Application
Alloy 6B wrought base-cobalt alloys
No. 6B and 6K have been used successfully for many years in
applications involving severe conditions of wear or wear combined
with corrosion and/or high temperature. They are used particularly for
shaft sleeves, bushings, valve parts, pump plungers, doctor blades,
feed screws, knives, wear plates, and bearings.
Tough
and Abrasion Resistant
Alloys No. 6B and 6K are
cobalt-based alloys with outstanding resistance to most types of wear.
Their wear resistance is inherent. It is a "built-in"
characteristic and not the result of heat-treatment, plating,
nitriding, or other methods used to produce a superficial hardness on
metal parts. Half bushings and haft sleeves made of alloy No. 6B
can be used in locations where abrasive particles like fly ash, coke,
metal powder, shale, or cement dust tend to collect in bearing
surfaces. The ability of these parts to withstand the wearing effects
of hard, sharp particles makes them especially useful in screw
conveyors, rock crushing rollers, tile-making machines, and cement
and steel-mill equipment.
Resist
Seizing and Galling
Alloy No. 6B is resistant to the
effects of seizing or galling. In many cases, its low coefficient of
friction allows sliding contact with other metals without damage by
metal pick-up. Alloy No. 6B has been used in equipment
where no lubricants were used because of the nature of the product
being handled. Sleeves made of alloy No. 6B move smoothly, with a
minimum of resistance, even when operating in contact with other
metal parts. They have been useful in inaccessible areas where
efficient lubrication is impossible. Sleeves and bushings have
resisted seizing even when lubricants were diluted by gasoline,
cleaning fluids, and other liquids that wash out an oil film. They
have operated at peak efficiency even when lubricants decomposed
under heat, or were destroyed by abrasive particles.
Resist
Erosive Wear
Parts made of alloy No. 6B have had
long service life - even under constant erosive conditions. It has
outstanding resistance to cavitation-erosion. Alloy No. 6B
used for steam turbine erosion shields has protected the blades of
one turbine for over 19 years of continuous service.
Good
Impact and Thermal Shock Resistance
Alloy No. 6B combines wear
and corrosion resistance with good impact strength and resistance to
thermal stock.
Resist
Heat and Oxidation
High temperatures have little effect
on the hardness, toughness, and dimensional stability of these
alloys. They are highly resistant to atmospheric oxidation at
ordinary temperatures, and have good resistance to oxidation at
elevated temperatures.
Excellent
Hot Hardness
Alloy 6B wrought, cobalt-based alloy
No. 6B retains high hardness even at red heat. Once cooled back to
room temperature, it recovers it's full original hardness.
Corrosion
Resistance
In addition to its wear-resistance,
alloy No. 6B has good resistance to a variety of corrosive
media. This combination of properties makes alloy No. 6B particularly
useful in such applications as food handling machinery, chemical
equipment, and others where both wear - and corrosion-resistance are
necessary. Where extraordinary resistance to corrosion is
required, one of the Hastelloy nickel-based alloys may prove more
suitable.
Available
Forms
Alloy No. 6B and No. 6K are available
in the form of sheet, plate, and fabricated shapes. Alloy No. 6B is
also available as bar.
Heat
Treatment
Wrought forms of alloy No. 6B
and No. 6K are supplied in the solution heat-treated condition unless
otherwise specified. The standard heat-treatment is at 2250°F
(1232°C) followed by air cooling.
Properties
Data
The properties listed in this page
are typical or average values based on laboratory tests conducted by
the manufacturer. They are indicative only of the results obtained in
such tests and should not be considered as guaranteed maximums or
minimums. Materials must be tested under actual service conditions to
determine their suitability for a particular purpose. All data
represent the average of four or less tests unless otherwise noted.
The secondary units (metric) used in this page are those of the SI
system.
Chemical
Composition, Percent
Alloy
|
Cobalt
|
Nickel
|
Silicon
|
Iron
|
Manganese
|
Chromium
|
Molybdenum
|
Tungsten
|
Carbon
|
No.
6B
|
Bal
|
3.00
max
|
2.00
max
|
3.00
max
|
2.00
max
|
28.00- 32.00
|
1.50
max
|
3.50- 5.50
|
0.90- 1.40
|
No.
6K
|
Bal
|
3.00 max
|
2.00 max
|
3.00 max
|
2.00 max
|
28.00 32.00
|
1.50 max
|
3.50- 5.50
|
1.40- 1.90
|
Average
Physical Properties
Physical
Properties
|
Temp., °C
|
Metric
Units Alloy
|
Temp., °F
|
British
Units Alloy
|
No.
6B / No. 6K
|
No.
6B / No. 6K
|
Density
|
22
|
kg/cubic m 8387
/ 8387
|
72
|
lb./cubic in. 0.303
/ 0.303
|
Melting Range
|
|
1265 to 1354°C
|
|
2310 to 2470°F
|
Electrical
Resistivity
|
22
|
Microhm-m 0.91
/ ---
|
72
|
Microhm-in. 36
/ -- (546 ohms per cir. mil ft.)
|
Thermal
Conductivity
|
22
|
W/m-K 14.8
/ ---
|
72
|
Btu-in./sq. ft.-hr.
