{"currentpage":1,"firstResult":0,"maxresult":10,"pagecode":5,"pageindex":{"endPagecode":5,"startPagecode":1},"records":[{"abstractinfo":"叙述了现行工艺<span style=\"color:red\">模锻</span>的GH4133B合金<span style=\"color:red\">精</span><span style=\"color:red\">化</span><span style=\"color:red\">模锻件</span>的性能和组织特点;叙述了直接时效、添加预备热处理<span style=\"color:red\">精</span><span style=\"color:red\">化</span><span style=\"color:red\">模锻件</span>的性能和组织特点.叙述了标准热处理固溶加热温度与<span style=\"color:red\">精</span><span style=\"color:red\">化</span><span style=\"color:red\">模锻件</span>组织和性能的关系.","authors":[{"authorName":"刘公安","id":"d5cc3013-8e91-483f-840f-c987b3d89cda","originalAuthorName":"刘公安"},{"authorName":"王月乔","id":"a4dc7d1f-b86a-4cd0-b4d6-44288384b849","originalAuthorName":"王月乔"}],"doi":"10.3969/j.issn.1005-5053.2003.z1.015","fpage":"66","id":"d7bc16e5-e8f3-433e-a01c-ee5fd4a2d6d9","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":"6a0e8b17-bb78-4b41-9d78-5e21672cb310","keyword":"GH4133B合金","originalKeyword":"GH4133B合金"},{"id":"d7d18ad5-4c1c-45a8-819a-2d921afdc219","keyword":"<span style=\"color:red\">精</span><span style=\"color:red\">化</span><span style=\"color:red\">模锻件</span>","originalKeyword":"精化模锻件"},{"id":"30681512-4354-4bc3-9df1-083a7f32fe71","keyword":"直接时效","originalKeyword":"直接时效"},{"id":"43fb62a4-aab7-4b75-b2f8-7d192d0435ac","keyword":"预备热处理","originalKeyword":"预备热处理"},{"id":"4e24f341-dbe7-4bc2-a5c1-89d0cff2118e","keyword":"固溶","originalKeyword":"固溶"},{"id":"99797e6c-f0ee-4df5-8af5-508cca2b9097","keyword":"机械性能","originalKeyword":"机械性能"}],"language":"zh","publisherId":"hkclxb2003z1015","title":"GH4133B合金<span style=\"color:red\">精</span><span style=\"color:red\">化</span><span style=\"color:red\">模锻件</span>的性能及工艺控制","volume":"23","year":"2003"},{"abstractinfo":"叙述了用于WP-13发动机的GH4133B合金<span style=\"color:red\">模锻件</span>中形成的低倍粗晶粒与<span style=\"color:red\">模锻</span>工艺的关系;探讨了防止形成低倍粗晶粒的预备热处理工艺及<span style=\"color:red\">模锻</span>工艺的关键参数.","authors":[{"authorName":"刘公安","id":"450d8492-b78d-45b3-9e28-4961f4e0eb3e","originalAuthorName":"刘公安"},{"authorName":"王月乔","id":"6c2ad7d8-554e-4a6e-bf51-6e756c471a51","originalAuthorName":"王月乔"}],"doi":"","fpage":"81","id":"a30675c4-e3ab-4950-a685-1e314922c1e7","issue":"z1","journal":{"abbrevTitle":"GTYJXB","coverImgSrc":"journal/img/cover/GTYJXB.jpg","id":"30","issnPpub":"1001-0963","publisherId":"GTYJXB","title":"钢铁研究学报"},"keywords":[{"id":"eab5ab0c-29a7-40e8-b0df-553ff10a30c5","keyword":"GH4133B合金","originalKeyword":"GH4133B合金"},{"id":"829df21c-e7e6-4fad-862d-62fff80d85b2","keyword":"<span