Heat Treatment:
- Normalise at a temperature of 810C/840CCelsius
- Harden in oil from a temperature between 810C/840CCelsius
- Temper at a suitable temperature, 550CCelsius for condition “T”, 610CCelsius for condition “S” and 660C Celsius for condition “R”
Specification: EN19 – 709M40
Colour Code: Black |
Availability:
- Black Round Bar in “as rolled “ and hardened and tempered to condition “T”
- Black rolled and forged surface: 16mm diameter to 350mm diameter
- Bright Peeled Round Bar, “as rolled” and condition “T”: 16mm diameter to 160mm diameter
|
Characteristics:
- This material distorts when machining shafts or long spindles, especially once hardened and tempered
- In practice, the work pieces should be rough machined to plus
tolerance and left in the open on the floor for 36 hours after which the
material would have “aged” and stress relieved itself and thereby
minimising distortion on the finishing of the product
- Machinability is good but allow 6% on outside diameter for removal of surface defects
- This material can be welded but welding should only be attempted by
using the appropriate methods and materials as advised by welding
expertise
- Ideal for 60 ton tensile applications up to 100mm max
- Sizes above limited ruling section will be heat treated to hardness only, with no guarantee on mechanical properties
|
Applications:
- Utilised when higher than carbon steel mechanical properties are required
- Commonly used for axles, drive shafts, crankshaft connecting rods,
high tensile bolts, studs, propeller shaft joints, rifle barrels, and
induction hardened pins
- Bolt specification: 9.8 (in condition “T”)
- Bolt specification: 10.9 (in condition “U”)
|
Comparable Specifications:
- Din 42CrMo4
- SAE 4240
- Deutsche W/No 1.7225
- Euro Norm EN 10083-1 (1991) 970 Part 1; 42CrMo4
- BS970 Part 1 1983, 709M40
- BS970 of 1955 EN19
|
Chemical Composition (%):
Carbon (C) |
0.36 (Min) – 0.44 (Max) |
Silicon (Si) |
0.10 (Min)- 0.40 (Max) |
Manganese (Mn) |
0.70 (Min) - 1.00 (Max) |
Chromium (Cr) |
0.90 (Min) – 1.20 (Max) |
Sulphur (S) |
nil (Min) – 0.04 (Max) |
Phosphorus (P) |
nil (Min)- 0.035 (Max) |
Molybdenum (Mo) |
0.25 (Min) – 0.35 (Max) |
|
Working and Heat Treatment:
- Forging: Forge within the temperature range of 1250C/900C Celsius
- Anneal: Anneal at a temperature of 850C Celsius and cool steadily
- Normalising: not applicable
- Hardening: oil quench from a temperature of 850C/880C Celsius
|
Mechanical Properties:
|
Annealed
|
R
|
S
|
T
|
U
|
V
|
W
|
Y
|
Ruling Section (mm) |
150
|
150
|
100
|
65
|
65
|
30
|
30
|
25
|
Tensile Strength (MPa) |
680/720
|
690/850
|
770/930
|
850/1000
|
930/1080
|
1000/1160
|
1080/1240
|
1280
|
Yield Stress (MPa) |
440/480
|
480
|
570
|
665
|
740
|
835
|
895
|
1050
|
Elongation (% Min) |
22
|
15
|
15
|
13
|
12
|
12
|
10
|
10
|
ISO V Impact (Joule) |
30
|
30
|
30
|
30
|
25
|
25
|
22
|
7
|
Hardness (Brinell) |
190/210
|
201/255
|
223/277
|
248/302
|
269/321
|
293/341
|
311/375
|
363/415
|
|
|
|
|
|
|
|
|
|
Proof Stress (0.2%) if required (MPa, Min) |
|
495
|
550
|
630
|
710
|
770
|
850
|
985
|
Specification: EN24 – 817M40
Colour Code: Blue and Black |
Availability:
