{"currentpage":1,"firstResult":0,"maxresult":10,"pagecode":5,"pageindex":{"endPagecode":5,"startPagecode":1},"records":[{"abstractinfo":"采用浸泡腐蚀和电化学腐蚀试验研究了等通道转角挤压制备的超细晶ZL203合金的晶间腐蚀行为.结果表明:等通道转角挤压细化了合金的显微组织,同时也显著降低了合金晶间腐蚀敏感性;合金晶间腐蚀敏感性降低的原因一是θ相网状结构的破碎打断了晶间腐蚀扩展通道,二是变形α-Al基体氧化膜耐蚀性能的提高.","authors":[{"authorName":"宋丹","id":"64b8b49a-508b-4fb4-8a97-75fba4c553e9","originalAuthorName":"宋丹"},{"authorName":"马爱斌","id":"bbbaba6b-f8c7-4dae-9d47-a05107b79785","originalAuthorName":"马爱斌"},{"authorName":"江静华","id":"f6fd41ae-ac16-4e60-8c68-dfcbf191a978","originalAuthorName":"江静华"},{"authorName":"林萍华","id":"bcb32c5e-aa2f-4fce-a571-5a277fe7b6fc","originalAuthorName":"林萍华"},{"authorName":"范俊峰","id":"05885898-41b7-40dd-a58e-d988b2225ac9","originalAuthorName":"范俊峰"},{"authorName":"杨东辉","id":"581e510d-7e59-424e-8273-beb0740bbf1b","originalAuthorName":"杨东辉"}],"doi":"","fpage":"27","id":"fe509753-0a9a-4842-9607-b81cf4b9e05d","issue":"3","journal":{"abbrevTitle":"JXGCCL","coverImgSrc":"journal/img/cover/JXGCCL.jpg","id":"45","issnPpub":"1000-3738","publisherId":"JXGCCL","title":"机械工程材料"},"keywords":[{"id":"86ae7765-b041-43dd-920f-61bb926386fe","keyword":"等通道转角挤压","originalKeyword":"等通道转角挤压"},{"id":"cf3e5101-2867-4302-ae12-e8c1afefd2a4","keyword":"ZL203合金","originalKeyword":"ZL203合金"},{"id":"897174a9-09a9-4a01-aff3-0d709d81d359","keyword":"超细晶","originalKeyword":"超细晶"},{"id":"65d83141-ae06-4a76-8675-533764731047","keyword":"晶间腐蚀","originalKeyword":"晶间腐蚀"}],"language":"zh","publisherId":"jxgccl201003008","title":"等通道转角挤压超细晶ZL203合金的晶间腐蚀行为","volume":"34","year":"2010"},{"abstractinfo":"采用混合盐反应法原位合成TiB2颗粒制备了ZL203基复合材料,研究了不同载荷条件下复合材料的干摩擦磨损行为。结果表明:该复合材料中的TiB2颗粒分布较均匀,平均尺寸约为500nm与基体材料相比,复合材料的力学性能和耐磨性明显提高,延缓了高载荷条件下严重磨损的发生,复合材料摩擦表面形成了一层致密的机械混合层,对复合材料具有很好的保护作用。","authors":[{"authorName":"张磊","id":"9fdf3a82-56d2-41e2-b258-5943298fbfab","originalAuthorName":"张磊"},{"authorName":"邱辉","id":"97e57916-6216-4fc3-a85b-cd39d2f4d160","originalAuthorName":"邱辉"},{"authorName":"尧军平","id":"aaaa22d9-1408-4294-8d9f-a9e75eb3f683","originalAuthorName":"尧军平"},{"authorName":"黄磊萍","id":"35e87a46-5583-4ad7-bb74-dd336705a145","originalAuthorName":"黄磊萍"},{"authorName":"蔡媛媛","id":"a87491a7-cb1a-405b-abd2-73dd1eea51c3","originalAuthorName":"蔡媛媛"}],"doi":"","fpage":"89","id":"21314df5-5a36-4d89-88aa-3d30e576cafb","issue":"11","journal":{"abbrevTitle":"JXGCCL","coverImgSrc":"journal/img/cover/JXGCCL.jpg","id":"45","issnPpub":"1000-3738","publisherId":"JXGCCL","title":"机械工程材料"},"keywords":[{"id":"bc679148-2397-47cd-8183-cab36b915266","keyword":"原位合成","originalKeyword":"原位合成"},{"id":"ece6ac8a-de9b-4740-8d7e-67bf2422c315","keyword":"复合材料","originalKeyword":"复合材料"},{"id":"52ae71e6-6d1d-4c1c-bfd7-df3a2b4d8f18","keyword":"TiB2颗粒","originalKeyword":"TiB2颗粒"},{"id":"06888be6-2c79-40ed-b30f-71e7d92efc6b","keyword":"机械混合层","originalKeyword":"机械混合层"},{"id":"695818b3-9667-4968-82fe-3f130b162fd6","keyword":"耐磨性能","originalKeyword":"耐磨性能"}],"language":"zh","publisherId":"jxgccl201111024","title":"原位合成TiB2颗粒增强ZL203基复合材料的摩擦磨损性能","volume":"35","year":"2011"},{"abstractinfo":"通过对ZL205A合金的成分、熔模精密铸造方法的分析;同时结合现场生产实践对ZL205A合金熔模铸造的工艺控制要点提出了看法.","authors":[{"authorName":"谭芳","id":"61af1735-fbe6-4817-89c1-0ec7f5a13cc0","originalAuthorName":"谭芳"},{"authorName":"陈治海","id":"761165a1-a5e3-4e9d-b188-a6b34bd17706","originalAuthorName":"陈治海"}],"doi":"10.3969/j.issn.1005-5053.2003.z1.025","fpage":"113","id":"80be9e5c-147b-4912-9169-18732e64839f","issue":"z1","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":"f39963c0-9004-4ba2-b527-3e0063caf249","keyword":"ZL205A合金","originalKeyword":"ZL205A合金"},{"id":"9e005897-f17c-4d52-bced-8f8089767d21","keyword":"熔模铸造","originalKeyword":"熔模铸造"},{"id":"e2670f03-8b8a-457b-adc6-37b3cb23ee21","keyword":"工艺","originalKeyword":"工艺"}],"language":"zh","publisherId":"hkclxb2003z1025","title":"ZL205A合金熔模铸造工艺研究","volume":"23","year":"2003"},{"abstractinfo":"研究ZL114A合金的拉伸性能和轴向应力疲劳行为(K1=1,R=-1).结果表明,ZL114A合金的疲劳性能与美国A357合金的疲劳性能相当.系统研究了L114A合金疲劳损伤特征,分析疏松、夹杂物等铸造缺陷在疲劳裂纹的形核、裂纹的扩展以及瞬断中所起的作用,表明铸造过程中形成的铸造缺陷数量、尺寸、位置对金属的疲劳性能都有不同程度的影响.","authors":[{"authorName":"周永江","id":"06992145-ddbf-4184-913e-8044e92cc4f4","originalAuthorName":"周永江"},{"authorName":"熊艳才","id":"9129aa16-3e6a-44f2-b513-d7513387d0fd","originalAuthorName":"熊艳才"},{"authorName":"洪润洲","id":"02f1a9c7-a601-4033-9dec-0434b1fc3c5f","originalAuthorName":"洪润洲"},{"authorName":"姚惟斌","id":"2fecd248-c5e4-4aaa-8822-d41025dc7d6b","originalAuthorName":"姚惟斌"},{"authorName":"张喆","id":"e968f751-26f2-4640-a845-e10bfef7fd7e","originalAuthorName":"张喆"}],"doi":"10.3969/j.issn.1005-5053.2007.04.003","fpage":"10","id":"1c7af45c-7c74-43a4-a3e3-3b0829d6fa62","issue":"4","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":"7640b90a-2c2e-4bd8-a0b3-b0d99216d3a2","keyword":"ZL114A合金","originalKeyword":"ZL114A合金"},{"id":"5fd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对ZL101合金的Sr变质效果与保温时间、 Sr含量及晶粒尺寸的关系进行了研究. 