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Experimental evaluation of HFMI effectiveness for weld repairs Cover

Experimental evaluation of HFMI effectiveness for weld repairs

Open Access
|Jun 2026

Figures & Tables

Figure 1:

Principle of the HFMI treatment method (Campagnolo et al., 2021)

Figure 2:

Allowed FAT category increase for HFMI treated Welds (Marquis & Barsoum, 2016)

Figure 3:

Geometry of the specimen with butt V-weld (identical for the specimen with X-weld)

Table 1:

Number of specimens for fatigue testing

Weld typeV and X
Stress ratio R0.1
TreatmentAs WeldedHFMIHFMI repair
S355J2+N444
S460NL654
S690QL544
S960QL444
Table 2:

Technical manufacturing parameters

S355 specimens: Technical manufacturing parameters
Welding method135 (MAG) according to EN ISO 4063
Filler materialEN ISO 14341-A: G46 3 C1 4Si1/G50 5 M21 4Si1
Shielding gasM21 (82% Ar + 18% CO2) – STARGON 18
Preheat temperature-
S460 specimens: Technical manufacturing parameters
Welding method135 (MAG) according to EN ISO 4063
Filler materialEN ISO 14341-A: G46 3 C1 4Si1/G50 5 M21 4Si1
Shielding gasM21 (82% Ar + 18% CO2) – STARGON 18
Preheat temperature-
S690 specimens: Technical manufacturing parameters
Welding method135 (MAG) according to EN ISO 4063
Filler materialEN ISO 16834-A: G 69 4 M21 Mn3Ni1CrMo
Shielding gasM21 (82% Ar + 18% CO2) – STARGON 18
Preheat temperature100 °C
S960 specimens: Technical manufacturing parameters
Welding method135 (MAG) according to EN ISO 4063
Filler materialEN ISO 16834-A: G 89 4 M20 Mn4Ni2CrMo
Shielding gasM21 (82% Ar + 18% CO2) – STARGON 18
Preheat temperature150 °C
Figure 4:

Testing equipment with specimen during the fatigue experiment

Figure 5:

Localization of the fatigue crack using NDT penetrant testing (PT) after completion of loading

Figure 6:

Repair of a specimen affected by a fatigue crack

Table 3:

Number of cycles to failure for S355 steel grade specimens

MaterialS355
Stress ratio R0.1
Spec. numberTreatmentStress range [MPa]Number of cycles to failure
1As Welded10010 000 000*
2As Welded10010 000 000*
3As Welded2001 531 011
4As Welded2001 486 900
5HFMI20010 000 000*
6HFMI2005 000 000*
7HFMI2505 000 000*
8HFMI3001 900 389
9HFMI repair3002 728 703
10HFMI repair3001 741 976
11HFMI repair320474 210
12HFMI repair320974 818

* No failure occurred in the specimen. The limit number of cycles was reached without the formation of a fatigue crack (runout).

Figure 7:

Comparison of results S355 steel grade specimens

Table 4:

Number of cycles to failure for S460 steel grade specimens

MaterialS460
Stress ratio R0.1
Spec. numberTreatmentStress range [MPa]Number of cycles to failure
13As Welded200474 157
14As Welded2003 018 047
15As Welded300210 929
16As Welded300331 088
17As Welded350129 096
18As Welded350309 218
19HFMI2004 393 464
20HFMI2005 000 000*
21HFMI300984 402
22HFMI350847 345
23HFMI350947 066
24HFMI repair300589 985
25HFMI repair3001 175 960
26HFMI repair350254 244
27HFMI repair350688 634

* No failure occurred in the specimen. The limit number of cycles was reached without the formation of a fatigue crack (runout).

Figure 8:

Comparison of results S460 steel grade specimens

Table 5:

Number of cycles to failure for S690 steel grade specimens

MaterialS690
Stress ratio R0.1
Spec. numberTreatmentStress range [MPa]Number of cycles to failure
28As Welded2002 674 867
29As Welded300501 424
30As Welded300372 388
31As Welded50055 796
32As Welded50079 230
33HFMI3005 000 000*
34HFMI3505 000 000*
35HFMI500167 150
36HFMI500289 026
37HFMI repair400426 198
38HFMI repair400116 523
39HFMI repair450309 494
40HFMI repair450160 857

* No failure occurred in the specimen. The limit number of cycles was reached without the formation of a fatigue crack (runout).

Figure 9:

Comparison of results S690 steel grade specimens

Table 6:

Number of cycles to failure for S960 steel grade specimens

MaterialS960
Stress ratio R0.1
Spec. numberTreatmentStress range [MPa]Number of cycles to failure
41As Welded300492 569
42As Welded50055 205
43As Welded50060 774
44As Welded80016 832
45HFMI3005 000 000*
46HFMI50070 656
47HFMI500293 794
48HFMI80015 584
49HFMI repair450110 727
50HFMI repair450172 590
51HFMI repair50032 423
52HFMI repair500110 359

* No failure occurred in the specimen. The limit number of cycles was reached without the formation of a fatigue crack (runout).

Figure 10:

Comparison of results S960 steel grade specimens

DOI: https://doi.org/10.2478/cee-2026-0027 | Journal eISSN: 2199-6512 (formerly 1336-5835) | Journal ISSN: 1336-5835
Language: English
Page range: 620 - 631
Submitted on: Jul 27, 2025
Accepted on: Sep 30, 2025
Published on: Jun 19, 2026
Published by: University of Žilina
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2026 Jakub Štěpán, Pavel Ryjáček, Miloslav Kepka, Radovan Minich, published by University of Žilina
This work is licensed under the Creative Commons Attribution 4.0 License.