{"currentpage":1,"firstResult":0,"maxresult":10,"pagecode":5,"pageindex":{"endPagecode":5,"startPagecode":1},"records":[{"abstractinfo":"简要综述了Ti-6Al-4V合金的显微组织和织构对其疲劳性能的影响及其机理.","authors":[{"authorName":"李兴无","id":"b3b3b138-09e4-4224-9d13-7a58f58e62e9","originalAuthorName":"李兴无"},{"authorName":"夏绍玉","id":"de3ccc54-dae0-4fb1-8792-321efca3aedc","originalAuthorName":"夏绍玉"},{"authorName":"沙爱学","id":"ec39910f-8184-4c8f-bcae-618073a9f9fb","originalAuthorName":"沙爱学"}],"doi":"10.3321/j.issn:0412-1961.2002.z1.081","fpage":"277","id":"1878028c-d808-47dc-b033-25432ec83f98","issue":"z1","journal":{"abbrevTitle":"JSXB","coverImgSrc":"journal/img/cover/JSXB.jpg","id":"48","issnPpub":"0412-1961","publisherId":"JSXB","title":"金属学报"},"keywords":[{"id":"71ff6af2-8ee2-4b09-9072-9d54b63831ae","keyword":"Ti-6Al-4V 合金,疲劳性能,显微组织,织构","originalKeyword":"Ti-6Al-4V 合金,疲劳性能,显微组织,织构"}],"language":"zh","publisherId":"jsxb2002z1081","title":"Ti-6Al-4V合金的疲劳性能","volume":"38","year":"2002"},{"abstractinfo":"研究了Ti-6Al-4V钛合金细晶等轴组织的应变疲劳性能及其断裂行为.实验结果表明,Ti-6Al-4V铁合金的应变疲劳的过渡疲劳寿命Nt约为560个循环周次,其疲劳行为具有非常明显的循环软化特性.在不同应变幅测试条件下,均为多源疲劳萌生模式.Ti-6Al-4V合金应变疲劳断口表面大量的二次裂纹特征说明该合金具有优异的应变疲劳性能.","authors":[{"authorName":"沈莉莉","id":"b5acdbf6-1cb7-4d99-b06c-a6471bb60845","originalAuthorName":"沈莉莉"},{"authorName":"陶春虎","id":"8fa69a4d-8b08-4ed4-9069-36021d7c2b01","originalAuthorName":"陶春虎"}],"doi":"10.3969/j.issn.1001-4381.2010.z1.082","fpage":"377","id":"aa397bb5-3e37-426a-9e21-4466c911df58","issue":"z1","journal":{"abbrevTitle":"CLGC","coverImgSrc":"journal/img/cover/CLGC.jpg","id":"9","issnPpub":"1001-4381","publisherId":"CLGC","title":"材料工程"},"keywords":[{"id":"1fc42d4e-e3b7-4bc9-b964-66d19689b83e","keyword":"应变疲劳","originalKeyword":"应变疲劳"},{"id":"32a1ed5d-4b13-4164-bfee-626fb4294c68","keyword":"过渡疲劳寿命","originalKeyword":"过渡疲劳寿命"},{"id":"69d8b406-c98d-45cb-b4c1-84ab7f5438c5","keyword":"循环软化特性","originalKeyword":"循环软化特性"}],"language":"zh","publisherId":"clgc2010z1082","title":"Ti-6Al-4V钛合金细晶组织的应变疲劳行为研究","volume":"","year":"2010"},{"abstractinfo":"研究了Ti-6Al-4V ELI合金板材的显微组织对疲劳裂纹扩展速率的影响.用金相显微镜对不同热处理制度下该合金α和β转变组织的变化进行了观察分析.采用MTS-810低周疲劳试验机测试合金的裂纹扩展速率.通过Origin 6.0软件对数据进行处理并绘制裂纹扩展速率(△a/△N)与应力强度因子幅△K的关系曲线.