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X5CrNiMo17-12-2

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X5CrNiMo17-12-2 properties and heat treatment forged piece, Including X5CrNiMo17-12-2 application and specifications, We have all specifications,Including X5CrNiMo17-12-2 steel plate, X5CrNiMo17-12-2 sheet, X5CrNiMo17-12-2 square steel, X5CrNiMo17-12-2 flat bar,X5CrNiMo17-12-2 round bar,X5CrNiMo17-12-2 forgings, we can own production and sales.


Introduction to Our Products:

Specialized high quality steel

We have the advantages of equipment, technologies and price

forged/hot rolling/ extrusion of steel


We can produce the X5CrNiMo17-12-2 has the following specifications:

Round bar steel: 1mm to 3000mm

Square-shape steel: 1mm to 2000mm

Plate steel:0.1mm to 2500mm

Width: 10mm to 2500mm

Lenth: We can supply any lenth based on the customer's requirement.

Forging: Shafts with flanks/pipes/tubes/slugs/donuts/cubes/other shapes

Tubings: OD: φ6-219 mm, with wall thickness ranging from 1-35 mm.

Finished goods condition: hot forging/hot rolling + annealing/normalizing + tempering/quenching + tempering/any conditions based on the customer's requirement

Surface conditions: scaled (hot working finish)/ground/rough machining/fine machining/based on the customer's requirement

Furnaces for metallurgical processing: electrode arc + LF/VD/VOD/ESR/Vacuum consumable electrode.

Ultrasonic inspection: 100% ultrasonic inspection for any inperfections or based on the customer's requirementExcellent service for all kinds of industries,with advantages of technologies, equipment and price.

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Chemical composition % of the ladle analysis of grade X5CrNiMo17-12-2 and Standards

Identification
 
Designation by Standards
Brand Name
Ravne No.
Mat. No.
DIN
EN
AISI
PK12
915
1.4401
X5CrNiMo17122
X5CrnNiMo17122
316
 
Chemical Composition
 
Chemical Composition in Weight %
C
Si
Mn
Cr
Mo
Ni
V
W
Others
max. 0.07
max. 1.00
max. 2.00
17.50
2.25
11.50
-
-
-
 
General Information
 

Description
This austenitic stainless steel has an increased molybdenum content to increase its resistance to corrosion when compared to other 300 series alloys. It will resist scaling at temperatures up to 871�C and maintains good mechanical properties and ductility.

Applications
Widely used in industry, it was initially designed for paper mill machinery. It has been used in marine environments and a wide variety of general industrial components. Component parts for the cellulose, paper, oil, soap and textile industry, production of paints, meat processing industry, breweries, dairies and for surgical instruments.
 
Properties
 

Physical properties (avarage values) at ambient temperature:
Modulus of elasticity [103 x N/mm2]: 200, 186 (200�C), 172(400�C)
Density [g/cm3]: 7.98
Thermal conductivity [W/m.K]: 15.0
Electric resistivity [Ohm mm2/m]: 0.75
Specific heat capacity[J/g.K]: 0.50
Coefficient of Linear Thermal Expansion 10-6 oC-1
20-100�C
20-200�C
20-300�C
20-400�C
20-500�C
16.5
17.5
17.5
18.5
18.5
 
 

Hardening
Harden from a temperature of 1020-1100�C followed by water or oil quenching. Structure is austenite with small ferrite component.

Mechanical properties in solution-annealed condition and reistance to intercrystalline corrosion:
0.2 % proof stress: 200 N/mm2 (for d<=160, 160<d<=250)
1.0 % proof stress: 235 N/mm2 (for d<=160, 160<d<=250)
Tensile strength: 500-700 N/mm2
Elongation: 40% (for d<=160, longit.), 30% (for 160<d<=250, transv.)
Notch impact energy (ISO-V): 100 J (for d<=160, longit.), 60 J (for 160<d<=250, transv.) Resistance to interystalline corrosion: yes (in as delivered condition), no (in sensitised condition)
Note: Sensitisation treatment for 15 min at 700�C with subsequent cooling in air.
Mechanical Properties At Elevated Temperatures
Temperature
100�C
150�C
200�C
250�C
300�C
350�C
400�C
450�C
500�C
550�C
0.2 % proof stress in N/mm2
175
158
145
135
127
120
115
112
110
108
1.0 % proof stress in N/mm2
210
190
175
165
155
150
145
141
139
137
 
Workability
 

Forging
Hot forming temperature: 1200-900�C.

Machinability
Low speeds and constant feeds will minimize this alloy's tendency to work harden. Tougher than 304 stainless with a long stringy chip, the use of chip breakers is recommended.
 
Other Information
 
Corrosion Resistance: Resistant to a wide variety of marine environments, salts, dilute nitric, acetic and sulfuric acids.

Welding: All common fusion and resistance methods except oxyacetylene Welding have proven successful. Use AWS E/ER316 or 316L filler metal for best results.

Cold working: Shearing, stamping, heading and drawing can be successfully performed . To remove internal stresses, a post-work annealing is recommended.

Forms manufactured: Please see the Dimensional Sales Program.
 
Disclaimer
The information and data presented herein are typical or average values and are not a guarantee of maximum or minimum values. Applications specifically suggested for material described herein are made solely for the purpose of illustration to enable the reader to make his own evaluation and are not intended as warranties, either express or implied, of fitness for these or other puposes. There is no representation that the recipient of this literature will receive updated editions as the become available.
 
Contact our Sales Office or one of our International Sales Offices for more information.
 



Machining performance

Download X5CrNiMo17-12-2 the mechanical properties of the report, the report provides detailed performance analysis and application. Download >>


Principal Design Features

One of the most widely used precipitation hardening grades in the business. While soft and ductile in the solution annealed condition, it is capable of high properties with a single precipitation or aging treatment. Characterized by good corrosion resistance, high harness, toughness and strength.


Machinability

Long, gummy chips characterize this alloys machinability. It can be machined in the annealed condition, however condition H1150M will yield best results. Post machining solution treatment of parts will be required prior to final hardening if machining in this condition.


Heat Treatment

CONDITION A--Soak at 1900 F (1038 C) for 30 minutes and cool below 60 F (16 C) for complete martensite transformation. CONDITION H 950- Treat Condition A material at 900 F(482 C) for 1 hour, air cool.. CONDITION H925, H1025, H1075, H1100, H1150- Soak solution treated material for 4 hours at specified temperature, air cool, CONDITION H1150M- Soak solution treated material at 1400 F (760 C) for 2 hours, air cool, then re-heat to 1150 F (620 C) for 4 hours and air cool.


Welding

Successfully welded by common fusion and resistance methods, this alloy should not be joined by oxyacetylene welding. AWS E/ER630 filler metal is recommended if required.


Forging

Soak for 1 hour at 2150 F (1177 C) prior to forging. Do not work below 1850 F (1010 C). Post-work solution treatment is required prior to final hardening.





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