This part of ISO 898
specifies mechanical and physical properties of bolts, screws and studs made of
carbon steel and alloy steel when tested at an ambient temperature range of 10
<C to 35 <C. Fasteners ! the term used when bolts, screws and studs are
considered all together ! that conform to the requirements of this part of ISO
898 are evaluated at that ambient temperature range. They might not retain the
specified mechanical and physical properties at elevated temperatures (see Annex
B) and/or lower temperatures.
ISO 898-1 Chemical
Composition
Property
class
Material
and heat treatment
Chemical
composition limits
(cast analysis, %) a
Tempering
temperature
,c
nin.
c
p
max.
s
max.
a •
max.
min.
max.
4.6 c, d
Carbon
steel or carbon steelwith additives
-
055
0.050
0,060
Not
specified
-
4.8 d
5.6 c
013
055
0.050
0,060
5.8 d
-
055
0.050
0,060
6.8 d
015
055
0.050
0,060
8.8 f
Carbon
steel with additives (e.g. Boron or Mn or Cr) quenched and tempered
015.
040
0.025
0,025
0,003
425
or
Carbon steel quenched and tempered
025
055
0.025
0,025
or
Anoy steelquenched and tempered 9
020
055
0.025
0,025
9.8 f
Carbon
steel with additives (e.g. Boron or Mn or Cr) quenched and tempered
015.
040
0,025
0,025
0,003
425
or
Carbon steel quenched and tempered
025
055
0.025
0,025
or
Alloy steelquenched and tempered 9
020
055
0.025
0,025
10.9 f
Carbon
steel with additives (e.g. Boron or Mn or Cr) quenched and tempered
0,20 .
055
0,025
0,025
0,003
425
or
Carbon steel quenched and tempered
025
055
0.025
0,025
or
Alloy steel quenched and tempered 9
020
055
0,025
0,025
12..9 f.h.i
Alloy steel
quenched and tempered 9
030
050
0.025
0,025
0,003
425
12..9 f.h.i
Carbon
steel with additives (e.g. Boron or Mn or Cr or Molybdenum)quenched and
tempered
028
050
0.025
0,025
0,003
380
Note:
a. In case of dispute, the product analysis applies.
b. Boron content can reach 0,005 %, provided that non-effective boron is
controlled by addition of titanium and/or aluminium.
c. For cold forged fasteners of property classes 4.6 and 5.6, heat treatment of
the wire used for cold forging or of the cold forged fastener itself may be
necessary to achieve required ductility.
d. Free cutting steel is allowed for these property classes with the following
maximum sulphur, phosphorus and lead contents: sulphur 0,34 %; phosphorus 0,11
%; lead 0,35 %.
e. In case of plain carbon boron steel with a carbon content below 0,25 % (cast
analysis), the minimum manganese content shall be 0,6 % for property class 8.8
and 0,7 % for 9.8 and 10.9.
f. For the materials of these property classes, there shall be a sufficient
hardenability to ensure a structure consisting of approximately 90 % martensite
in the core of the threaded sections for the fasteners in the ^as-hardened ̄
condition before tempering.
g. This alloy steel shall contain at least one of the following elements in the
minimum quantity given: chromium 0,30 %, nickel 0,30 %, molybdenum 0,20 %,
vanadium 0,10 %. Where elements are specified in combinations of two, three or
four and have alloy contents less than those given above, the limit value to be
applied for steel class determination is 70 % of the sum of the individual limit
values shown above for the two, three or four elements concerned.
h. A metallographically detectable white phosphorus enriched layer is not
permitted for property class 12.9/12.9. It shall be detected by a suitable test
method.
i. Caution is advised when the use of property class 12.9/12.9 is considered.
The capability of the fastener manufacturer, the service conditions and the
wrenching methods should be considered. Environments may cause stress corrosion
cracking of fasteners as processed as well as those coated.
ISO 898-1 Mechanical
Requirements
No.