结果表明:在Pairs区范围内,疲劳裂纹扩展速率对双态组织中初生α相含量的多少不敏感,而在近门槛区和快速扩展区,裂纹扩展速率对组织比较敏感;在本实验研究的条件下,细针编织状魏氏组织的da/dN<平直状片层组织的da/dN<双态组织的da/dN.","authors":[{"authorName":"李辉","id":"a73b9d49-d149-479a-96d3-cbbf4dcfb9b5","originalAuthorName":"李辉"},{"authorName":"曲恒磊","id":"c07b92f0-c697-4fb6-8b62-eaf61fb197dd","originalAuthorName":"曲恒磊"},{"authorName":"赵永庆","id":"6df9d015-5bfa-45b6-9003-7c2b6cf59fc7","originalAuthorName":"赵永庆"},{"authorName":"曾卫东","id":"82b98c10-784b-4f5d-9421-8b02fcb0e9c5","originalAuthorName":"曾卫东"},{"authorName":"冯亮","id":"7277a2ea-ade4-48b1-956b-8aa6689d0d25","originalAuthorName":"冯亮"},{"authorName":"陈军","id":"e5f0368e-c8c7-422f-8cf3-6b1c162445c9","originalAuthorName":"陈军"}],"doi":"10.3969/j.issn.1674-3962.2006.03.005","fpage":"26","id":"e5858166-c0c6-4f20-b666-4e4b56cabce8","issue":"3","journal":{"abbrevTitle":"ZGCLJZ","coverImgSrc":"journal/img/cover/中国材料进展.jpg","id":"80","issnPpub":"1674-3962","publisherId":"ZGCLJZ","title":"中国材料进展"},"keywords":[{"id":"c7386970-28d1-4905-8b09-ae46d88c4cfc","keyword":"Ti-6Al-4VELI合金","originalKeyword":"Ti-6Al-4VELI合金"},{"id":"9b57c4d3-afc9-4667-96fe-5577e87a6114","keyword":"板材","originalKeyword":"板材"},{"id":"cdceb0a0-29cc-41e8-ae49-0568df79b76c","keyword":"疲劳裂纹扩展速率","originalKeyword":"疲劳裂纹扩展速率"}],"language":"zh","publisherId":"zgcljz200603005","title":"显微组织对Ti-6Al-4V ELI合金疲劳裂纹扩展速率的影响","volume":"25","year":"2006"},{"abstractinfo":"研究了Ti-6Al-4V ELI合金板材的显微组织与力学性能.结果表明:双态组织,强度、塑性都比较高;而对于片层组织,随着片层的粗化,强度降低,延伸率先升高后降低,面缩呈下降趋势.片层粗化,抵抗裂纹穿越、迫使裂纹拐弯能力增大,提高了断裂韧性.","authors":[{"authorName":"李辉","id":"a211f24d-58bc-4b00-a605-290b79b7e893","originalAuthorName":"李辉"},{"authorName":"曲恒磊","id":"019d89c9-3db8-47d8-a1db-5585675862a4","originalAuthorName":"曲恒磊"},{"authorName":"赵永庆","id":"6080a0e4-b013-4eba-a95a-d27367a2364c","originalAuthorName":"赵永庆"},{"authorName":"冯亮","id":"e8bdca62-d031-495e-87d3-416407344ef8","originalAuthorName":"冯亮"},{"authorName":"郭红超","id":"3642011e-94c4-4ac1-a852-ec793b930ece","originalAuthorName":"郭红超"},{"authorName":"周伟","id":"0e8011f5-5bfe-4417-8c91-98be44f0cb78","originalAuthorName":"周伟"}],"doi":"10.3969/j.issn.1009-9964.2005.06.006","fpage":"24","id":"568a8801-2fab-43c9-8db5-69fb0c9eadd4","issue":"6","journal":{"abbrevTitle":"TGYJZ","coverImgSrc":"journal/img/cover/TGYJZ.jpg","id":"60","issnPpub":"1009-9964","publisherId":"TGYJZ","title":"钛工业进展"},"keywords":[{"id":"b31973e8-a5cb-4f2d-a22e-145ca7699b3a","keyword":"Ti-6Al-4V