- Black Round Bar in “as rolled” or hardened and tempered to condition “T”
- Black Round Bar: 20mm diameter to 350mm diameter (as rolled / as forged)
|
Characteristics:
- This is more versatile specification than 709M40
as the limiting ruling sections for heat treatment are amplified
because of the addition of Nickel
- Welding should only be attempted by using the appropriate methods and materials as advised by welding expertise
- Machinability is good and has little distortion in machining
- Allow 6% on the outside diameter for removal of surface defects during machining
- Ideal for 60 ton tensile applications up to 250mm diameter max
- This material is often used in the annealed, as rolled or as forged
condition for machining. Subsequent heat treatment is used to achieve a
higher tensile i.e. condition “T”, “U”,” V”, ”W”, “X”, “Y” and “Z”
- This material can be certified as a safety
specification in lifting equipment when such equipment is subject to
impacts and requires a high tensile property, such as shaft sinking
equipment in the mining industry
|
Applications:
- This material is used where high tensile strengths and good impact values are required
- Some of the more popular uses include differential shafts, pinion
sleeves, eccentric crusher shafts, eccentric high pressure shafts, high
duty connection rods, power transmission slide gears and slide cams,
mandrels for tube mills, heavy axles and high tensile gears, bolts and
nuts
- Bolt Specification: 10.9 (in condition “U”)
- Bolt Specification: 12.9 (in condition “V”)
|
Comparable Specifications:
- Din 40CrM0 8 – 4
- SAE 4340
- Deutsche W/No 1.6562
- Euro Norm EN10083-1 (1991) 970 Part 1; 34CrN1Mo6
- BS970 Part 1 1983, 817M40
- BS970 of 1955 EN24
- American AISI 4340
|
Chemical Composition (%):
Carbon (C) |
0.36 (Min) – 0.44 (Max) |
Silicon (Si) |
0.10 (Min) – 0.35 (Max) |
Manganese (Mn) |
0.45 (Min) – 0.70 (Max) |
Sulphur (S) |
Nil (Min) – 0.04 (Max) |
Phosphorus (P) |
Nil (Min) – 0.040(Max) |
Nickel (Ni) |
1.30 (Min) – 1.70 (Max) |
Chromium (Cr) |
1.00 (Min) – 1.40 (Max) |
Molybdenum (Mo) |
0.20 (Min) – 0.35 (Max) |
|
Working and Heat Treatment:
- Forging within the temperature range 1100⁰/850⁰ Celsius
- Anneal at a temperature of 760⁰ Celsius, soaking for four hours after reaching temperature
- Normalising is not applicable
- Hardening by oil quench at a temperature of 820⁰/850 Celsius after soaking through
|
Mechanical Properties:
|
Annealed
|
S
|
T
|
U
|
V
|
W
|
X
|
Y
|
Z
|
Ruling Section (mm) |
250
|
250
|
250
|
100
|
65
|
30
|
30
|
30
|
30
|
Tensile Strength (MPa) |
620
|
680/770
|
850/1000
|
930/1080
|
1000/1160
|
1080/1240
|
1235 (Min)
|
1540 (Min)
|
1540 (Min)
|
Yield Stress (MPa) |
410
|
480
|
635
|
740
|
835
|
925
|
1005
|
1130
|
1130
|
Elongation (% Min) |
16
|
16
|
12
|
12
|
12
|
11
|
10
|
5
|
5
|
ISO V Impact (Joule) |
30
|
32
|
40.7
|
47.5
|
47.5
|
40.7
|
34
|
30
|
10
|
Hardness (Brinell) |
180/220
|
223/277
|
248/302
|
269/321
|
293/341
|
311/375
|
341/388
|
363/415
|
444 (Min)
|
Proof Stress (0.2%) if required (MPa, Min) |
|
550
|
630
|
710
|
770
|
850
|
910
|
990
|
1235
|
Note: Interestingly, the impact values do not alter between condition “U” and condition “V”.
