Is 810 1991
Is 810 1991
Indian Standard
INTERNALCOMBUSTIONENGINES-
ENGINEVALVES-SPECIFICATION
( Second Revision )
October 1991
Automotive Primemovers Sectional Committee, TED 2
FOREWORD
This Indian Standard was adopted by the Bureau of Indian Standards, after the draft finalized by the
Automotive Primemovers Sectional Committee had been approved by the Transport Engineering
Division Council.
This Indian Standard was first published in 1974. In this revision, the scope has been enlarged to cover
all types of engine valves ( other than aircraft engines ) presently being used by the manufacturers and
the users in internal combustion engines. The types of valves included are:
In the preparation of this revision ~assistance has been derived from JIS E 101 ‘Engine valves for
automobiles’ issued by the Japanese Industrial Standards Committee. ’
For the purpose of deciding whether a particular requirement of this standard is complied with, the
final value observed or calculated expressing the results of a test. shall be rounded off in accordance
with IS 2 : 1960 ‘Rules for rounding off numerical values ( revised)‘. The number of significant places
retained in the rounded off value should be the same as that of the specified value in this standard.
h&m Standard
INTERNAL COMBUSTION ENGINES -
ENGINE VALVES - SPECIFICATION
/ Second Revision)
1 SCOPE IS No. Title
1.1 This standard specifies the general require- 3703 : 1981 Code of practice for magnetic
ments for inlet and exhaust valves for all particle flaw detection (Jirst
internal combustion engines other than for air- revision )
craft use. 7494 : 1981 Steel for valves for internal com-
1.2 Sodium filled valves, phosphated valves, bustion engines (first revision )
shrouded valves and valves with more than 12969 : 1990 Method of test for quality charac-
100 mm head diameter are not covered by this teristics of valves
standard.
3 TERMINOLOGY
1.3 The methods of test for quality characteris-
tics of engine valves are covered in IS lL969 : For the purpose of this standard the following
1990. definitions shall apply to denote the parts of a
2 REFERENCES valve ( see Fig. 1 ). The term, valve face, is to be
preferred to designate the cone shaped seating
The following Indian Standards are necessary surface of the valve and the term ‘valve seat’ is
adjuncts to this standard. to be preferred to designate the corresponding
IS No. Title mating part when the valve is assembled in the
engine.
1586 : 1968 Methods for Rockwell hardness
test ( B and C scales ) for steel 3.1 crown
( jirst revision ) The extreme upper surface of the valve head.
1608 : 1972 Method for tensile testing of steel
products (first revision ) 3.2 Valve Face
3073 : 1967 Assessment of surface roughness Coned surface of the valve that sits on the
3658 : 1981 Code of practice for liquid pene- corresponding seat surface of the cylinder head
trant flaw detection (Jirst revision ) or cylinder block, as the case may be.
GAUGE
DIA
GROOVE WID’IH
13
LAND OR MARGIN
4
HEAD 4 STEM
4 I ?
FIG. 1 TERMINOLOGY
1
IS81O:l~l .
That part of the valve between the crown and 5.3 Heat Treatment
the valve face. Valves made from martensitic steels or austeni-
tic alloys shall be used either in the fully heat
3.12 Gauge Diameter treatment condition or in the forged and stress-
An imaginary geometrical contact diameter relieved condition subject to the minimum
between the valve face and seat. tensile strength specified in 5.2. The heat treat-
ment particulars for the alloys are given in A-3.
3.13 Reference Diameter Valves made out of martensitic steels when
hardened and tempered shall have a general
A nominal value, designated to enable measure- hardness of 25 to 35 HRC, when tested as
ment of head thickness against a fixed reference. per IS 1586 : 1968.
4 TYPES OF VALVES 5.3.1 Any other range of hardness may be
agreed upon between the purchaser and the
4.1 The two main types of valves are: supplier.
a) Single piece valve; and 6 MANUFACTURE OF VALVE FORGINGS
b) Two-piece or bimetallic construction. 6.1 The valve forgings shall be manufactured
either by the upsetting process or by extrusion.
‘There can be additional features by way of
surface treatment and hard facing as well as 6.2 The grain flow shall be continuous and
local hardening. shall generally follow the throat contour.