style=\"color:red\">模锻件</span>","originalKeyword":"模锻件"},{"id":"3ae801f9-86cb-46f9-af50-77fa8802e027","keyword":"粗晶粒","originalKeyword":"粗晶粒"}],"language":"zh","publisherId":"gtyjxb2003z1019","title":"GH4133B合金<span style=\"color:red\">精</span><span style=\"color:red\">化</span><span style=\"color:red\">模锻件</span>的低倍粗晶粒","volume":"15","year":"2003"},{"abstractinfo":"从等温锻造的低变形抗力、高的延伸率,变形均匀,工艺参数的可控性明显提高等方面阐述了等温锻造<span style=\"color:red\">精</span><span style=\"color:red\">化</span><span style=\"color:red\">锻件</span>的原理,分析了等温锻造技术的经济效益,介绍了等温锻造的典型精密<span style=\"color:red\">锻件</span>.","authors":[{"authorName":"庞克昌","id":"f9ad3976-7982-4e13-ad15-c4a0812dc93d","originalAuthorName":"庞克昌"}],"doi":"10.3321/j.issn:0412-1961.2002.z1.108","fpage":"356","id":"748b1dfe-9bc2-4c88-ab4b-1587bc487b91","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":"298388d1-ebd2-4fec-9cca-75ff24e2f7ca","keyword":"等温锻造","originalKeyword":"等温锻造"},{"id":"c61bd197-08c5-41ce-a7e1-529fc8e84236","keyword":"航空<span style=\"color:red\">锻件</span>","originalKeyword":"航空锻件"},{"id":"3f08f703-dbbc-49fc-bcb8-82777b5bf8e1","keyword":"<span style=\"color:red\">锻件</span><span style=\"color:red\">精</span><span style=\"color:red\">化</span>","originalKeyword":"锻件精化"}],"language":"zh","publisherId":"jsxb2002z1108","title":"航空<span style=\"color:red\">锻件</span><span style=\"color:red\">精</span><span style=\"color:red\">化</span>的重要途径-等温锻造技术","volume":"38","year":"2002"},{"abstractinfo":"钛合金飞机隔框件往往具有窄筋薄腹板等非对称特殊复杂形状,非常适合于进行近无余量精密体积成形.本研究采用等温精密<span style=\"color:red\">模锻</span>工艺成功地试制出了Ti-1023合金大型隔框<span style=\"color:red\">锻件</span>,<span style=\"color:red\">锻件</span>成形质量良好,形状尺寸大为<span style=\"color:red\">精</span><span style=\"color:red\">化</span>,可节约大量贵重原材料和机加工工时.<span style=\"color:red\">锻件</span>流线沿外形合理分布,显微组织细小均匀,力学性能优异.以钛代钢,零件减重约40%.","authors":[{"authorName":"郭鸿镇","id":"587a0adb-9527-4216-8831-b2362354a5a3","originalAuthorName":"郭鸿镇"},{"authorName":"姚泽坤","id":"b9c9d780-a44b-4d37-83cb-08bc6301a9c1","originalAuthorName":"姚泽坤"},{"authorName":"苏祖武","id":"22e52b3d-ce04-4ce2-b513-e0d25d70f2e7","originalAuthorName":"苏祖武"},{"authorName":"虢迎光","id":"3e44b084-71a7-41c6-b3e9-d81da76b9e6b","originalAuthorName":"虢迎光"},{"authorName":"苏梅英","id":"e23f5692-612b-42f1-a6ab-69d8dc172ec2","originalAuthorName":"苏梅英"},{"authorName":"骆兴正","id":"57d9996b-c2ea-4eb0-9585-ddd4133bce21","originalAuthorName":"骆兴正"},{"authorName":"