结果表明: ZL101共晶硅的Sr变质具有长效性, 且达到最佳变质效果前有一时间间隔;加入的Sr量有一临界值, 超过此值, 变质效果变化不明显; 若共晶硅越细小, 变质效果则越好, 达到最佳变质效果的时间也随之缩短. ","authors":[{"authorName":"张静武","id":"e9bc3eee-2f8f-4133-9eba-b17122270c09","originalAuthorName":"张静武"},{"authorName":"李慧","id":"4cf58181-97e1-42ec-b805-0131a1280e67","originalAuthorName":"李慧"},{"authorName":"孟显哲","id":"5d0dbca1-e794-4de0-8323-ef2f2923b364","originalAuthorName":"孟显哲"},{"authorName":"刘春海","id":"bbb5bfbb-64d0-49b8-811b-beb3ade47422","originalAuthorName":"刘春海"}],"doi":"","fpage":"91","id":"589d3a2d-7704-4268-979b-daef5661b029","issue":"z2","journal":{"abbrevTitle":"ZGYSJSXB","coverImgSrc":"journal/img/cover/ZGYSJSXB.jpg","id":"88","issnPpub":"1004-0609","publisherId":"ZGYSJSXB","title":"中国有色金属学报"},"keywords":[{"id":"064789f1-fe16-44e3-9304-de64cf227528","keyword":"ZL101合金","originalKeyword":"ZL101合金"},{"id":"dcdf7b07-b83b-422c-b398-f6678eba97e0","keyword":"变质处理","originalKeyword":"变质处理"},{"id":"b697ed6b-6846-41af-bb94-b3d338d36563","keyword":"TPRE机制","originalKeyword":"TPRE机制"},{"id":"6837000f-43ce-4c0d-a750-2d07193e235c","keyword":"晶粒细化","originalKeyword":"晶粒细化"}],"language":"zh","publisherId":"zgysjsxb2001z2020","title":"ZL101合金的变质","volume":"11","year":"2001"},{"abstractinfo":"采用不同的时效工艺,研究了时效温度和时间对ZL101A合金性能的影响,得出了该合金较理想的时效制度,在此制度下,ZL101A合金的金属型典型性能达到σb≥330MPa,δ5≥10%,为满足航空、航天等领域对高性能铝合金精密铸件的需求奠定了材料基础.","authors":[{"authorName":"洪润洲","id":"b39ccbef-fd3b-400e-87e0-bfcdeec28a2f","originalAuthorName":"洪润洲"},{"authorName":"周永江","id":"3e48dd5e-6596-4f83-8a4d-55cc76148fea","originalAuthorName":"周永江"},{"authorName":"姚惟斌","id":"e652ffd4-f3e7-43fc-98fe-cbc4b0a284b3","originalAuthorName":"姚惟斌"}],"doi":"10.3969/j.issn.1001-4381.2004.10.010","fpage":"39","id":"bbd74173-5c94-43dd-96a6-d3dfd40a1b9d","issue":"10","journal":{"abbrevTitle":"CLGC","coverImgSrc":"journal/img/cover/CLGC.jpg","id":"9","issnPpub":"1001-4381","publisherId":"CLGC","title":"材料工程"},"keywords":[{"id":"df8d8859-48fd-4a7d-bcdb-00dd83c19a74","keyword":"ZL101A合金","originalKeyword":"ZL101A合金"},{"id":"c2e0912b-e8f6-4c70-b53b-469d6af7b50f","keyword":"时效工艺","originalKeyword":"时效工艺"},{"id":"ee449b87-f827-44b9-b062-6436fc9fdd0a","keyword":"力学性能","originalKeyword":"力学性能"}],"language":"zh","publisherId":"clgc200410010","title":"时效工艺对ZL101A合金性能的影响","volume":"","year":"2004"},{"abstractinfo":"对铸态ZL401合金进行了低温人工时效处理,利用低频内耗测试技术研究了合金的阻尼性能及实模量与应变振幅、频率和温度的关系,并与铸态合金进行了对比.