2
Is 810 : 1991
to.10 +0*05
-0.15 -0.15
r
6 d,
3
IS 810 : 1991
Table 1 Dimensional Tderanees for Vahes Table 3 Surface Fin&h (M Crowd Regioas
( Clause 7.2 and Fig. 3 ) ( Clause 7.3.1 )
Valve face angle f + 30’ 12.1 The valve shall be given one of the follow-
< - 0’ ing two surface treatments, to improve the anti-
1
1)Not applicable in the case of round and tapered seizure properties of the valve stem in particular
grooves. and the corrosion resistance of the valve in
general. The testing procedures are outlined
in IS 12969 : 1990.
Table 2 Dimensions for Stem Diameters
( Clause 7.2 ) 12.1.1 Hard Chromium Plating
Figure 7 shows the details of the stem region
Stem Diameter Tolerances protected by hard chromium platjng along with
mm mm
the suggested minimum plating thickness. When
3-6 - 0’01.5
specified, the hard chromium plating shall be
> 6-10 - 0’020 carried out in a~plating bath by any one of the
>lO-18 - 0’025 standard electrochemical methods. The plating
NOTE - Tolerance for stem diameter 18 mm and thickness shall be 0.003 mm minimum. Higher
above shall be as agreed to between the purchaser plating thickness values shall be as agreed to
and the supplier. between the purchaser and the supplier.
4
IS 810 : 1991
DETAIL X
5
a) b) e) d)
All dimensions in millimetres.
FIG. 6 HARDFACINGANDINDUCTIONHARDBNINGOF VALVE FACE
7 Bd,
_ _
?
!
. -
- 0.006
- o*ooo
CF 3 CHROMIUM PLAl:EO OR FLASH 04 !
FIG. 7 CHROMIUMPLATING
13.1.2 Hardfacing of the tappet face shall con- an external gap width and depth of 0.2 mm
sist of depositing by oxy-acetylene flame or by maximum are permitted. Longitudinal seams
any other approved welding methods, approxi- typical of continuously cast raw material is
mately 1 to 2 mm layer of a wear resistant permitted over the stem region of the valve but
material. A few typical hardfacing alloys, along shall not extend into the undercut or groove
with values of minimum hardness obtainable regions. The depth of these seams shall be less
after hardfacing, are indicated in A-2. Other than 0.5 mm and the root shall not be a
alloys, not indicated in A-2 shall be used subject V-notch.
to agreement between the purchaser and .the
15 TESTS
supplier.
15.1 Macro Etch Examination
14 SURFACE IMPERFECTIONS
151.1 Valves shall be subjected to a grain flow
14.1 The valve shall be free of tool marks or detection test by hot etching in hydrochloric
any other cut marks that are likely to interfere acid, cold etching in Marble’s Reagent, or by
with the functioning of the valve. However, any other approved method of macro etching.
certain minor blemishes due to forging, machin- The etching shall be done so as not to cause
ing or handling shall be permitted subject to excessive pittings and corrosion of the sample.
agreement between the purchaser and the sup- The grain flow shall be continuous and shall
plier. Typical minor forging flaws are those in generally follow the throat contour.