ELI","originalKeyword":"Ti-6Al-4V ELI"},{"id":"a05b9b14-cb3d-438c-bdb1-e71ee0d61d36","keyword":"厚板","originalKeyword":"厚板"},{"id":"c8c95d78-e82e-4c6a-8ae6-3b588a707b65","keyword":"组织","originalKeyword":"组织"},{"id":"d9343473-6c3c-431a-8f30-015ebe3b99a3","keyword":"性能","originalKeyword":"性能"}],"language":"zh","publisherId":"tgyjz200506006","title":"Ti-6Al-4V ELI合金板材的显微组织与力学性能研究","volume":"22","year":"2005"},{"abstractinfo":"研究采用一种新的热机械处理工艺获得的SP700和Ti-6Al-4V钛合金细晶组织的室温疲劳裂纹扩展性能及其疲劳断裂行为.实验结果表明,与Ti-6Al-4V合金相比,SP700钛合金具有更低的疲劳裂纹扩展速率,特别是在较大的△K的情况下.SP700和Ti-Al-4V合金具有基本相同的波浪滑移疲劳断裂特征.","authors":[{"authorName":"蔡建明","id":"63b5ce1f-7989-4262-8247-007d16bd2a73","originalAuthorName":"蔡建明"},{"authorName":"许超","id":"f7bed2b3-4d31-4d6d-a813-e368e507465a","originalAuthorName":"许超"},{"authorName":"郝孟一","id":"be79f0b0-02dc-460f-b216-b19b68a31edd","originalAuthorName":"郝孟一"},{"authorName":"黄旭","id":"cee319b0-bc25-42dd-82d0-fac2cb41a8af","originalAuthorName":"黄旭"},{"authorName":"马济民","id":"a670a25a-5607-40a9-9897-783774d5e996","originalAuthorName":"马济民"},{"authorName":"曹春晓","id":"663c476f-4212-4382-992b-015c5c69add8","originalAuthorName":"曹春晓"}],"doi":"10.3969/j.issn.1005-5053.2006.03.014","fpage":"71","id":"32173e3e-8d4c-460a-9563-3ef63813ad4f","issue":"3","journal":{"abbrevTitle":"HKCLXB","coverImgSrc":"journal/img/cover/HKCLXB.jpg","id":"41","issnPpub":"1005-5053","publisherId":"HKCLXB","title":"航空材料学报"},"keywords":[{"id":"4c65b406-280b-4f6f-8944-555fa1564606","keyword":"SP700","originalKeyword":"SP700"},{"id":"083d3904-c6c3-4093-a90b-311e8382b53d","keyword":"Ti-6Al-4V","originalKeyword":"Ti-6Al-4V"},{"id":"5abe94e4-0674-4e52-9f45-d02b8722723b","keyword":"疲劳裂纹扩展速率","originalKeyword":"疲劳裂纹扩展速率"}],"language":"zh","publisherId":"hkclxb200603014","title":"SP700和Ti-6Al-4V钛合金细晶组织的疲劳裂纹扩展特征","volume":"26","year":"2006"},{"abstractinfo":"针对Ti-6Al-4V合金在加工和服役过程中的损伤特点,对Ti-6Al-4V合金锻件的3种典型误加工缺陷--槽缺陷、面缺陷和体缺陷进行了激光快速修复研究.激光修复区与锻件基体形成致密冶金结合,Al、V合金元素由锻件基体到激光修复区均匀分布,无宏观偏析.激光修复区组织为粗大原始β晶粒内分布细长的α针及编织细密的α+β板条组织,呈现典型的魏氏结构,热影响区组织从锻件的等轴α+转变β组织逐步过渡到魏氏(α+β)组织.对预制有3种类型缺陷的激光修复试样进行室温静载拉伸试验和硬度测试,结果表明修复试样的拉伸性能达到锻件标准(HB5224-1982).激光修复试样的硬度和强度高于锻件基体,而塑性则低于锻件基体.