发现合金阻尼与应变振幅及应变频率相关,随温度的提高而增大,且在低温和高温时合金阻尼与频率的关系出现了相反的变化.ZL401合金振动过程中实模量的亏损随频率的降低和温度的升高而增大.认为ZL401合金的阻尼行为是界面阻尼和位错阻尼二者效应叠加的结果,室温阻尼主要归功于位错阻尼,而高温阻尼主要归功于界面阻尼.","authors":[{"authorName":"张忠明","id":"546c34be-50de-4bd0-ab73-83b3ca42b8a5","originalAuthorName":"张忠明"},{"authorName":"王锦程","id":"a9cc9350-7076-4c9a-a610-339d5bc7f440","originalAuthorName":"王锦程"},{"authorName":"郭学锋","id":"55c4a1be-4c86-4b94-aa99-16a0407473d5","originalAuthorName":"郭学锋"},{"authorName":"杨根仓","id":"39e15289-74af-4c13-b6ad-6d79a4f73554","originalAuthorName":"杨根仓"}],"doi":"10.3969/j.issn.1009-6264.2004.01.010","fpage":"36","id":"1718ce72-1beb-44bf-b429-d326c1be65b8","issue":"1","journal":{"abbrevTitle":"CLRCLXB","coverImgSrc":"journal/img/cover/CLRCLXB.jpg","id":"15","issnPpub":"1009-6264","publisherId":"CLRCLXB","title":"材料热处理学报"},"keywords":[{"id":"1e237498-6f41-421a-bbfa-bd27e7aefb86","keyword":"ZL401合金","originalKeyword":"ZL401合金"},{"id":"4d33ff9c-d434-45fe-96b5-13e242f7d761","keyword":"时效","originalKeyword":"时效"},{"id":"932f6c89-f6d4-4815-ace5-aa01309f86c2","keyword":"阻尼行为","originalKeyword":"阻尼行为"},{"id":"f49931dc-ef8c-4d8a-841b-d01551ce433f","keyword":"弹性模量","originalKeyword":"弹性模量"}],"language":"zh","publisherId":"jsrclxb200401010","title":"ZL401合金的阻尼行为研究","volume":"25","year":"2004"},{"abstractinfo":"本文综述了高强ZL205A合金铸造特性、成分和性能特点,介绍了该合金优质铸件在飞机、导弹等武器上的应用,对大飞机设计时选用ZL205A合金优质铸件提出几点体会.","authors":[{"authorName":"贾泮江","id":"55dfab00-dff1-41fc-820c-73403038acbd","originalAuthorName":"贾泮江"},{"authorName":"陈邦峰","id":"efb9d26e-4549-4845-b823-d502e37e852a","originalAuthorName":"陈邦峰"}],"doi":"10.3969/j.issn.1001-4381.2009.01.018","fpage":"77","id":"0dca7176-4bdc-42a9-9fe1-85bdd37e5d06","issue":"1","journal":{"abbrevTitle":"CLGC","coverImgSrc":"journal/img/cover/CLGC.jpg","id":"9","issnPpub":"1001-4381","publisherId":"CLGC","title":"材料工程"},"keywords":[{"id":"c2542577-00f7-436a-babc-e6758b137594","keyword":"高强度","originalKeyword":"高强度"},{"id":"c188341e-cf03-4436-9e04-7685345718ae","keyword":"ZL205A合金","originalKeyword":"ZL205A合金"},{"id":"78c76caa-7ea1-4f0b-b2d2-6bbf7f459a44","keyword":"优质铸件","originalKeyword":"优质铸件"}],"language":"zh","publisherId":"clgc200901018","title":"ZL205A合金高强优质铸件在大飞机上的应用","volume":"","year":"2009"},{"abstractinfo":"研究了ZL211A合金的铸造状态和热处理状态的组织和力学性能,进行了合金熔炼、铸造、热处理、力学性能测试、微观组织和拉伸断口形貌观察等试验.