The
production of machined and welded parts for automobile construction prompted
Don Foster to make a particularly selective choice among steel grades. From
the company's many years of experience, it has been found that 15CDV6 is the
best option for resolving the technical and economic problems that arise today.
IMPLEMENTATION
OF 15CDV6
Machining in the annealed or treated state does not generate any particular
difficulties.
In the treated state, steel can be rolled or bent with radii greater than
2.5 times the thickness.
Heat treatment has been defined specially to obtain excellent results by fluo-turning.
Similarly, deep stamping requires special annealing for the stamping techniques.
WELDING
15CDV6
steel is remarkably suitable for every welding process, whether oxyacetylene,
electric, arc, resistance, electron beam or laser.
The main coated electrode manufacturers have defined rods with a special grade
that are totally suitable and offer the same strength in the joint.
Soudure
Autogène Française: Electrode Safer CDV 100
ESAB: Electrode OK 78-05
PFor
torch or argon welding (TIG or MIG), a flux wire has been produced using slag
and copper coating conforming to standard Air 9114.
No preheating is needed to a thickness of 10 mm, and welding in the treated
state is just as easy as for annealed metals. After welding, there is no excessive
hardening of the cord requiring stress-relief treatment.
Indeed, the presence of molybdenum and vanadium means that the annealing effect
near the cord, affecting the mechanical strength of steel welded assemblies,
is almost insensitive when 15CDV6 is used. The strength of the treated metal
is maintained intact within the cord and around it, so that assemblies with
consistent strength exceeding 1,000 MPa can be obtained without any heat treatment.
This unique property is confirmed by the thousands of rolled and welded power plants envelopes that have been produced in which the welded generating line is put through the same stresses as the base metal.
MIXED ASSEMBLIES
One
major advantage of 15CDV6 steel is that it can be assembled, by welding, with
other grades of steel.
For similar grades like 25CD4S, there is naturally little difficulty, but
it can equally well assemble very different steels or alloys. For instance,
for ballistic device construction, calling for structural hardening stainless
steel, 15CDV6 steel not only welds very well with them, but preserves its
properties after complex treatment.
There
are also application where Z10CNT18 stainless steel is welded with 400CDV-20-25CD4S-XC18S
steel, etc.
15CDV6 has replaced in the AIR 9160/C standard the 25CD4S steel because of
its higher performance, whether in terms of weldability, suitability for tempering,
or mechanical properties.
L'ASSOCIATION EUROPEENNE des CONSTRUCTEURS de MATERIELS AEROSPATIAL (AECMA)
has standardized it under the designator FE-PL 52 S.

STEEL PROPERTIES, ESPECIALLY 15CDV6
MECHANICAL CHARACTERISTICS ON SHEET METAL
By
tempering and annealing in air, tensile strength of between 980 and 1,180
MPa is obtained for sheet metal less than or equal to 8 mm in thickness. Beyond
this thickness, 15CDV6 is still worth considering. Accordingly, the minimum
strength of 1,000 MPa is preserved with good working capability on 25 mm oil
or water tempered sheet metal, annealed, and even after electric arc welding,
without preheating or post-heating.
From a thickness of 8 mm on, oil or water tempering ensures consistent strength
exceeding 1,000 MPa with good working capability.
| Chemical composition ( % ) |
|
Elements
|
C
|
Si
|
Mn
|
P
|
S
|
Cr
|
Mo
|
Ni
|
V
|
| Min. |
0,12
|
-
|
0,80
|
-
|
-
|
1,25
|
0,80
|
-
|
0,20
|
| Max. |
0,18
|
0,20
|
1,10
|
0,015
|
0,015
|
1,50
|
1,00
|
-
|
0,30
|
| Elasticity modulus according to temperature |
|
º
C
|
20
|
100
|
200
|
300
|
400
|
500
|
550
|
600
|
|
MPa
|
209
000
|
204
000
|
199
000
|
190
300
|
181
500
|
170
200
|
163
300
|
158
000
|
|
COMPOSITION
|
| Carbon | 0.15 |
| Chromium | 1.25 |
| Molybdenum | 0.90 |
| Vanadium | 0.25 |
|
HEAT
TREATMENT
|
|
TEMPERING
|
|
Heating
to 975°C, tempering in oil or air depending on the thickness of
the parts.
|
|
ANNEALING
|
|
Depending
on the desired properties.
|
|
MECHANICAL
CHARACTERISTICS
|
|
AT
AMBIENT TEMPERATURE
|
|
In
the annealed state: approximately strength 550 MPa.
|
|
|
Oil
tempering at 975°C. Annealing at 625°C, quenching in oil
|
| * Strength | 1050 Mpa |
| * el. Limit 0,2 % | 1100 Mpa |
| * Elongation. (5d) | 17 % |
| * KCU Resilience | 130 J/cm2 |
MECHANICAL
PROPERTIES DEPENDING ON
ANNEALING TEMPERATURE

|
AT
THE FOLLOWING TEMPERATURES:
* el. Limit 0.2 % depending on temperature, on treated metal: 1100 MPa |
|
Temperature
in °C
|
Load
application time
5 Minutes ..............10 Minutes |
|
|
300
|
780
Mpa
|
750
Mpa
|
|
400
|
730
Mpa
|
710
Mpa
|
|
500
|
670
Mpa
|
640
Mpa
|
|
600
|
500
Mpa
|
470
Mpa
|
|
PROPERTIES
|
Density: 7,8
Average
dilatation coefficient in m/m °C:
*between 20°C and 200°C: 12,6X10(exponent-6)
*between 20°C and 400°C: 13,5X10(exponent-6)
*between 20°C and 600°C: 14,3X10(exponent-6)
Transformation
points:
*Ac 1 = 765°C
*Ac 3 = 950°C
Thermal
conductivity in W m/m2 °C
*at 20°C : 46
FORGING
1100 / 900°C
ANNEALING
CHeating to 875°C and slow cooling. In the softened state, approximate
Brinell hardness 174.
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| COMPOSITION | |||||
|
Carbon
(C)
|
Chrome
(Cr)
|
Molybdenum
(Mo)
|
Vanadium
(V)
|
||
| 15 CDV6 |
min
|
0,12
|
1,25
|
0,8
|
0,2
|
|
max
|
0,18
|
1,5
|
1
|
0,3
|
|
|
25
CD 4S
|
average
|
0,25
|
1
|
0,2
|
0
|
| 4130 |
min
|
0,27
|
0,8
|
0,15
|
0
|
|
max
|
0,33
|
1,1
|
0,25
|
0
|
|
| DESCRIPTION | ||
| AFNOR | 15 CDV 6 | 25 CD 4 S |
| WERKSTOFF | 1,7734 | 1,7218 |
| DIN . | 14 Cr Mo V6,9 | 25 Cr Mo 4 |
15
CDV 6 is compatible with standard AIR 9160 C
25 CD 4 S is replaced by 15 CDV 6 in standard AIR 9160 C
4130 is compatible with US standard MIL-S-18729 C and MIL-S-6758 A
| MECHANICAL PROPERTIES | |||
|
Rm
> 700 Mpa
|
980
< Rm < 1180
|
1080
< Rm < 1250
|
|
|
15
CDV 6
|
Annealed
|
Quenched
in air
|
Quenched
in oil
|
|
1,7734
|
1,7734.4
|
1,7734.5
|
1,7734.6
|
|
25
CD 4S
|
Rm
maxi: 820 Mpa
|
||
|
4130
|
Rm
maxi: 820 Mpa
|
||