Repair welding of wrought superalloys: Alloy 718, Allvac 718Plus and Waspaloy

被引:32
作者
Andersson, J. [1 ,2 ]
Sjoberg, G. P. [1 ,2 ]
机构
[1] Volvo Aero Corp, Dept Mat Technol, S-46181 Trollhattan, Sweden
[2] Chalmers Univ Technol, S-41296 Gothenburg, Sweden
关键词
Heat affected zone cracking; Strain age cracking; WELDABILITY; CRACKING; INCONEL;
D O I
10.1179/1362171811Y.0000000077
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The ability to weld repair three precipitation hardening superalloys, i.e. Alloy 718, Allvac 718Plus and Waspaloy, with gas tungsten arc welding, is compared in this study. Four different solution heat treatment conditions for each material were examined: Alloy 718 and Allvac 718Plus heat treated at 954 degrees C-1 h, 982 degrees C-1 h, 954 degrees C-15 h and 1020 degrees C-1 h and Waspaloy for 4 h at 996 degrees C, 1010 degrees C, 1040 degrees C and at 1080 degrees C. By metallography, the total number of cracks was evaluated in both the heat affected zone and the fusion zone, which made it possible to consistently rate the repair weldability of these three materials. Alloy 718 was significantly the best one, with Allvac 718Plus slightly better than Waspaloy. As expected, the solution heat treatment conditions only affected the heat affected zone cracking behaviour.
引用
收藏
页码:49 / 59
页数:11
相关论文
共 19 条
[1]   Metallurgical Response of Electron Beam Welded Allvac® 718Plus™ [J].
Andersson, J. ;
Sjoberg, G. ;
Hanninen, H. .
HOT CRACKING PHENOMENA IN WELDS III, 2011, :415-+
[2]  
Andersson J., 2011, THESIS CHALMERS U TE
[3]  
Andersson J, 2008, P 47 C MET WINN CAN, P401
[4]  
[Anonymous], 2009, 5662M AMS SAE INT
[5]  
[Anonymous], 2006, 5544H AMS SAE INT
[6]  
[Anonymous], 2002, 5706K AMS SAE INT
[7]  
[Anonymous], 2006, 5441 AMS SAE INT
[8]   The influence of minor elements on the weldability of an INCONEL 718-type superalloy [J].
Benhadad, S ;
Richards, NL ;
Chaturvedi, MC .
METALLURGICAL AND MATERIALS TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 2002, 33 (07) :2005-2017
[9]  
BOUCHER C, 1976, REV METALL-PARIS, V73, P817
[10]  
Kennedy RL, 2005, SUPERALLOYS 718, 625, 706 AND DERIVATIVES, PROCEEDINGS, P1