the crown and throat ( neck ) regions and shall
not be deeper than 0.5 mm and the root shall 15.2 Crack Detection Test
not be a V-notch. Hardness check marks taken 15.2.1 Valves when tested for crack detection
onRockwell ‘A’ scale or Vickers are acceptable. by the magnetic crack detection, the colour,
Circumferential indications either in visual dye penetrant, the fluoroscopic dye penetrant
inspection or in crack detection are not accept- or by any other approved method as agreed to‘
able except at the button welded interface where between the purchaser and the supplier, shall,
6
IS 810 : 19Yl
Sl Material Type C Si Ni Cr MO W V Na S P
No. Max Max
1. 4OCr4 M 0’35-0’45 0’10-0’35 0’60-0’90 - 0’90-1’20 - - - - 0’04 0’04
2. 40NiOCr4Mo3 M 0’35-0’45 0’10-0’35 0’40-0’70 1.25-l ‘75 0’9-1’3 0’2-0’35 - - - 0’035 0’04
3. X50Cr9Si2 M 0’45-0’55 1 ‘O-2.0 0’6 Max 0’6 Max 7’5-9’5 - - - - 0’035 0’04
4. X45Cr9Si3 M 0’40-0’50 2’75-3’75 0’80 Max 0’50 Max 7’50-9’50 - - - - 0’035 0’04
5. X40CrllSiZMol M 0’35-0’45 1’8-2’5 0’6 Max 10‘0-12’0 0’7-1’3 - - - 0’035 0’04
6. X80Cr20Si2Nil M 0’75-0’85 1’75-2’50 0’80 Max 1’00-1’70 19’0-21’0 - - - - 0’035 0’04
7. X45019Ni9Si3Wl A 0’4-0’5 2’0-3’0 0.8-l ‘5 8’0-10’0 17’0-20’0 - 0’8-1’2 - - 0’035 0’05
8. X20Cr21Ni12N A 0’15-0’25 0.75-l ‘25 1’5 Max l”.5-12.5 20’0-22’0 - - - 0’15-0’30 0‘035 0’05
9. X70Cr21Mn6Ni2N A 0’65-0’75 0’45-0’85 5’5-7’0 1‘4-1’9 20’0-22’0 - - - 0’180’28 6’035 0’05
10. X55Cr21Mn8Ni2N A 0’50-0’60 1’0 Max 7’0-9’5 1’5-2’75 20’0-22’0 - - - 0’20-0’40 0’035 0’05
11. X53Cr22Mn9Ni4N A 0’480’58 0’25 Max 8’0-10’0 3’25-4’50 20’0-23’0 - - - 0’38-0’50 0’035 0’05
12. X30Cr20NillMo2P A 0’25-0’35 1’0 Max 1’2 Max 10’0-12’0 19’0-21’0 1’8-2’5 - B. O’Ol- - 0’035 0’18-0’25
13. X33Cr23Ni8Mn3N A 0’28-0’38 0.5-l ‘0 1’5-3’5 7’0-9’0 22’0-24’0 - - - 0’25-0’40 0’035 0’05
14. Nickel Alloy SOA A 0’10 Max 1’0 Max 1’0 Max Base 18’0-21’0 Ti 1 ‘O-2.70 Al 1 ‘O-1‘80 d’03 0’045
Fe 3’0 Max Co 2’0 Max
15. Nickel Alloy 751 A 0’10 Max 1-o Mnx 1’0 Max 70’0 Min 14’0-17.0 Ti 2’0-2’6 Fe 5’0-9’0 0’03 0’045
Al 0’9-1’5 Nb+Fa 0’7/1’2
NOTES
1 Alloys 9, 10 and 11 may have sulphur upto 0’09 percent for free machining.
2 The letter ‘M’ has been used to denote Martensitic steels and the letter ‘A’ to denote Austenitic steels/alloys.
IS 810 : 1991
CoCr Alloy 2’0-3’0 0’4-2’0 1.0 Max 3’0 Max 26’0-33’0 Base 11’0-14’0 3’0 Max 48 Min Tappet end
Type 1
CoCr Alloy 1 ‘O-l ‘7 0’4-2’0 1’0 Max 3’0 Max 26’0-33.0 Base 7’0-9’5 3’0 Max 45 Min Tappet end
Type 12 and valve
face
CoCr Alloy 0’9-1’4 0’4-2’0 1’0 M’ax 3’0 Max 26’0-33’0 Base 3’0-6’0 3’0 Max 38 Min Valve face
Type 6
CoNiCr Alloy 1’5-2’0 0’9-1’3 0’3 Max 21’0-23’0 24’0-27’0 Base 11’5-13’0 0’85-1’35 38 Min valve face
Type 32
Nickel Alloy 0’3-0’7 2’5-5’0 3’0 Max 58’0-63’0 14’0-18’0 - - Balance 20 Min Valve face
60
FeCrNiMo 2’0-2’5 0’8-1’3 - 10’0-12’0 22’0-26’0 - MO Base 35 Min Valve face
Alloy 5’0-6’0
Fe Cr Alloy 2’5-2’7 - - - 25’5-28’5 - - Base 50 Min Tappet face
NOTE - The hardness figures given refer to the as cast hardness and the hardfacing alloys are not heat-treatable.
9
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