[0001] This invention deals with an austenitic stainless, precipitation hardenable chromium-nickel-aluminium
steel with good cold workability. By tempering the martensite obtained by cold working,
quenching or in some cases cooling to subzero temperatures, precipitation hardening
is obtained. The new alloy can be produced as hot rolled products such as wire rod,
bar, strip and plate.
[0002] Precipitation hardening of stainless steel using aluminium is a well-known technique.
These steels can either be given an annealing treatment designed to raise the M
stemperature so much that martensite is formed on quenching, or they can be annealed
at a higher temperature giving an austenitic structure when quenched. In the latter
case the steel can be subsequently cold worked, thus transforming the austenite into
martensite. After one of these treatments the material can be precipitation hardened.
[0003] The disadvantage with these steels is that the rate of martensite formation when
cold working is extremely high, thus rendering the material difficult to work. The
risk of stress cracks, for example, during the wire drawing process is extremely high.
[0004] The main purpose of the present invention is thus to improve the workability in the
cold condition of Cr-Ni-Al steels by lowering the M
s and the M
d30 temperatures sufficiently to ensure that good workability is obtained without at
the same time lowering them so far that the austenite is not transformed to martensite
when cold worked. Martensite is desirable in the final product since it raises the
mechanical strength considerably.
[0005] Two production heats with the following analyses have been made under production
conditions.

[0006] Both heats were melted in a 10-ton high-frequency induction furnace, ingot teemed
and rolled to billets. These were conditioned and rolled to wire rod, 0 6.0 mm for
heat 3423-71 and 0 5.6 mm for heat 4029-71. The wire rod was subjected to a normal
anneal at 1050°C, pickled and inspected before being drawn to wire.
[0007] As reference material a heat (3226-71) in steel of type 17-7 PH (AISI 631) has been
produced by the same method. This is a precipitation hardenable Cr-Ni-Al-steel with
the following heat analysis (Table 2).

[0008] Heats 3423-71 (Table 1) and 3226-71 have been drawn from wire rod, 0 6.0 mm, using
single drafts. The tensile strength (R
m), yield strength (R
e), and reduction of area (Z) as measured by tensile testing are compared in Figure
1. It is apparent that the yield and tensile strengths increase more slowly for the
alloy in the invention (continuous curve) thus causing the drawability, measured as
maximum achievable area reduction, to increase from 75% to 92%. Moreover, the ductility
measured as reduction of area is higher for the alloy in the invention over the whole
range and particularly at large area reductions. It should be noted that stress cracks
are completely absent in the material for area reductions as large as 92% compared
with 17-7 PH where a definite risk of stress crack formation exists at area reductions
as low as 45%.
[0009] The precipitation hardening effect of the alloy in the invention has been tested
for two different area reductions and the results are shown below in Table 3.

[0010] Tempering treatment: 30 minutes at 450°C.
[0011] Thus, the tempering treatment gives an increase of yield and tensile strengths of
about 200 N/mm
2 for heat 3423-71 and about 400 N/mm
2 for heat 4029-71. The large difference between these effects can be explained by
the fact that wire rod from heat 3421-71 has not been worked sufficiently, i.e. the
austenite has not been transformed to martensite insufficient quantities prior to
tempering.
[0012] The alloy in this invention has mainly been developed in order to improve the cold
workability of precipitation hardenable stainless Cr-Ni-Al steels. Within the area
ABCD in Figure 2 the composition can be set so that annealing in the temperature range
600-950°C leads to a rise in the Ms temperature due to carbide precipitation. The
material can subsequently be cooled to ambient or subzero temperatures in order to
obtain a transformation to martensite which can then be tempered.
[0013] A particularly interesting application is cold heading where tensile strengths as
low as 540 - 560 N/mm
2 have been measured on material annealed at 1050°C. This is true for both heats 3423-71
and 4029-71.
[0014] The technical result of the invention is that the drawability is considerably improved
at the same time as the precipitation hardening effect is retained. It is reasonable
to assume that the good weldability can be improved by additions of zirconium and
uranium instead of titanium. Since the'alloy has an extremely sluggish martensitic
transformation in the annealed state the material can be stored and transported outdoors
under cold weather conditions without risk of spontaneous martensite formation.
[0015] Chromium and nickel contents should lie within the area ABCD as shown in Figure 2
where chromium can be partly replaced by molybdenum with up to 2%, and nickel can
be partly replaced by manganese according to the formula % Ni = 1/2 (% Mn - 1%). In
one, particularly preferred, form of the alloy chromium and nickel should lie within
the area ABCD in Figure 2.
[0016] The alloy according to the invention is annealed within the temperature range 600
- 950°C, quenched and cooled to below room temperature. The alloy can then be precipitation
hardened by tempering.
[0017] The alloy can also be quenched direct after hot rolling and subsequently cold worked
and precipitation hardened by tempering.
1. Austenitic, precipitation hardenable, stainless chromium-nickel-aluminium steel
with good cold workability and characterized by containing Cr 13 - 22% and Ni 5 -
17% and C up to 0.15%, Si up to 3.0%,.Mn up to 8.0%, P up to 0.045%, S up to 0.040%,
Mo up to 2.0%, N up to 0.15%, Al 0.5 - 2.5% and preferably one or more of the metals
Ti, Zr and U up to 2%, with the balance of iron and impurities normally occurring
in stainless steels and the sum of Ni and Mn expressed as Ni' = %Ni + 1/2 (% Mn-1)
and the sum of Cr and Mo expressed as Cr' according to the formula Cr' = %Cr + %Mo
lies within the area ABCD in the enclosed diagram Figure 2.
2. Steel according to claim 1, characterized by the fact that it contains either Ti
up to 0.5% or Zr up to 0.5% or U up to 1%.
3. Steel according to claims 1 and 2, characterized by a chromium content of 22% corresponding
to a nickel content between 5.25 and 12.5% and a chromium content of 13% corresponding
to a nickel content between 10.15 and 17%.
4. Steel according to claims 1 and 2, characterized by the fact that the chromium
content lies between 16.5% and 18.2% and the nickel content between 8.25% and 9.75%.