonlinear von-Karman strain displacement relations are employed for the analysis. The temperature-dependent material properties of shape memory alloy are considered in the formulation. A nine-noded isoperimetric element is accounted for synthesizing the element for the finite formulation. The Young's modulus and the recovery stress vary with temperature and higher nonlinearity. The incremental method is used to generate the inputs for the temperature-dependent nonlinear properties of materials. The temperature change is divided by many small temperature increments. The temperature-dependent material properties are assumed constant during the small increment. The mechanics of shape memory alloy in substrate are presented and the governing equation of laminated composite with shape memory alloy is obtained and implemented in the MATLAB 7.8 program. 相似文献
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Bangyi CHEN Chenghao LIANG Daojun FU School of Chemical Engineering Dalian University of Technology Dalian China State Key Laboratory for Corrosion Protection Shenyang China 《材料科学技术学报》2005,21(2):226-230
Electrochemical test technology and surface analysis method were employed to investigate the pitting corrosion of Cu-Zn-AI shape memory alloy in simulated uterine fluid. The results showed that the breakage of the breaking-renovating equilibrium of surface layers resulted in the pitting corrosion of Cu-Zn-AI shape memory alloy in simulated uterine fluid. The development of pitting corrosion was controlled by dissolution of surface layers. The critical pitting corrosion potential was 1.70 VSCE. The kinetics equation for the development of pitting corrosion for Cu-Zn-AI shape memory alloy in simulated uterine fluid was io=465.68 t-0.5+1.5. Pitting appearances of pits could be two types: tortoise-shell, and anomaly abscess. Cl- ion facilitated the pitting corrosion of Cu-Zn-AI shape memory alloy by competing adsorption and concentrating on alloy surface at high positive potential. 相似文献
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《Science and Technology of Advanced Materials》2005,6(7):772-777
Ferromagnetic shape memory alloys, exhibiting large recoverable strain and rapid frequency response, appear to be promising shape memory actuator material. These materials exhibit large shape memory effect associating with martensitic transformation, and magnetic-field-induced strain in the martensite state. The recent development in researches on NiMnGa, NiFeGa, and CoNiGa in our group is briefly reviewed. The perspectives of the ferromagnetic shape memory alloy are also described. 相似文献