Repair of gas turbine engine components with laser powder deposition

被引:0
|
作者
Miller, S [1 ]
Heath, M [1 ]
Woods, B [1 ]
Costello, A [1 ]
Sears, J [1 ]
机构
[1] S Dakota Sch Mines & Technol, Dept Mech Engn, Rapid City, SD 57701 USA
关键词
lasers; deposition; metal powder; repair; Gas Turbine Engines (GTE);
D O I
暂无
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Laser Powder Deposition (LPD) for component repair offers some unique solutions for Gas Turbine Engine applications. LPD is a CAD/CAM solid freeform fabrication technology that uses metal powder and laser fusion to repair components. Inherent to LPD is the ability to add material for repair of critical GTE components with minimal heat affect to the under lying material. Also, due to the nature of LPD, hard coatings can be achieved without heat treatment allowing for repair of heat-treated steels. In some cases LPD repair can be used to replace hard chrome or carburized surfaces. Details of several GTE components that have been repaired will be disclosed.
引用
收藏
页码:333 / 339
页数:7
相关论文
共 50 条
  • [31] Braze repair of gas turbine components: Retrospective, perspective, prospective
    O'Neill, WM
    Kennedy, A
    HEAT TREATING, VOLS 1 AND 2, PROCEEDINGS, 2000, : 1040 - 1045
  • [32] Single crystal metal deposition using laser additive manufacturing technology for repair of aero-engine components
    Kumar, S. Anand
    Rajkumar, V
    Nagesha, B. K.
    Tigga, Amit Kumar
    Barad, Sanjay
    Suresh, T. N.
    MATERIALS TODAY-PROCEEDINGS, 2021, 45 : 5395 - 5399
  • [33] Automated health management for gas turbine engine accessory system components
    Byington, Carl S.
    Watson, Matthew J.
    Bharadwaj, Sudarshan P.
    2008 IEEE AEROSPACE CONFERENCE, VOLS 1-9, 2008, : 3691 - 3702
  • [34] A BEARING DEPOSITION TEST FOR EVALUATING AIRCRAFT GAS TURBINE ENGINE LUBRICANTS
    BABER, BB
    CUELLAR, JP
    LUBRICATION ENGINEERING, 1969, 25 (03): : 117 - &
  • [35] Ceramic composite development for gas turbine engine hot section components
    DiCarlo, James A.
    van Roode, Mark
    Proceedings of the ASME Turbo Expo 2006, Vol 2, 2006, : 221 - 231
  • [37] INFLUENCE OF MISSION VARIABILITY ON FRACTURE RISK OF GAS TURBINE ENGINE COMPONENTS
    Enright, Michael P.
    Moody, Jonathan P.
    Chandra, Ramesh
    Pentz, Alan C.
    PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 7, PTS A AND B, 2012, : 439 - +
  • [38] Gas chromatographic monitoring of hydroxyl components in oxidized turbine engine lubricants
    Keller, MA
    Saba, CS
    TRIBOLOGY TRANSACTIONS, 2003, 46 (04) : 576 - 579
  • [39] REPRESENTATION OF COMPONENTS CHARACTERISTICS UNDER PERFORMANCE DEGRADATION OF GAS TURBINE ENGINE
    Jiang, Zhen
    Wang, Xi
    Yang, Shubo
    Liu, Jiashuai
    Chen, Huairong
    PROCEEDINGS OF ASME TURBO EXPO 2022: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2022, VOL 2, 2022,
  • [40] Repair and manufacturing of single crystal Ni-based superalloys components by laser powder deposition-A review
    Vilar, R.
    Almeida, A.
    JOURNAL OF LASER APPLICATIONS, 2015, 27