Chromium-nickel-molybdenum stainless construction steel with aluminum additive X3CrNiMoAl13-8-2, 1.4534, PH 13-8 Mo, 13-8 Mo precipitation strengthened for use in the aerospace, petroleum and petrochemical industries.
| Standards | Steel Grades | ||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Chemical Composition % | |||||||||||
| C: | Mn: | Si: | P: | S: | Cr: | Mo: | Ni: | Al: | Ti: | N: | |
| ASTM ASME | PH 13-8 Mo - PH 13-8Mo - XM-13 - XM13 - 13/8Mo | ||||||||||
| <0.05 | <0.2 | <0.1 | <0.01 | <0.008 | 12.3 - 13.2 | 2.0 - 2.5 | 7.5 - 8.5 | 0.90 - 1.35 | - | <0.01 | |
| LW | 1.4534 - X3CrNiMoAl13-8-2 - X 3 CrNiMoAl 13-8-2 | ||||||||||
| <0.05 | <0.1 | <0.1 | <0.01 | <0.008 | 12.25 - 13.25 | 2.0 - 2.5 | 7.5 - 8.5 | 0.90 - 1.20 | - | <0.01 | |
| AMS UNS | AMS 5629 - UNS S13800 | ||||||||||
| <0.05 | <0.2 | <0.1 | <0.01 | <0.008 | 12.3 - 13.2 | 2.0 - 2.5 | 7.5 - 8.5 | 0.90 - 1.35 | - | <0.01 | |
| AFNOR | X1CrNiMoAl12-9 - Z1CNDA12-09 | ||||||||||
| <0.05 | - | <0.1 | - | - | 11.5 - 12.5 | 1.8 - 2.5 | 8.0 - 9.5 | 0.6 - 0.9 | <0.35 | - | |
| BS | BS 13-8 | ||||||||||
| <0.05 | <0.2 | <0.1 | - | - | 12.25 - 13.25 | 2.0 - 2.5 | 7.5 - 8.5 | 0.90 - 1.35 | - | <0.01 | |
| AFNOR | Z4CNDAT13-09 - Z 4 CNDAT 13-09 | ||||||||||
| <0.04 | <0.2 | <0.1 | <0.015 | <0.008 | 11.5 - 13.5 | 1.8 - 2.5 | 7.5 - 9.5 | 0.6 - 1.4 | <0.40 | - | |
PH 13-8Mo, 1.4534, X3CrNiMoAl13-8-2 - specification and application
13-8Mo is acid resistant special steel with martensitic structure, subjected to precipitation hardening, showing excellent mechanical properties - high hardness, strength and relatively high corrosion resistance, dynamic loads and cracking resistive.
Compared to other high alloyed grades exhibiting corrosion resistance, 13-8Mo steel has much more limited acceptability of sulfur and phosphorus in its chemical composition, which demonstrates a relatively difficult manufacturing process and high purity and quality of steel.
In aggressive environments (excluding moisture resistance) the species exhibits very good resistance to NaCl, Nitric Acid, and Sodium Hydroxide.
The PH13-8Mo is mainly used in the aerospace, nuclear, and petrochemical industries for parts and components subject to corrosion and heavy loads.
