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DIN 1.4016

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DIN 1.4016 properties and heat treatment forged piece, Including DIN 1.4016 application and specifications, We have all specifications,Including DIN 1.4016 steel plate, DIN 1.4016 sheet, DIN 1.4016 square steel, DIN 1.4016 flat bar,DIN 1.4016 round bar,DIN 1.4016 forgings, we can own production and sales.


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We can produce the DIN 1.4016 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.

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Chemical composition % of the ladle analysis of grade DIN 1.4016 and Standards

Category  steel
Class  Stainless steel
Type  Ferritic standard
Common Names  Chromium steel
Designations  France: AFNOR Z 8 C 17
Germany: DIN 1.4016
Italy: UNI X 8 Cr17
Japan: JIS SUS 430
Sweden: SS 2320
United Kingdom: B.S. 430 S 15
United States: AMS 5503 , AMS 5627 , ASME SA182 , ASME SA240 , ASME SA268 , ASME SA479 , ASTM A176 , ASTM A182 , ASTM A240 , ASTM A268 , ASTM A276 , ASTM A314 , ASTM A473 , ASTM A479 , ASTM A493 , ASTM A511 , ASTM A554 , ASTM A580 , ASTM A651 , FED QQ-S-763 , FED QQ-S-766 , FED QQ-W-423 , FED STD-66 , MIL SPEC MIL-S-862 , SAE 51430 , SAE J405 (51430) , UNS S43000

Composition
Element Weight %
C  0.12 
Mn  1.00 
Si  1.00 
Cr  16.0-18.0 
P  0.04 
S  0.03 

Mechanical Properties
Properties  Conditions 
T (°C) Treatment
Density (×1000 kg/m3) 7.8 25  
Poisson's Ratio 0.27-0.30 25  
Elastic Modulus (GPa) 200 25  
Tensile Strength (Mpa) 480  25  annealed, hot finished (plate, sheet, strip) more
Yield Strength (Mpa) 275 
Elongation (%) 20 
Reduction in Area (%) 45 
Hardness (HRB) 88 (max)  25  annealed (plate, sheet, strip) 

Thermal Properties
Properties  Conditions 
T (°C) Treatment
Thermal Expansion (10-6/ºC) 10.4  0-100 more  
Thermal Conductivity (W/m-K) 26.1  100 more  
Specific Heat (J/kg-K) 460  0-100   

Electric Properties
Properties  Conditions 
T (°C) Treatment
Electric Resistivity (10-9W-m) 600  25   




Machining performance

Download DIN 1.4016 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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