| 查看: 992 | 回复: 3 | ||
casclzb金虫 (正式写手)
|
[求助]
15个金币求12th国际钛会的一篇文章的检索信息
|
|
2011年6月,在北京召开了第12届钛会,但至今没有收到论文集,现LZ以15个金币查询一篇文章的检索信息,论文信息如下: Zebao Lang, Xuhu Zhang, Jinliang SHI, Liang Wang, Wenjun JIa. Study on Production of Pre-alloyed Powders and Powder Metallurgy Proceeding of a Gamma Titanium Aluminide. 若得到该文章的EI或者SCI检索信息,作者以15个金币为酬谢,呵呵。前5位回帖但有有用信息的可拿到<5个金币的鼓励,谢谢啊! |
» 猜你喜欢
请问有评职称,把科研教学业绩算分排序的高校吗
已经有4人回复
孩子确诊有中度注意力缺陷
已经有12人回复
2025冷门绝学什么时候出结果
已经有3人回复
天津工业大学郑柳春团队欢迎化学化工、高分子化学或有机合成方向的博士生和硕士生加入
已经有4人回复
康复大学泰山学者周祺惠团队招收博士研究生
已经有6人回复
AI论文写作工具:是科研加速器还是学术作弊器?
已经有3人回复
2026博士申请-功能高分子,水凝胶方向
已经有6人回复
论文投稿,期刊推荐
已经有4人回复
硕士和导师闹得不愉快
已经有13人回复
请问2026国家基金面上项目会启动申2停1吗
已经有5人回复
» 本主题相关价值贴推荐,对您同样有帮助:
20金币求一篇文章
已经有5人回复
分享一篇用namd2做模拟来解释二甲基化的文章
已经有5人回复
中国争夺稀土定价权 整合政策引发国际争议
已经有4人回复
【资源】2010年诺 贝 尔 物理奖得主最经典的10篇文章全下载(被引次数高达上万次)
已经有26人回复
求下列三篇文章被引用情况的检索页
已经有6人回复
【分享】神经计算、机器学习最好会议之一的nips历年(1987-2008)文章免费下载
已经有50人回复

2楼2012-03-03 07:02:07
hnwl
木虫 (著名写手)
- 应助: 12 (小学生)
- 金币: 3080.2
- 散金: 3148
- 红花: 4
- 沙发: 1
- 帖子: 2479
- 在线: 248.7小时
- 虫号: 1342115
- 注册: 2011-07-10
- 性别: GG
- 专业: 计算机应用技术
【答案】应助回帖
★
感谢参与,应助指数 +1
casclzb(金币+1): 2012-03-03 15:23:25
感谢参与,应助指数 +1
casclzb(金币+1): 2012-03-03 15:23:25
|
可以通过如下EI查询入口查询: http://www.engineeringvillage2.org/ Username :utmshah Password :utmshah |
3楼2012-03-03 09:52:45
nandehutu9327
至尊木虫 (职业作家)
- CE-EPI: 1
- 应助: 279 (大学生)
- 金币: 18121.7
- 散金: 780
- 红花: 5
- 沙发: 2
- 帖子: 4555
- 在线: 590.4小时
- 虫号: 784367
- 注册: 2009-06-01
- 性别: GG
- 专业: 控制理论与方法
【答案】应助回帖
★
感谢参与,应助指数 +1
casclzb(金币+1): 2012-03-03 15:23:50
感谢参与,应助指数 +1
casclzb(金币+1): 2012-03-03 15:23:50
|
只见到一篇。 Accession number: 20102513015887 Title: Study on microstructures and properties and near-net-shape process of powder metallurgy heat resistant titanium alloy Authors: Liang, Wang1 ; Hongjun, Lv1 ; Zebao, Lang1 ; Gang, Shi1 ; Yanqing, Jiang1 ; Caogen, Yao1 Author affiliation: 1 Aerospace Research Institute of Material and Processing Technology, China Box 9211, Beijing, 100076, China Corresponding author: Liang, W. (wliangsn@sina.com) Source title: 60th International Astronautical Congress 2009, IAC 2009 Abbreviated source title: Int. Astronaut. Cong., IAC Volume: 7 Monograph title: 60th International Astronautical Congress 2009, IAC 2009 Issue date: 2009 Publication year: 2009 Pages: 5915-5923 Language: English ISBN-13: 9781615679089 Document type: Conference article (CA) Conference name: 60th International Astronautical Congress 2009, IAC 2009 Conference date: October 12, 2009 - October 16, 2009 Conference location: Daejeon, Korea, Republic of Conference code: 80592 Publisher: International Astronautical Federation, IAF, 94bis Avenue de Suffren, Paris, 75015, France Abstract: The prealloyed powder metallurgy (PM) process is studied in this paper to prepare PM TC11 (Ti-6.5Al-3.5Mo-l.5Zr-0.3Si) alloy, which is a kind of heat resistant titanium alloy. And HIP technology and PREP powders are used in the prealloyed processing to get full density material. Heat treatments are studied to optimize the micro structures and properties of the PM TCI 1 alloy. The micro structures are examined by optical microscope, and the morphologies of PREP powders are observed by SEM. Room temperature and high temperature (550°C) tensile properties (including ultimate tensile strength, yield strength, elongation and reduction of area) and elastic modulus of PM TCI 1 alloy are tested and discussed. The micro structures and properties of the PM TCI 1 alloy are compared with that of the same batch forged rod. Near-Net-Shape processes are studied to fabricate PM TC11 parts. By using of special dies, a big dimension thin wall integrity PM TC11 alloy spacecraft cabin with inner gridding stiffening ribs is near-net-shaped and no inner defect is detected. The results show that the PM TC11 alloy has same good tensile properties as forged material and plus perfect elastic modulus. The micro structures of the PM TC11 alloy are fine and uniform and the typical ones are basket weave structures surrounded by equiaxed a. The PM TCI 1 alloy and suitable near-net-shape process can be used in the field of fabricating high performance-to-cost, high reliability, lightweight and heat resistant parts for spacecrafts. Number of references: 17 Main heading: Titanium alloys Controlled terms: Alloys - Aluminum powder metallurgy - Cerium alloys - Elastic moduli - Heat treatment - Spacecraft - Structural properties - Tensile strength - Titanium - Weaving - Zirconium Uncontrolled terms: Big dimension - Forged materials - Gridding - Heat resistant - Heat-resistant titanium alloys - High reliability - High temperature - Inner defects - Near-net-shape - Optical microscopes - Pre-alloyed powder - Reduction of areas - Room temperature - SEM - Stiffening ribs - TC11 alloy - Thin walls - Ultimate tensile strength - Weave structures - Yield strength Classification code: 951 Materials Science - 541.1 Aluminum - 542.3 Titanium and Alloys - 547.2 Rare Earth Metals - 549.3 Nonferrous Metals and Alloys excluding Alkali and Alkaline Earth Metals - 655.1 Spacecraft, General - 819.5 Textile Products and Processing - 537.1 Heat Treatment Processes - 531.1 Metallurgy - 422.2 Strength of Building Materials : Test Methods - 422 Strength of Building Materials; Test Equipment and Methods - 421 Strength of Building Materials; Mechanical Properties - 408 Structural Design - 536 Powder Metallurgy Database: Compendex Compilation and indexing terms, © 2011 Elsevier Inc. |
4楼2012-03-03 11:41:15














回复此楼