因此,激光修复区和锻件基体可看作是一种\"强+弱\"的组合,这与二者的显微组织是相对应的.","authors":[{"authorName":"薛蕾","id":"321bf22b-23f4-4775-b833-12230f82a9d6","originalAuthorName":"薛蕾"},{"authorName":"陈静","id":"3c0bbc4e-3d2b-4949-a072-53b00f82d289","originalAuthorName":"陈静"},{"authorName":"林鑫","id":"f960c58e-2ae2-4b37-bde2-54ea4d397c0e","originalAuthorName":"林鑫"},{"authorName":"王维","id":"c6cd1f55-7f18-411e-808b-90542d5d8f37","originalAuthorName":"王维"},{"authorName":"吕晓卫","id":"e9fad2dc-7836-45d1-93bb-51800d8a7263","originalAuthorName":"吕晓卫"},{"authorName":"黄卫东","id":"9e7b3380-f6b8-4188-bb57-7714546b3481","originalAuthorName":"黄卫东"}],"doi":"","fpage":"989","id":"fa63cc56-bef8-400e-ae3d-db5eaa4a7ad7","issue":"6","journal":{"abbrevTitle":"XYJSCLYGC","coverImgSrc":"journal/img/cover/XYJSCLYGC.jpg","id":"69","issnPpub":"1002-185X","publisherId":"XYJSCLYGC","title":"稀有金属材料与工程"},"keywords":[{"id":"6c037b4d-8223-4620-b0d7-59841be11b66","keyword":"激光快速修复","originalKeyword":"激光快速修复"},{"id":"4481ff70-e9f6-458d-b1d6-5ce13ba23c93","keyword":"Ti-6Al-4V合金","originalKeyword":"Ti-6Al-4V合金"},{"id":"7fab25fd-0056-4169-ba07-b0fe62390f7a","keyword":"显微组织","originalKeyword":"显微组织"},{"id":"d144cd26-3ab1-4abb-a0c1-a1a6fb8ebd4c","keyword":"力学性能","originalKeyword":"力学性能"}],"language":"zh","publisherId":"xyjsclygc200706011","title":"激光快速修复Ti-6Al-4V合金的显微组织与力学性能","volume":"36","year":"2007"},{"abstractinfo":"
采用自行研制的超声疲劳实验装置, 研究不同表面粗糙度下Ti-6Al-4V合金的超高周疲劳性能. 结果表明, 当表面凹痕宽深比a/c (a为凹痕宽度, c为凹痕深度)在2~10之间时, Ti-6Al-4V合金的临界凹痕深度在0.49~1.10 μm之间. 当表面凹痕深度小于临界深度时, 表面粗糙度对Ti-6Al-4V合金的超高周疲劳性能没有影响. 当表面凹痕深度大于临界深度时, Ti-6Al-4V合金疲劳寿命随表面粗糙度的增加而下降, 并且随着循环周次的增加, Ti-6Al-4V合金疲劳性能对表面粗糙度的敏感性下降. 随着表面粗糙度的增加, Ti-6Al-4V合金超高周疲劳裂纹的萌生方式发生变化. 超高周疲劳裂纹源有由一个向多个、由内部向次表面转移的趋势; 当表面凹痕深度增加到一定程度后, 在超高周疲劳寿命区间, Ti-6Al-4V合金疲劳寿命随粗糙度的增加而大幅下降. 疲劳裂纹全部从合金表面凹痕根部处萌生, 没有内部萌生的情况.
","authors":[{"authorName":"朱莉娜","id":"a03ad59d-9fd0-4dca-9946-f43d53c2faa6","originalAuthorName":"朱莉娜"},{"authorName":"邓彩艳","id":"e8a6e20e-3cc1-4973-b78e-5c7d712a3cc4","originalAuthorName":"邓彩艳"},{"authorName":"王东坡","id":"3fb64483-3fe9-4fac-a1cd-725f947bae53","originalAuthorName":"王东坡"},{"authorName":"胡绳荪","id":"57bd626e-a708-4e19-8b98-38a9324bd996","originalAuthorName":"胡绳荪"}],"categoryName":"Orginal