夏齐喻","id":"078e8ade-cecb-4115-a36d-44ad6af0f1c4","originalAuthorName":"夏齐喻"},{"authorName":"楼瑞祥","id":"25dd9fff-f104-4382-af7f-a11ed49b14b9","originalAuthorName":"楼瑞祥"},{"authorName":"武振林","id":"2f47773a-de71-4036-becc-16481cb7adf4","originalAuthorName":"武振林"},{"authorName":"谢宏","id":"4e7db1cf-27ff-44b4-a693-30fe4583e366","originalAuthorName":"谢宏"},{"authorName":"李园春","id":"ae9505f9-fc79-4e66-a1c7-c7e580f093b6","originalAuthorName":"李园春"},{"authorName":"杨洪涛","id":"0a9ea350-54fd-48a6-9e98-e5fc6469cb66","originalAuthorName":"杨洪涛"},{"authorName":"王家宣","id":"cecfe56d-5b92-4826-8564-093cf6f1020d","originalAuthorName":"王家宣"}],"doi":"10.3321/j.issn:0412-1961.2002.z1.112","fpage":"366","id":"062f5637-be6f-4c80-8415-c342f8e7f3ef","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":"f0574803-93ec-43af-845c-62ca452e2a25","keyword":"Ti-1023合金","originalKeyword":"Ti-1023合金"},{"id":"12721405-8732-4d99-8f5a-c008e88c86ad","keyword":"隔框","originalKeyword":"隔框"},{"id":"9daadef3-7807-4a3a-8ae5-d2dc9e043110","keyword":"等温精密<span style=\"color:red\">模锻</span>","originalKeyword":"等温精密模锻"},{"id":"027fbf17-6094-4e8c-a746-6ba266cd6c13","keyword":"热处理","originalKeyword":"热处理"}],"language":"zh","publisherId":"jsxb2002z1112","title":"大型钛合金隔框<span style=\"color:red\">锻件</span>等温精密<span style=\"color:red\">模锻</span>试制研究","volume":"38","year":"2002"},{"abstractinfo":"通过对AZ80变形镁合金的<span style=\"color:red\">模锻</span>坯料进行挤压比为4的预挤压处理.研究挤压预变形对AZ80<span style=\"color:red\">模锻件</span>的组织和力学性能的影响.结果表明,预挤压处理的<span style=\"color:red\">模锻</span>样品时效时,以晶界颗粒状连续析出β相为主,而铸锭直接<span style=\"color:red\">模锻</span>的β相时效析出,则以品内大量层片状不连续析出为主.经过挤压预变形的AZ80<span style=\"color:red\">模锻件</span>相比铸锭直接<span style=\"color:red\">模锻件</span>.其<span style=\"color:red\">模锻</span>态和T5态的抗拉强度、伸长率得到明显提高,屈服强度变化不明显,脆性断裂明显减少,出现大量韧窝.","authors":[{"authorName":"王振","id":"3d577ce5-f5a3-48da-9f07-f45dd4170c53","originalAuthorName":"王振"},{"authorName":"朱秀荣","id":"a1bf5951-cea4-44dd-8b50-6b9b1072d50b","originalAuthorName":"朱秀荣"},{"authorName":"王荣","id":"f8ca059a-7073-4fff-b4ac-b5f9e159456d","originalAuthorName":"王荣"},{"authorName":"龚朝辉","id":"b80604f5-322f-4fa5-8ef3-1d2d0623569f","originalAuthorName":"龚朝辉"}],"doi":"10.3969/j.issn.1004-244X.2011.02.024","fpage":"80","id":"90fefae8-6f78-41af-bc75-97ec6d30765e","issue":"2","journal":{"abbrevTitle":"BQCLKXYGC","coverImgSrc":"journal/img/cover/BQCLKXYGC.jpg","id":"4","issnPpub":"1004-244X","publisherId":"BQCLKXYGC","title":"兵器材料科学与工程   "},"keywords":[{"id":"ae4bc396-5469-4674-b92d-19d5ea548307","keyword":"镁合金","originalKeyword":"镁合金"},{"id":"dec8dc81-d7ab-465e-854f-4044377e80fd","keyword":"挤压","originalKeyword":"挤压"},{"id":"ac21510f-6de9-477c-9e56-770fd72d1f7a","keyword":"锻造","originalKeyword":"锻造"},{"id":"d8878790-5619-404f-940e-96807fa7b4d0","keyword":"微观结构","originalKeyword":"微观结构"}],"language":"zh","publisherId":"bqclkxygc201102024","title":"预挤压对AZ80<span style=\"color:red\">模锻件</span>的组织和力学性能的影响","volume":"34","year":"2011"},{"abstractinfo":"开展了新型7085铝合金材料高温拉伸试验,得到了其基本性能参数与力学模型,运用ABAQUS有限元软件对7085铝合金框梁结构航空<span style=\"color:red\">模锻件</span>淬火过程进行了数值仿真,研究了淬火工艺参数与方式对残余应力分布规律的影响.研究表明:框梁结构航空<span style=\"color:red\">模锻件</span>淬火残余应力主要集中于腹板与筋板交汇处,呈现外压内拉的分布特点；淬火温度对残余应力有显著影响,提高淬火温度可有效降低残余应力；固溶温度对淬火残余应力的影响较小,对于大尺寸框梁<span style=\"color:red\">模锻件</span>,入水方式及转移时间对淬火残余应力的影响甚微.","authors":[{"authorName":"王少辉","id":"694912cc-893d-45de-9e73-fce7fd68da53","originalAuthorName":"王少辉"},{"authorName":"易幼平","id":"1cc9ece4-0204-4b5d-be43-7ea2d7aa5f5b","originalAuthorName":"易幼平"},{"authorName":"黄始全","id":"9b3cff2f-f742-468c-8652-35184fe13ff3","originalAuthorName":"黄始全"},{"authorName":"廖国防","id":"35be5c43-19cd-442c-bcc4-495c40f96f33","originalAuthorName":"廖国防"}],"doi":"10.3969/j.issn.1007-2330.2011.04.021","fpage":"85","id":"2d89b1c1-f8b8-4a80-af40-7314d0deae43","issue":"4","journal":{"abbrevTitle":"YHCLGY","coverImgSrc":"journal/img/cover/YHCLGY.jpg","id":"77","issnPpub":"1007-2330","publisherId":"YHCLGY","title":"宇航材料工艺   "},"keywords":[{"id":"10cfd244-277f-4fb0-865a-6f1495d5c337","keyword":"7085铝合金","originalKeyword":"7085铝合金"},{"id":"a91d3299-1fe9-4eba-93d5-9bef603bd735","keyword":"框梁<span style=\"color:red\">模锻件</span>","originalKeyword":"框梁模锻件"},{"id":"c5a26a21-c18d-464c-9080-27e677c62fb1","keyword":"淬火残余应力","originalKeyword":"淬火残余应力"},{"id":"e16d71c5-4549-4185-a233-55e761230de1","keyword":"有限元","originalKeyword":"有限元"}],"language":"zh","publisherId":"yhclgy201104021","title":"大型铝合金框梁结构航空<span style=\"color:red\">模锻件</span>淬火残余应力分析","volume":"41","year":"2011"},{"abstractinfo":"利用Gleeble-1500热模拟试验机对300M超高强钢进行了热压缩试验,建立了材料流变应力模型；采用DEFORM 3D有限元软件对300M超高强钢起落架外筒<span style=\"color:red\">模锻件</span>锤锻成型过程进行了数值模拟,研究了不同工艺参数对<span style=\"color:red\">锻件</span>成型的影响.