Mechanical or physical property
Property class
4.6
4.8
5.6
5.8
6.8
8.8
9.8
d + 16 mm
10.9
12.9/ 12.9
d+
16
mm
d
>
16
mm
1
Tensile
strength, Rm, MPa
nom.c
400
500
600
800
900
1000
1200
min.
420
500
520
600
800
830
900
1040
1220
2
Lower
yield strength, ReL d, MPa
nom.c
240
-
300
-
-
-
-
-
-
-
min.
240
-
300
-
-
-
-
-
-
-
3
Stress
at 0,2 % non, proportional elongation,
Rp0.2' MPa
nom.c
-
-
-
-
-
640
640
720
900
1080
min.
-
-
-
-
-
640
660
720
940
1100
4
Stress
at 0,0048 d non-proportional elongation for full-size fasteners,
Rpf, MPa
nom.c
-
320
-
400
480
-
-
-
-
-
min.
-
340e
-
420e
48e
-
-
-
-
-
5
Stress
under proof load, Sp,f,MPa
nom.c
225
310
280
380
440
580
600
650
830
970
Proof
strength ratio Sp,nom/ReL min or Sp,nom/Rp0,2 min or Sp,nom/Rpf min
min.
094
091
0.93
090
0.92
0.91
0.91
0.90
0.88
0.88
6
Percentage elongation after fracture for machined test pieces, A, %
min.
22
-
20
-
-
12
12
10
9
8
7
Percentage reduction of area after fracture for machined test
pieces, Z, %
min.
-
52
48
48
44
8
Elongation after fracture for full-size fasteners, Af (see also
Annex C)
min.
-
0.24
-
0.22
0.20
-
-
-
-
-
9
Head
soundness
No
fracture
10
Vickers
hardness, HV F W 98 N
min.
120
130
155
160
190
250
255
290
320
385
max.
220 g
250
320
335
360
380
435
11
Brinell
hardness, HBW F = 30 D2
min.
114
124
147
152
181
238
242
276
304
366
max.
209 g
238
304
318
342
361
414
12
Rockwell hardness, HRB
min.
67
71
79
82
89
!
max.
95,0 g
99,5
!
Rockwell hardness, HRC
min.
-
22
23
28
32
39
max.
-
32
34
37
39
44
13
Surface
hardness, HV 0,3 max.
!
h
h, i
h, j
14
Height
of non-decarburized thread zone, E, mm
min.
!
1/2 H1
2 /3 H1
3 /4H1
Depth
of complete decarburization in the thread, G, mm
max.
!
0,015
15
Reduction of hardness after retempering, HV
max.
!
20
16
Breaking torque, MB, Nm
min.
!
in
accordance with ISO 898-7
17
Impact
strength, KV k, l, J
min.
!
27
!
27
27
27
27
m
18
Surface
integrity in accordance with
ISO
6157-1 n
ISO
6157-3
Note: a. Values do
not apply for structural bolting.
b. For structural bolting d W M12.
c. Nominal values are specified only for the purpose of the designation system
for property classes. See Clause 5.
d. In cases where the lower yield strength ReL cannot be determined, it is
permissible to measure the stress at 0,2 % non-proportional elongation Rp0,2.
e. For the property classes 4.8, 5.8 and 6.8 the values for Rpf min are under
investigation. The present values are given for calculation of the proof stress
ratio only. They are not test values.
f. Proof loads are specified in Tables 5 and 7.
g. Hardness determined at the end of a fastener shall be 250 HV, 238 HB or 99,5
HRB maximum.
h. Surface hardness shall not be more than 30 Vickers points above the measured
core hardness of the fastener when determination of both surface hardness and
core hardness are carried out with HV 0,3.
i. Any increase in hardness at the surface which indicates that the surface
hardness exceeds 390 HV is not acceptable.
j. Any increase in hardness at the surface which indicates that the surface
hardness exceeds 435 HV is not acceptable.
k. Values are determined at a test temperature of −20 <C, see 9.14.
l.Applies to d W 16 mm.
m. Value for KV is under investigation.
n. Instead of ISO 6157-1, ISO 6157-3 may apply by agreement between the
manufacturer and the purchaser.