Specification: EN26 – 826M40
Colour Code: Black/Orange |
Availability:
- Availability is extremely limited in the South African market
- Prospective users of this specification are advised to check availability before any commitments
|
Characteristics:
- A 6% allowance should always be made for removal of surface defects during machining
- Welding is not recommended on this specification
- Machinability good
- Ideal for heat treated condition (U/60/70 ton tensile) or V (65/75 ton tensile)
- As with EN24, this material is ordered in the annealed, as rolled or
as forged condition for machining. Subsequent heat treatment is used
to achieve higher tensile
strength i.e. Condition T, U, V,
W, X, Y and Z
- Some applications require this material to be heat treated to BS2772 Part 2 Grade 826M31 to qualify as a safety standard
|
Applications:
- Similar applications and uses as EN24 817M40 but for higher tensile requirements
- This specification is prescribed by the mining industry in South
Africa for lifting equipment e.g. stress parts in winches and cranes and
general lifting tackle such as eyebolts, shackles and hooks. However,
the material has to be manufactured to 826M31 procedures to qualify as a
safety standard
- When this material is specified for safety reasons it is used in
spline shafts, gear shafts, winder equipment parts, heavy duty mining
head gears and in other safety critical mining applications
- It is further used as high impact eccentric
shafts, crusher shafts, turnbuckles, brake pins, tie rods and main line
railway armature shafts
|
Comparable Specifications:
- Din 40NiMoCr 10-5
- Deutsche W/No 1.6745
- BS970 Part 1 1983, 826M40
- BS970 of 1955 EN26
|
Chemical Composition (%):
Carbon (C) |
0.36 (Min)- 0.44 (Max) |
Silicon (Si) |
0.10 (Min) – 0.35 (Max) |
Manganese (Mn) |
0.45 (Min) – 0.70 (Max) |
Sulphur (S) |
Nil (Min) – 0.040 (Max) |
Phosphorus (P) |
Nil (Min) – 0.040 (Max) |
Nickel (Ni) |
2.30 (Min) – 2.80 (Max) |
Chromium (Cr) |
0.50 (Min) – 0.80 (Max) |
Molybdenum (Mo) |
0.45 (Min) – 0.65 (Max) |
|
Working and Heat Treatment:
- Forging is done within the temperature range 1100⁰ / 850⁰ Celsius
- Annealing at a temperature of 670⁰ Celsius, soaking for 4 hours after reaching temperature
- Normalising, not applicable
- Hardening, oil quench at a temperature of 820⁰/850⁰ Celsius, after soaking through
|
Mechanical Properties:
|
U
|
V
|
W
|
X
|
Y
|
Z
|
Ruling Section (mm) |
150
|
150
|
150
|
100
|
100
|
100
|
Tensile Strength (MPa) |
930/1080
|
1000/1160
|
1080/1240
|
1235 (Min)
|
1540 (Min)
|
1540 (Min)
|
Yield Stress (MPa) |
740
|
835
|
925
|
1005
|
1130
|
1130
|
Elongation (% Min) |
17
|
14
|
13
|
14
|
14
|
10
|
ISO V Impact (Joule) |
47.5
|
47.5
|
40.7
|
34
|
34
|
14
|
Hardness (Brinell) |
269/321
|
293/341
|
311/375
|
341/388
|
363/415
|
444 (Min)
|
Proof Stress (0.2%) if required (Mpa, Min) |
710
|
770
|
850
|
910
|
990
|
1235
|
Specification: EN30B – 835M30 (Annealed)
Colour Code: Orange |
Availability:
- Black Round Bars supplied only in the annealed condition
- Availability is extremely restricted and
prospective users of this specification are advised to check
availability before committing to using it
|
Characteristics:
- This is a very expensive steel specification not
just because of the high alloying elements but also the refining
methods utilised to keep the hydrogen (H) content of the steel to less
than two parts per million, (H = ≤ 2PPM). It is more costly than other
B.S. 970 specifications
- This is 1500 MPa minimum tensile steel , air hardening in sections up to 65mm diameter
- Specially recommended for intricately shaped parts where an air hardening steel is preferred
- This material can be case hardened , can be carburised and induction hardened or shorterised (flame hardened)
|
Applications:
- 835M30 is a versatile specification.
- The applications of this material are numerous and includes the following
- In Engineering: ultra high tensile applications,
shafts, gears, bolts, spline shafts, crusher shafts, eccentric shafts,
hard wearing bushes and high impact pistons
- In mining: rock drill, knock off bits, mill hammers, cyclone plates, high tensile mechanical and thermal shock applications
- In Tooling: plastic extrusion dies, die bolster rings and punches
|
Comparable Specifications:
- Din 36NiCrMo16
- Deutsche W/No 1.6773
- Euro Norm EN 10220-3 (1999)
- 36NiCrMo16
|
Chemical Composition (%):
Carbon (C) |
0.26% (Min) |
0.34% (Max) |
Silicon (Si) |
0.10% (Min) |
0.35% (Max) |
Manganese (Mn) |
0.40% (Min) |
0.60% (Max) |
Sulphur (S) |
Nil |
0.25% (Max) |
Phosphorus (P) |
Nil |
0.25% (Max) |
Nickel (Ni) |
3.90% (Min) |
4.30% (Max) |
Chronium (Cr) |
1.10% (Min) |
1.40% (Max) |
Molybdenum (Mo) |
0.20% (Min) |
0.40% (Max) |
|
Mechanical Properties:
Tensile Strength |
1500 MPa (Min) |
Yield Stress |
1300 MPa (Min) |
Elongation |
10% (Min) |
ISO V Impact |
20 Joule (Min) |
Hardness |
444 Brinell (Min) |
|
Working and Heat Treatment:
- Forging: Do not charge into a hot or preheated furnace. Heat from cold to forging temperature 950⁰/1000⁰Celsius. Do not exceed 1100⁰ Celsius. Forge
carefully and do not work on the steel below 850⁰/900⁰ Celsius as the
material is then hardening and this condition excessive stresses will
build up in the workpiece. Cool the forging slowly and out of draughts
or bury in lime or ashes.