结果表明:<span style=\"color:red\">模锻件</span>在1100℃始锻温度下,经三火成型填充完全,<span style=\"color:red\">锻件</span>平均应力228 MPa,平均应变1.51.","authors":[{"authorName":"代伟","id":"2c8cb883-cdc6-49f6-8f24-37d811bfc1b3","originalAuthorName":"代伟"},{"authorName":"易幼平","id":"aecc92d0-7a0b-4740-844e-6b105808e02d","originalAuthorName":"易幼平"},{"authorName":"李蓬川","id":"e953dd5a-2081-4acd-9b75-8aa4041286bc","originalAuthorName":"李蓬川"},{"authorName":"陈春","id":"992776c6-b03e-431e-ba23-c34224b37bbd","originalAuthorName":"陈春"}],"doi":"","fpage":"100","id":"2d3e38eb-72a0-4afb-8fa4-9f8211d87a4a","issue":"6","journal":{"abbrevTitle":"YHCLGY","coverImgSrc":"journal/img/cover/YHCLGY.jpg","id":"77","issnPpub":"1007-2330","publisherId":"YHCLGY","title":"宇航材料工艺   "},"keywords":[{"id":"c05f6e57-b181-402f-b2d0-a67f49811435","keyword":"300M超高强钢","originalKeyword":"300M超高强钢"},{"id":"c4f0e950-9823-4605-bff1-bd538a32938e","keyword":"流变应力模型","originalKeyword":"流变应力模型"},{"id":"507cd34f-9c4e-4988-9bf4-2cec9492b8aa","keyword":"数值模拟","originalKeyword":"数值模拟"}],"language":"zh","publisherId":"yhclgy201206021","title":"300M超高强钢起落架外筒<span style=\"color:red\">模锻件</span>锤锻工艺","volume":"42","year":"2012"},{"abstractinfo":"采用相同规格 TA15棒材分别利用800MN <span style=\"color:red\">模锻</span>压力机、1 MJ 对击<span style=\"color:red\">模锻</span>锤制备同种形状钛合金大型航空<span style=\"color:red\">模锻件</span>，对两种<span style=\"color:red\">模锻</span>条件下的<span style=\"color:red\">锻件</span>组织及力学性能进行了对比研究。结果表明：800MN 制备的<span style=\"color:red\">锻件</span>塑性流线分布好，每火次变形量大、变形速率低，比1 MJ <span style=\"color:red\">锻件</span>再结晶晶粒尺寸小、等轴初生α相比例高且颗粒更加细小，室温、500℃高温拉伸性能以及冲击韧性和断裂韧性均有所提高。","authors":[{"authorName":"王卫红","id":"35216d2c-74be-42bb-8b3b-47a37ad65304","originalAuthorName":"王卫红"}],"doi":"10.11868/j.issn.1005-5053.2015.3.005","fpage":"24","id":"e91446d2-a6fe-428f-bfa0-47c79894b302","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":"698da214-6d4f-4cd8-997a-636071f60dc3","keyword":"800MN压力机","originalKeyword":"800MN压力机"},{"id":"53e2dde2-b818-4145-a2ef-fb8289ce0953","keyword":"1MJ对击锤","originalKeyword":"1MJ对击锤"},{"id":"be8f6b82-774c-49f9-a336-2f69e60ac0ce","keyword":"TA15钛合金","originalKeyword":"TA15钛合金"},{"id":"6315df02-b6b7-4cd6-9df5-45bc00282e20","keyword":"大型航空<span style=\"color:red\">锻件</span>","originalKeyword":"大型航空锻件"}],"language":"zh","publisherId":"hkclxb201503005","title":"TA15钛合金大<span style=\"color:red\">锻件</span>两种<span style=\"color:red\">模锻</span>工艺的组织性能对比研究","volume":"","year":"2015"},{"abstractinfo":"采用锻后直接时效处理的方法研究了时效处理工艺对高强耐热镁合金等温<span style=\"color:red\">模锻件</span>的组织与性能的影响,分析了其时效强化过程中第二相的形成及时效处理制度相关的断裂行为,得出了其时效强化的内在机理及优化的锻后时效制度.研究表明优化的时效处理制度为200℃×63 h.