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61.
Daniel G. Sanders Mamidala Ramulu 《Journal of Materials Engineering and Performance》2004,13(6):744-752
Superplastic forming (SPF) combined with diffusion bonding (DB) has been used successfully for the fabrication of titanium
aerospace hardware. Many of these applications have been for military aircraft, whereby a complex built-up structure has been
replaced with monolithic parts. Several methods for applying the two- and four-sheet titanium SPF/DB processes have been devised,
including the welding of sheets prior to forming and the use of silk-screened stop-off (yttria) to prevent bonding where it
is undesirable. Very little progress has been made in the past few years toward understanding and modeling the SPF/DB process
using constitutive equations and data by laboratory testing. Concerns that engineers face in designing for fatigue life, acceptable
design loads, and damage tolerance are currently being studied, but the database is very limited. This is a summary of past
work found in the literature and forms the foundation for additional research.
This paper was presented at the International Symposium on Superplasticity and Superplastic Forming sponsored by the Manufacturing
Critical Sector at the ASM International AeroMat 2004 Conference and Exposition, June 8–9, 2004, in Seattle, WA. The symposium
was organized by Daniel G. Sanders, The Boeing Company. 相似文献
62.
63.
喷涂与激光重熔技术制备镍基纳米钴包碳化物复合涂层的研究 总被引:1,自引:0,他引:1
采用横流2.0kW CO2激光器,在45钢表面制备了表面较平整、较细密、基本消除了裂纹与孔隙并与基体呈冶金结合的镍基纳米WC/Co复合涂层。通过SEM,EDAX,XRD,AFM及Nano Indenter XP分析了熔覆层的显微组织、成分、物相及结合强度。结果表明,涂层的显微组织为涂层中镶嵌着大量与Ni基合金结合良好的WC/C。颗粒,其中在原子力显微镜下可见相当数量的粒度≤100μm的纳米颗粒。涂层的结合强度比传统热喷涂涂层提高了2.1倍。涂层中纳米WC/Co的纳米效应在激光熔覆中起着重要作用。 相似文献
64.
Advances in fabricating superplastically formed and diffusion bonded components for aerospace structures 总被引:1,自引:0,他引:1
Larry D. Hefti 《Journal of Materials Engineering and Performance》2004,13(6):678-682
Superplastic forming and diffusion bonding (SPF/DB) production hardware is being fabricated today for aerospace applications.
Metal tooling is being used to bring the titanium sheets into contact so diffusion bonding can occur. However, due to material
sheet and tooling tolerances, good bond quality is difficult to achieve over large areas. A better method for achieving DB
is to use “stop-off” inside sealed sheets of titanium, which constitutes a pack, and then the pack is bonded using external
gas pressure. A good method for heating the pack for this process is to use induction heating. Components using “stop-off”
that were diffusion bonded first and then superplastically formed have shown much better bond quality than components that
were produced using matched metal tooling. This type of tooling has been successful at bonding small areas as long as the
exerted pressure is concentrated on the area where bonding is required. Finite element modeling is providing weight effect
solutions for titanium SPF/DB aerospace structures.
This paper was presented at the International Symposium on Superplasticity and Superplastic Forming, sponsored by the Manufacturing
Critical Sector at the ASM International AeroMat 2004 Conference and Exposition, June 8–9, 2004, in Seattle, WA. The symposium
was organized by Daniel G. Sanders, The Boeing Company. 相似文献
65.
66.
硬质合金与钢的热等静压扩散连接 总被引:2,自引:1,他引:2
研究了硬质合金YG15C与45~#碳钢的热等静压扩散连接工艺,探讨厂连接温度、压力、保温保压时间、中间夹层及其厚度和连接残余热应力等对接合强度的影响.结果表明:热等静压扩散连接强度强烈依赖于连接温度,受控于连接后因YG15C与45~#钢热膨胀失配而产生的残余热应力。采用镍箔作中间夹层可有效地减小残余热应力对连接的影响,显著提高接合强度. 相似文献
67.
双金属固相结合的有限元分析 总被引:3,自引:4,他引:3
双金属是由两种不同性能的金属结合而成的,经过恰当组合的两种金属结合以后,可以获得高强度、耐腐蚀以及导电、导热等综合性能,使材料在某些特殊的环境下发挥良好的作用。固相结合法是制造双金属的有效方法。本文基于刚粘塑性有限元理论,在两组元金属相互接触的表面之间引入摩擦单元,对Cu/Al双金属挤压固相结合的非稳态过程进行了有限元分析,得到了两组元金属之间的相对滑动量以及成形过程中的载荷-行程曲线,计算结果与试验结果比较接近。同时获得了变形体内的应力、应变分布,揭示了组元金属在成形过程中的流动规律。 相似文献
68.
Combined with ultrasonic pulse-echo technique, reflection spectrum analysis was introduced to evaluate TiAl and 40Cr diffusion bonding quality. Frequency dependence of reflection coefficient was used to distinguish perfect bonding from imperfect bonding. It is found that the reflection coefficient from perfect bonding interface does not vary with frequency. When the size of imperfections is much smaller than the wavelength of ultrasound, the reflection coeffwient depends on frequency. When the size of imperfections is the same order of or even larger than the wavelength of ultrasound, the reflection coeffwient does not exhibit frequency dependence. However the amplitude of imperfect interface is higher than the amplitude of perfect bonding interface. A combination of reflection spectrum analysis and ultrasonic pulse-echo technique provides more accurate information about the bonding quality of dissimilar materials. 相似文献
69.
70.