- Annealing: Heat carefully to 810⁰ Celsius and allow
to cool in the furnace or still air. Re-heat the steel slowly in the
furnace to 630⁰/640⁰ Celsius and soak for about four hours after wich it
may be cooled in still air (sub critically annealed). All parts for machining should be annealed.
- Normalising: Not applicable
- Hardening: To harden in air or oil, heat the parts
gradually and uniformly to a temperature of 810⁰/830⁰ Celsius. When air
hardening, place the parts out of draughts to avoid unequal hardening
and consequent stresses. For up to 65mm diameter the properties are
obtainable through air hardening. For larger sections, oil hardening
should be performed.
- Tempering: Where extreme
toughness is desired, the pieces, whether air or oil hardened should be
subsequently tempered at a maximum temperature of 250⁰ Celsius allowing
time for tempering through. Test results obtained on a 30mm diameter
test piece after hardening at 820⁰ Celsius and tempering at 250⁰ Celsius
|
Specification: EN36B – 655M13
Colour Code: White |
Availability:
- Black Round Bars: 20mm diameter to 350mm diameter (as rolled and as forged)
|
Characteristics:
- This material is also known as 3% Nickel-Chromium Case-Hardening Steel
- This specification is good for welding, prior to Carburising and Case Hardening
- Machinability is good but allow 6% on the outside diameter for removal of surface defects
- Required hardness can be achieved by case
hardening the outer surface by means of one of the following,
Carburising, Carbonitriding, Nitriding, Nitrocarbursing, Tufftriding
|
Applications:
- This material is often used in the manufacturing of gears, worm shafts, pinion shafts and spline shafts
- This specification is largely utilised when wear resistant hard surface is required along with high core strength
- Other common uses include Auto and heavy vehicle
transmission components, engineering machinery gear box parts, aircraft
gears mining steering worms, chuck jaws, track pins, gudgeon pins,mining
gearbox gears, pinions and cogs
|
Comparable Specifications:
- Din 15NiCr13
- SAE 3316
- Deutsche W NO 1.5752
- Euro Norm EN 10084 (1998) 15NiCr13
- BS970 Part 1 1983, 655M13
- BS970 of 1955 EN36B
|
Chemical Composition (%):
|
% Min
|
% Max
|
Carbon (C) |
0.10
|
0.16
|
Silicon (Si) |
0.10
|
0.035
|
Manganese (Mn) |
0.35
|
0.60
|
Phosphorus (P) |
Nil
|
0.04
|
Sulphur (S) |
Nil
|
0.04
|
Chromium (Cr) |
0.70
|
1.00
|
Nickel (Ni) |
3.0
|
3.75
|
|
Mechanical Properties:
- Mechanical Properties of the core of a case hardened test bar of 28mm diameter
- Hardness of the test bar surface, Rc65
Tensile Strength (Min) |
1000 MPa
|
Elongation (Min) |
9%
|
ISO V Impact |
40 Joule
|
|
Working and Heat Treatment:
- Carburise at a temperature of 900⁰/930⁰ Celsius
- Refine at a temperature of 860⁰/880⁰ Celsius (see Note)
- Harden at a temperature of 760⁰/780⁰ Celsius in oil
Note: A “Single Quench” treatment may suffice to
obtain the specified results. Intricate parts, or parts of large
sectional differences may distort in the refining treatment, thus the
tendency to avoid refining after carburising. However, should the
hardness not be uniform, cryogenic (sub zero) treatment is recommended.
Through the analysis (chemical composition), the refining treatment
after carburising may be omitted an a “Single Quench” treatment may be
employed |
|
|
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