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An investigation of plasma pretreatments and plasma polymerized thin films for titanium/polyimide adhesion.

机译:等离子预处理和等离子聚合薄膜对钛/聚酰亚胺附着力的研究。

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Plasma pretreatments are environmentally benign and energy efficient processes for modifying the surface chemistry of materials. In an effort to improve the strength of the titanium alloy/FM-5 polyimide adhesive joint for aerospace applications, oxygen plasma pretreatments and novel thin plasma polymerized (PP) films were investigated as adhesion promoters. Plasma treatments were carried out using custom-built, low pressure, radio frequency, inductively coupled plasma reactors. Ti-6Al-4V coupons were plasma treated and used to prepare miniature single lap shear (SLS) joints. The effects of plasma pretreatments on surface chemistry were studied using x-ray photoelectron spectroscopy (XPS), Auger electron spectroscopy (AES), Fourier transform infrared analysis (FTIR), and contact angle measurements. Relationships between composition, mechanical properties, and adhesion of PP films on Ti-6Al-4V and silicon wafers were investigated. The nanomechanical properties (modulus, hardness and adhesion) were studied using atomic force microscopy (AFM) nanoindentation and nanoscratch testing.; A design of experiments (DOE) three factorial model was used to optimize the parameters for oxygen plasma treatments. Oxygen plasma pretreatments enhanced joint strength by cleaning the titanium surface and creating an extended oxide layer. Nanoindentation of oxygen plasma treated substrates showed no change in the surface mechanical properties due to the oxygen plasma treatment. This suggested that the improved SLS strength of the oxygen plasma pretreated substrates was due to the cleaning of the substrate and the removal of carbonaceous contaminants, rather than any changes in the morphology of the oxide layer.; PP acetylene films were predominantly carbon, with oxygen as the other main constituent (incorporated mostly as C-O and C=O). For all SLS specimens tested, the adhesion between PP acetylene and FM-5 adhesive was adequate. However, the strength of SLS joints was limited by the adhesion of the PP acetylene to the Ti-6Al-4V substrate. The effects of a large number of plasma parameters, such as substrate pretreatment, carrier gas, input power, flow rate and film thickness were investigated. All samples failed at the PP film/Ti-6Al-4V interface or within the PP acetylene film, and thicker PP films yielded lower SLS strengths. PP films deposited at lower power exhibited higher hardness and reduced modulus than films deposited at higher power. Overall, thinner films exhibited higher hardness and reduced Young's modulus than thicker films. PP films of higher hardness yielded higher critical loads at debond (thickness normalized) during the nanoscratch test.; Thin films were developed via the vapor plasma polymerization of titanium(IV) isobutoxide (TiiB). XPS results suggested that titanium was incorporated into the film as TiO2 clusters dispersed in an organic matrix. No evidence for Ti-C was obtained from the XPS spectra. PP films of TiiB were much more compliant than PP acetylene films. This behavior was attributed to decreased fragmentation and lower crosslinking that occurred during PP TiiB film deposition. These PP films did not exhibit sol-gel-like qualities, and because of the way titanium was incorporated into the films, a more appropriate name for these films might be "titanium dioxide-doped plasma polymerized films."
机译:等离子体预处理是对环境无害且节能的方法,可以改变材料的表面化学性质。为了提高用于航空航天的钛合金/ FM-5聚酰亚胺粘合接头的强度,研究了氧等离子体预处理和新型薄等离子体聚合(PP)薄膜作为粘合促进剂的方法。使用定制的低压射频感应耦合等离子体反应器进行等离子体处理。 Ti-6Al-4V试样经过等离子处理,并用于制备微型单搭接剪切(SLS)接头。使用X射线光电子能谱(XPS),俄歇电子能谱(AES),傅里叶变换红外分析(FTIR)和接触角测量研究了等离子体预处理对表面化学的影响。研究了Ti-6Al-4V和硅晶片上PP膜的成分,力学性能和附着力之间的关系。使用原子力显微镜(AFM)纳米压痕和纳米划痕测试研究了纳米力学性能(模量,硬度和附着力)。实验设计(DOE)三因子模型用于优化氧等离子体处理的参数。氧等离子体预处理通过清洁钛表面并形成扩展的氧化层来增强接头强度。氧等离子体处理的基材的纳米压痕未显示由于氧等离子体处理的表面机械性能的变化。这表明经氧等离子体预处理的基材的SLS强度提高是由于基材的清洁和含碳污染物的去除,而不是由于氧化物层形态的任何改变。 PP乙炔膜主要是碳,氧是其他主要成分(主要以C-O和C = O的形式结合)。对于所有测试的SLS标本,PP乙炔和FM-5粘合剂之间的粘合力都足够。但是,SLS接头的强度受到PP乙炔与Ti-6Al-4V基底的粘附性的限制。研究了大量等离子体参数的影响,例如基板预处理,载气,输入功率,流速和膜厚。所有样品在PP膜/ Ti-6Al-4V界面处或PP乙炔膜内均不合格,较厚的PP膜产生较低的SLS强度。与以较高功率沉积的膜相比,以较低功率沉积的PP膜具有较高的硬度和降低的模量。总体而言,较厚的薄膜比较厚的薄膜具有更高的硬度和降低的杨氏模量。较高硬度的PP膜在纳米划痕试验中在脱胶(厚度归一化)时产生较高的临界载荷。通过异丁醇钛(IV)(TiiB)的气相等离子体聚合开发了薄膜。 XPS结果表明,钛是作为TiO2簇分散在有机基质中而掺入薄膜的。从XPS光谱中未获得Ti-C的证据。 TiiB的PP薄膜比PP乙炔薄膜具有更高的柔顺性。此行为归因于在PP TiiB膜沉积过程中发生的碎裂减少和交联降低。这些PP膜没有表现出溶胶-凝胶状的性质,并且由于将钛掺入膜中的方式,这些膜的更合适的名称可能是“掺杂二氧化钛的等离子体聚合膜”。

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