FSW of titanium alloys for aircraft engine components

被引:0
|
作者
Trapp, T [1 ]
Helder, E [1 ]
Subramanian, PR [1 ]
机构
[1] Edison Welding Inst, Columbus, OH 43221 USA
关键词
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper describes a USAF Metals Affordability Initiative Project being performed by GE Aircraft Engines and EWI to develop, demonstrate, and deploy friction stir welding (FSW) for joining titanium engine components. The overall goal of this project is to qualify FSW procedures for titanium alloy applications. Other goals included improved joint strength, production of welds that were free of tool debris, and reduced manufacturing cost and distortion. To achieve these goals, significant advancement in FSW tool design and materials were required. The project developed new FSW tool designs and materials, developed welding procedures for dissimilar titanium alloy combinations, and provided metallurgical and mechanical property data. This paper will provide a brief overview of the project and potential applications. The paper will discuss the FSW procedure development efforts, FSW microstructures and mechanical properties, as well as the effect of pre- and post-weld heat treatments on microstructure and properties.
引用
收藏
页码:173 / 178
页数:6
相关论文
共 50 条
  • [1] A new fixture for FSW processes of titanium alloys
    Fratini, L.
    Micari, F.
    Buffa, G.
    Ruisi, V. F.
    CIRP ANNALS-MANUFACTURING TECHNOLOGY, 2010, 59 (01) : 271 - 274
  • [2] Friction Stir Welding (FSW) of titanium alloys
    Laura, A.
    Rivista Italiana della Saldatura, 2009, 61 (03): : 291 - 303
  • [3] TITANIUM CASTINGS FOR AIRCRAFT COMPONENTS
    不详
    METALLURGIA AND METAL FORMING, 1975, 42 (02): : 34 - 34
  • [4] The influence of temperature on the wear mode and deterioration of coatings used for titanium aircraft engine components
    Freimanis, AJ
    Segall, AE
    Conway, JC
    Whitney, EJ
    TRIBOLOGY TRANSACTIONS, 2002, 45 (02) : 193 - 198
  • [5] PRODUCTION OF AIRCRAFT ENGINE COMPRESSOR ROTOR DISCS WITH DESIRED SERVICE LIFE IN TITANIUM ALLOYS
    Ermatchenko, A. G.
    Kashaev, R. M.
    MATERIALS PHYSICS AND MECHANICS, 2011, 11 (02): : 118 - 125
  • [6] On the characteristics of titanium alloys for the aircraft applications
    Singh, Paramjit
    Pungotra, Harish
    Kalsi, Nirmal S.
    MATERIALS TODAY-PROCEEDINGS, 2017, 4 (08) : 8971 - 8982
  • [7] Aircraft engine applications for gamma titanium aluminide
    Austin, CM
    Kelly, TJ
    McAllister, KG
    Chesnutt, JC
    STRUCTURAL INTERMETALLICS 1997, 1996, : 413 - 425
  • [8] Stability Assessment in Milling Aircraft Engine Components
    A. V. Martynyuk
    V. V. Kuritsyna
    M. V. Siluyanova
    Russian Engineering Research, 2024, 44 (7) : 990 - 993
  • [9] Precision heat treatment of aircraft engine components
    不详
    HEAT TREATMENT OF METALS, 2000, 27 (01): : 22 - 22
  • [10] Failure analysis of an aircraft piston engine components
    Turan, Dilek
    Karci, Adem
    ENGINEERING FAILURE ANALYSIS, 2009, 16 (04) : 1339 - 1345