Article","doi":"10.11900/0412.1961.2015.00511","fpage":"583","id":"edbb7f59-83c4-4f5d-a4c8-548f05e42eff","issue":"5","journal":{"abbrevTitle":"JSXB","coverImgSrc":"journal/img/cover/JSXB.jpg","id":"48","issnPpub":"0412-1961","publisherId":"JSXB","title":"金属学报"},"keywords":[{"id":"bcb00c0c-7a68-405e-b11c-49b30f35f1d4","keyword":"Ti-6Al-4V合金","originalKeyword":"Ti-6Al-4V合金"},{"id":"e043eaa7-a599-4c37-a5d9-2b7462ce829c","keyword":"超高周疲劳","originalKeyword":"超高周疲劳"},{"id":"2b5d23b2-e89b-455d-9363-7e61206889ff","keyword":"表面粗糙度","originalKeyword":"表面粗糙度"}],"language":"zh","publisherId":"C20150511","title":"表面粗糙度对Ti-6Al-4V合金超高周疲劳性能的影响*","volume":"52","year":"2016"},{"abstractinfo":"采用自行研制的超声疲劳实验装置,研究不同表面粗糙度下Ti-6Al-4V合金的超高周疲劳性能.结果表明,当表面凹痕宽深比a/c(a为凹痕宽度,c为凹痕深度)在2~10之间时,Ti-6Al-4V合金的临界凹痕深度在0.49~1.10 μm之间.当表面凹痕深度小于临界深度时,表面粗糙度对Ti-6Al-4V合金的超高周疲劳性能没有影响.当表面凹痕深度大于临界深度时,Ti-6Al-4V合金疲劳寿命随表面粗糙度的增加而下降,并且随着循环周次的增加,Ti-6Al-4V合金疲劳性能对表面粗糙度的敏感性下降.随着表面粗糙度的增加,Ti-6Al-4V合金超高周疲劳裂纹的萌生方式发生变化.超高周疲劳裂纹源有由一个向多个、由内部向次表面转移的趋势;当表面凹痕深度增加到一定程度后,在超高周疲劳寿命区间,Ti-6Al-4V合金疲劳寿命随粗糙度的增加而大幅下降.疲劳裂纹全部从合金表面凹痕根部处萌生,没有内部萌生的情况.","authors":[{"authorName":"朱莉娜","id":"31a8adc6-be30-4efb-ab67-8b1d9d77c79e","originalAuthorName":"朱莉娜"},{"authorName":"邓彩艳","id":"736593ec-ca56-4563-95f0-09dfe90c19f7","originalAuthorName":"邓彩艳"},{"authorName":"王东坡","id":"35baa12f-98ea-4dd9-b14e-e67523612cf8","originalAuthorName":"王东坡"},{"authorName":"胡绳荪","id":"115e3f58-592c-4f3f-9e7c-8138c4db8aef","originalAuthorName":"胡绳荪"}],"doi":"10.11900/0412.1961.2015.00511","fpage":"583","id":"139a221a-983b-4071-a9d8-76f27781c457","issue":"5","journal":{"abbrevTitle":"JSXB","coverImgSrc":"journal/img/cover/JSXB.jpg","id":"48","issnPpub":"0412-1961","publisherId":"JSXB","title":"金属学报"},"keywords":[{"id":"350197e5-9d21-41b5-8e2d-cd1d8192d1f7","keyword":"Ti-6Al-4V合金","originalKeyword":"Ti-6Al-4V合金"},{"id":"8da3839e-7991-4850-8e30-fe6809680c79","keyword":"超高周疲劳","originalKeyword":"超高周疲劳"},{"id":"6c0566d0-71f6-429e-9328-bc82a27b9ef6","keyword":"表面粗糙度","originalKeyword":"表面粗糙度"}],"language":"zh","publisherId":"jsxb201605009","title":"表面粗糙度对Ti-6Al-4V合金超高周疲劳性能的影响","volume":"52","year":"2016"},{"abstractinfo":"为研究除氢处理对置氢钛合金组织与性能的影响,对Ti-6Al-4V合金在不同参数条件下进行了置氢与除氢处理,采用光学显微镜分析了置氢-除氢处理过程中Ti-6Al-4V合金微观组织的演化规律,通过室温拉伸试验研究了置氢-除氢处理后Ti-6Al-4V合金的力学性能,探讨了Ti-6Al-4V合金置氢-除氢组织与力学性能之间的相关性.