结果表明,ZL211A合金的铸态金相组织主要由α(Al)、CuAl2和T(Al12CuMn2)相组成,力学性能较低,不能满足航空结构材料的要求,必须经热处理强化后才能使用;热处理状态的金相组织主要由α(A1)、T(Al12 CuMn2)相、θ″相和θ′相组成,经过二级固溶处理再人工时效后,即在535℃±5℃,保温7h,再升温到545+3-5℃,保温7h,淬入50~60℃的热水中,然后在165℃±5℃人工时效7h,可获得优良的综合力学性能.ZL211A合金拉伸试样断口表现为延性断裂,其微观形貌均为韧窝和撕裂棱,韧窝的大小和深浅有所不同.","authors":[{"authorName":"刘国利","id":"8e68502c-56f6-4ad9-a7b6-45e0ca125c5b","originalAuthorName":"刘国利"},{"authorName":"戴圣龙","id":"eb453132-3d33-47a2-a64c-156e940c61dd","originalAuthorName":"戴圣龙"}],"doi":"10.3969/j.issn.1001-4381.2010.z1.067","fpage":"312","id":"68ccf9c1-03f3-42bd-963d-4150325043b8","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":"6dad63b7-d289-488f-bffe-5c65a9196d4a","keyword":"ZL211A","originalKeyword":"ZL211A"},{"id":"baaf790d-ca7d-492b-ae9f-2dc680c2bd5c","keyword":"铸造铝合金","originalKeyword":"铸造铝合金"},{"id":"5b0a2e34-98dc-490f-9de0-f069a3c70f7a","keyword":"热处理","originalKeyword":"热处理"},{"id":"84ca6120-da07-4951-9557-48ebb2dfc305","keyword":"微观组织","originalKeyword":"微观组织"},{"id":"803c4cf1-d131-42cf-84c6-ad9fd534d1e4","keyword":"力学性能","originalKeyword":"力学性能"}],"language":"zh","publisherId":"clgc2010z1067","title":"ZL211A合金组织与性能研究","volume":"","year":"2010"},{"abstractinfo":"摘要:采用粉末冶金法制备了Fe-12Cr-2.5W-0.4Ti-0.3Y203合金,研究了压制压力及烧结温度对烧结体组织与性能的影响。结果表明:铬、钨原子在高能球磨过程中未能完全固溶于α-Fe中,而在烧结过程中能实现完全固溶;压坯密度和抗弯强度随压制压力增大而增加,并在压力达到700MPa后趋于稳定;提高压制压力与烧结温度可提高烧结体抗拉强度,在压制压力700MPa,烧结温度1400℃的条件下,烧结体抗拉强度为416.7MPa,材料断裂方式为韧性断裂。","authors":[{"authorName":"姚振华","id":"5169bf53-2c16-4666-83b8-65947761df59","originalAuthorName":"姚振华"},{"authorName":"熊惟皓","id":"46858704-11b1-4563-b0df-1a8753810924","originalAuthorName":"熊惟皓"},{"authorName":"彭倩筠","id":"f5fb2901-5cc2-4f6d-97a9-0298c0d70ade","originalAuthorName":"彭倩筠"},{"authorName":"周敏","id":"907ad471-fcd9-4e75-95a1-46f7907e54f9","originalAuthorName":"周敏"}],"doi":"","fpage":"4","id":"ee2232f5-c1b2-4dcf-a580-1f0453071426","issue":"6","journal":{"abbrevTitle":"JXGCCL","coverImgSrc":"journal/img/cover/JXGCCL.jpg","id":"45","issnPpub":"1000-3738","publisherId":"JXGCCL","title":"机械工程材料"},"keywords":[{"id":"caf0f1d6-66c0-47b0-a547-a1db7166fdcc","keyword":"粉末冶金","originalKeyword":"粉末冶金"},{"id":"7689eb90-f243-4821-8246-5f44666b192b","keyword":"压制压力","originalKeyword":"压制压力"},{"id":"bae7f739-c968-4fd8-8ead-d7af02fbfc20","keyword":"烧结温度","originalKeyword":"烧结温度"},{"id":"98487e48-6e16-4e7a-943d-4a9a46237d73","keyword":"抗拉强度","originalKeyword":"抗拉强度"}],"language":"zh","publisherId":"jxgccl201106002","title":"压制压力及烧结温度对Fe-Cr-W-Ti-Y203合金组织与性能的影响","volume":"35","year":"2011"}],"totalpage":3900,"totalrecord":38994}