在该时效制度下,材料的室温抗拉强度达到了371MPa,屈服强度达到243 MPa,伸长率达4.1％","authors":[{"authorName":"张浩","id":"d1f57a1c-ff3d-4655-8e85-c28fe4d55ddc","originalAuthorName":"张浩"},{"authorName":"杜志惠","id":"67f11a45-9478-475f-937b-c0b46fd533f5","originalAuthorName":"杜志惠"},{"authorName":"谢飞","id":"fff780ee-f9b2-4c59-a6af-9c23095101bd","originalAuthorName":"谢飞"},{"authorName":"周晓建","id":"6dcf50a5-93c9-4bed-9736-de2c556bcddd","originalAuthorName":"周晓建"},{"authorName":"单德彬","id":"81ece7e3-3ffd-4cc4-bf03-80bbd59cc05d","originalAuthorName":"单德彬"}],"doi":"10.3969/j.issn.1007-2330.2012.01.012","fpage":"54","id":"9953cd06-8ae1-47f7-bae1-2ed6122dd4fc","issue":"1","journal":{"abbrevTitle":"YHCLGY","coverImgSrc":"journal/img/cover/YHCLGY.jpg","id":"77","issnPpub":"1007-2330","publisherId":"YHCLGY","title":"宇航材料工艺   "},"keywords":[{"id":"e4c460ea-95ce-4af3-a95e-612a1163f7ba","keyword":"镁合金","originalKeyword":"镁合金"},{"id":"75a0558e-e3aa-441b-9f46-cbc797310b13","keyword":"等温成形","originalKeyword":"等温成形"},{"id":"2328bffa-1d01-4a43-8adf-ea9b0648ba63","keyword":"时效处理","originalKeyword":"时效处理"},{"id":"491f1210-b7cd-45ba-9068-9647b1978cae","keyword":"力学性能","originalKeyword":"力学性能"}],"language":"zh","publisherId":"yhclgy201201012","title":"时效处理对高强耐热镁合金等温<span style=\"color:red\">模锻件</span>组织与性能的影响","volume":"42","year":"2012"},{"abstractinfo":"针对实际生产中TC18钛合金<span style=\"color:red\">模锻件</span>存在的成形难和组织、性能不稳定的问题，对<span style=\"color:red\">锻件</span>分模面位置和结构进行了调整，并进行实验验证。结果表明，采用顶部分模方式可以大大改善金属的流动性，减少锻造火次，提高生产效率，同时<span style=\"color:red\">锻件</span>组织较采用中间分模得到的更加均匀，强度和断裂韧性得到了提高，塑性也保持了较高的水平，具有良好的综合性能。","authors":[{"authorName":"王华","id":"b953e2c1-40cd-4309-97c3-9623b6d0b4fe","originalAuthorName":"王华"},{"authorName":"翟江波","id":"d17f7e1f-fccd-48ea-9dba-34eaa04ad6d6","originalAuthorName":"翟江波"}],"doi":"","fpage":"28","id":"368bd6a2-5451-4e52-b615-35265722cc05","issue":"4","journal":{"abbrevTitle":"TGYJZ","coverImgSrc":"journal/img/cover/TGYJZ.jpg","id":"60","issnPpub":"1009-9964","publisherId":"TGYJZ","title":"钛工业进展"},"keywords":[{"id":"8c499392-a558-4546-aa54-de236bcfc87e","keyword":"TC18钛合金","originalKeyword":"TC18钛合金"},{"id":"f99cc66d-1a40-4b4f-9002-8f4a6b9d8562","keyword":"<span style=\"color:red\">模锻</span>","originalKeyword":"模锻"},{"id":"43d03bea-35b7-4791-b51d-f343b1ce6816","keyword":"分模面","originalKeyword":"分模面"},{"id":"56cd6561-62db-4159-a740-e059ace67025","keyword":"力学性能","originalKeyword":"力学性能"}],"language":"zh","publisherId":"tgyjz201404011","title":"分模方式对 TC18钛合金<span style=\"color:red\">模锻件</span>组织及力学性能的影响","volume":"","year":"2014"}],"totalpage":2655,"totalrecord":26544}