结果表明:Ti-6Al-4V合金置氢-除氢处理后,其微观组织与力学性能由置氢温度和氢的质量分数共同决定;氢质量分数为0.2%时,除氢后β相比例增加,材料的抗拉强度降低,而延伸率升高,延伸率最大增幅29.6%;氢质量分数为0.8%时,除氢后形成了魏氏组织,材料的强度升高,延伸率降低,抗拉强度最大提高100 MPa.","authors":[{"authorName":"王耀奇","id":"9a6f6165-db06-4c27-9060-f7c35f2bb9b1","originalAuthorName":"王耀奇"},{"authorName":"侯红亮","id":"c34482fa-64e0-4759-aaf7-428df6fd0d03","originalAuthorName":"侯红亮"},{"authorName":"李红","id":"26dbefed-0ea0-41cf-a7a1-7f4ae14d7504","originalAuthorName":"李红"}],"doi":"","fpage":"93","id":"d3e38fc2-47b5-4249-b29c-70039ddacb4c","issue":"3","journal":{"abbrevTitle":"CLKXYGY","coverImgSrc":"journal/img/cover/CLKXYGY.jpg","id":"14","issnPpub":"1005-0299","publisherId":"CLKXYGY","title":"材料科学与工艺"},"keywords":[{"id":"3feca644-b1af-470f-8ba5-f5b5425a1475","keyword":"Ti-6Al-4V合金","originalKeyword":"Ti-6Al-4V合金"},{"id":"d0b301b5-1d34-4bb0-909e-345d55d2ece1","keyword":"除氢","originalKeyword":"除氢"},{"id":"5cf05707-c697-47d2-8e67-6ade94546ae7","keyword":"微观组织","originalKeyword":"微观组织"},{"id":"dff26df4-dc87-4999-a5d7-d3ec14126744","keyword":"力学性能","originalKeyword":"力学性能"}],"language":"zh","publisherId":"clkxygy201103018","title":"TI-6Al-4V合金置氢-除氢组织与力学性能","volume":"19","year":"2011"},{"abstractinfo":"采用超声疲劳实验机分别确定了双态和网篮两种组织的Ti-6Al-4V合金在105~109周次范围内的疲劳寿命(S-N)曲线,并用扫描电镜观察疲劳断口,结果表明,这两种组织的Ti-6Al-4V合金的S-N曲线保持下降趋势,在105~109周次均没有水平段,都不存在传统意义的疲劳极限,在109时,双态组织的疲劳强度稍高于网篮组织;断口形貌分析表明,随着应力幅的降低,二者的断裂形式都发生了由表面到内部的转变。与加载频率为25Hz时的疲劳结果进行比较后发现,超声疲劳加载条件下,疲劳强度升高,疲劳寿命延长,且频率对网篮组织合金疲劳性能的影响大于对双态组织的影响。","authors":[{"authorName":"左景辉","id":"f6fec6ca-924d-4b10-adbe-61f0e82b0e34","originalAuthorName":"左景辉"},{"authorName":"王中光","id":"e505e6a3-18ef-4042-a163-6a76713adf4c","originalAuthorName":"王中光"},{"authorName":"韩恩厚","id":"a13c8d58-6601-41a3-b717-fec2aa07188e","originalAuthorName":"韩恩厚"}],"categoryName":"|","doi":"","fpage":"705","id":"aebc891c-429b-4699-8153-4298e20fdd29","issue":"7","journal":{"abbrevTitle":"JSXB","coverImgSrc":"journal/img/cover/JSXB.jpg","id":"48","issnPpub":"0412-1961","publisherId":"JSXB","title":"金属学报"},"keywords":[{"id":"3a11ab1f-0172-44ef-8c12-bce1b6df5583","keyword":"超高周疲劳","originalKeyword":"超高周疲劳"},{"id":"1bc27354-3b10-4f3b-ad97-06b04951c03a","keyword":"null","originalKeyword":"null"}],"language":"zh","publisherId":"0412-1961_2007_7_14","title":"Ti-6Al-4V合金的超高周疲劳行为","volume":"43","year":"2007"}],"totalpage":15230,"totalrecord":152295}