Mechanical properties for long products according to ASTM A564 XM-13
- +A
- HRC Hardness: <38
- HB Hardness: <363
- +H950
- Tensile strength, Rm: >1515 MPa
- Yield point, Re: >1415 MPa
- Elongation, A: >10%
- HRC Hardness: >45
- HB Hardness: >450
- +H1000
- Tensile strength, Rm: >1415 MPa
- Yield point, Re: >1310 MPa
- Elongation, A: >10%
- HRC Hardness: >43
- HB Hardness: >400
- +H1025
- Tensile strength, Rm: >1280 MPa
- Yield point, Re: >1210 MPa
- Elongation, A: >11%
- HRC Hardness: >41
- HB Hardness: >380
- +H1050
- Tensile strength, Rm: >1210 MPa
- Yield point, Re: >1140 MPa
- Elongation, A: >12%
- HRC Hardness: >40
- HB Hardness: >372
- +H1100
- Tensile strength, Rm: >1035 MPa
- Yield point, Re: >950 MPa
- Elongation, A: >14%
- HRC Hardness: >34
- HB Hardness: >313
- +H1150
- Tensile strength, Rm: >930 MPa
- Yield point, Re: >620 MPa
- Elongation, A: >14%
- HRC Hardness: >30
- HB Hardness: >283
- +H1150M
- Tensile strength, Rm: >860 MPa
- Yield point, Re: >585 MPa
- Elongation, A: >16%
- HRC Hardness: >26
- HB Hardness: >259
Mechanical properties for flat products PH 13-8Mo according to ASTM A693
In supersaturated condition:
- thickness from 0.038 - 101.6mm
- HRC Hardness: >38
- HB Hardness: >363
In condition after precipitation hardening - supersaturation and ageing at 510℃:
- Thickness <0.51mm
- Tensile strength, Rm: >1515 MPa
- Yield point, Re: >1410 MPa
- Elongation, A: >6%
- HRC Hardness: >45
- Thickness 0.51 - 4.76mm
- Tensile strength, Rm: >1515 MPa
- Yield point, Re: >1410 MPa
- Elongation A: >8%
- HRC Hardness: >45
- Thickness 4.76 - 15.88mm
- Tensile strength, Rm: >1515 MPa
- Yield point, Re: >1410 MPa
- Elongation, A: >10%
- HRC Hardness: >45
- Thickness 15.9 - 102.0mm
- Tensile strength, Rm: >1515 MPa
- Yield point, Re: >1410 MPa
- Elongation, A: >10%
- HRC Hardness: >45
- HB Hardness: >429
In condition after precipitation hardening - supersaturation and ageing at 540℃:
- Thickness <0.51mm
- Tensile strength, Rm: >1380 MPa
- Yield point, Re: >1310 MPa
- Elongation, A: >6%
- HRC Hardness: >43
- Thickness 0.51 - 4.76mm
- Tensile strength, Rm: >1380 MPa
- Yield point, Re: >1310 MPa
- Elongation A: >8%
- HRC Hardness: >43
- Thickness 4.76 - 15.88mm
- Tensile strength, Rm: >1380 MPa
- Yield point, Re: >1310 MPa
- Elongation, A: >10%
- HRC Hardness: >43
- Thickness 15.9 - 102.0mm
- Tensile strength, Rm: >1380 MPa
- Yield point, Re: >1310 MPa
- Elongation, A: >10%
- HRC Hardness: >43
- HB Hardness: >401
In the above mentioned grades the company provides:
- Flat bars PH 13-8Mo, 1.4534, 13-8Mo, X3CrNiMoAl13-8-2
- Round bars PH 13-8Mo, 1.4534, 13-8Mo, X3CrNiMoAl13-8-2
- Forgings and forged bars PH 13-8Mo, 1.4534, 13-8Mo, X3CrNiMoAl13-8-2
Other signs and equivalents:
AMS 5629, ASTM A693 Grade XM-13, ASTM A564 Grade XM-13, ASTM A705 Grade XM-13, PH13-8Mo, PH 13-8Mo, PH 13-8 Mo, N 4534, E 4534, 04Cr13Ni8Mo2Al, X1CrNiMoAl12-9, X 1 CrNiMoAl 12-9, Z4CNDAT13-09, Z 4 CNDAT 13-09, Z1CNDA12-09, Z 1 CNDA 12-09, MARVAL X12, X3CrNiMoAl13-8-2, X 3 CrNiMoAl 13-8-2, 1.4534, N709, 13-8Mo, BS13-8, ASTM A959 Grade XM-13, 13/8Mo, X1CrNiMoAlTi12-9, AMS 5928, S11800 UNS S13800, XM13, ABS 5442, ABS 5629A/B, AIMS 01-04-002, LN 668 / 1013, LN 1017, AMS 5622, AMS 5643, 1.4530.