°F 103 / --
|
Mean
Coefficient of Thermal Expansion
|
0-100 0-200 0-300 0-400 0-500 0-600 0-700 0-800 0-900 0-1000
|
x 10(-6)m/m-K 13.9
/ 13.8 14.1 / 13.8 14.5
/ 13.8 14.7 / 13.8 15.0
/ 13.8 15.3 / 14.0 15.8
/ 14.2 16.3 / 14.5 16.9
/ 14.9 17.4 / 15.5
|
32-212 33-392 32-572 32-752 32-932 32-1112 32-1292 32-1472 32-1652 32-1832
|
microinches/in.-°F 7.7
/ 7.7 7.8 / 7.7 8.0
/ 7.7 8.2 / 7.7 8.3
/ 7.7 8.5 / 7.8 8.8
/ 7.9 9.1 / 8.1 9.4
/ 8.3 9.7 / 8.6
|
Electrical
Conductivity Compared to Copper, percent
|
22
|
1.90
/ ---
|
72
|
109
/ --
|
Specific
Heat (calculated)
|
Room
|
J/kg-K 423
/ ---
|
Room
|
Btu/lb.- °F 0.101
/ --
|
Magnetic
Permeability at 200 Oersteds (15.900 A/m)
|
22
|
<1.2
/ <1.2
|
72
|
<1.2
/ <1.2
|
Reflecting
Power, percent
|
|
57-70
/ -----
|
|
57-70
/ ----
|
Average
Hot Hardness
Alloy
|
Test
Temp.,°F (°C)
|
Brinell
Hardness at Temperature Mutual indentation Method
|
No. 6B
|
1000(538) 1200(649) 1400(760) 1600(871)
|
226 203 167 102
|
Average
Compressive Strength
Alloy
|
Form
|
Test
Temp.
|
Average Compressive
Strength Ksi(MPa)
|
No.
6B No. 6K
|
1/2-in.
(12.7mm), Plate* Sheet*
|
Room Room
|
347(2392) 325(2241)
|
Average
Modulus of Rupture
Alloy
|
Form
|
Test
Temp.
|
Average Modulus
of Rupture Ksi(MPa)
|
No. 6B
|
Sheet*
|
Room
|
338(2360)
|
Average
Modulus of Elasticity
Alloy
|
Form
|
Test
Temp.
|
Average Modulus
of Elasticity psi x 10(6) (MPa)
|
No.
6B No. 6K
|
Sheet* 5/8-in.
(15.9 mm), Bar
|
Room Room
|
30.4(210,000) 31.1(214,000)
|
Average
Izod Impact Strength (un-notched)
Alloy
|
Form
|
Test
Temp.
|
Average
Izod Impact Strength (un-notched)
|
ft.lbs.
|
J
|
No. 6B
|
1/2-in. (12.7mm),
Plate*
|
Room
|
62
|
84
|
Average
Charpy Impact Strength
Alloy
|
Test
Temp., °F(°C)
|
Type
of Test
|
Average
Charpy Impact Strenght, ft. lbs. (J)
|
Longitudinal
|
Transverse
|
No. 6B 1/2-in.
(12.7 mm), Plate*
|
Room
|
Un-notched notched
|
72(98) 6(8)
|
65(88) ---
|
1000(538)
|
Un-notched notched
|
81(110) 15(20)
|
--- ---
|
1250(677)
|
Un-notched notched
|
116(157) 15(20)
|
--- ---
|
1500(816)
|
Un-notched notched
|
126(171) 15(20)
|
--- ---
|
*Solution heat-treated
at 2250°F (1232°C), air cooled.
Average
Room Temperature Data - Alloy No. 6B
Form
|
Condition
|
Ultimate
Tensile Strength Ksi (MPa)
|
Yield
Strength at 0.2% offset, Ksi (MPa)
|
Elongation in
2 in., (50.8mm), percent
|
Hardness Rockwell
C
|
Sheet 0.040 in. (1.0
mm),thick
|
Solution
Heat-treated*
|
145.0(1000)a
|
90.1(621)a
|
12a
|
36a
|
Sheet 0.065 in. (1.7
mm),thick
|
Solution
Heat-treated*
|
140.8(971)a
|
86.7(598)a
|
11a
|
36a
|
Sheet 0.125 in. (3.2
mm),thick
|
Solution
Heat-treated*
|
144.7(998)a
|
89.8(619)a
|
11a
|
37a
|
Sheet 0.187 in. (4.8
mm),thick
|
Solution
Heat-treated*
|
144.5(996)a
|
89.3(616)a
|
10a
|
37a
|
Plate 0.312 in. (7.9
mm),thick
|
Solution
Heat-treated* Aged 3 hrs at 1500°F (816°C)
|
140.2(967)b 142.4(982)
|
87.9(606)b 97.7(674)
|
10b 4c
|
37b 41
|
Plate 0.437 in.
(11.1 mm),thick
|
Solution
Heat-treated* Aged 3 hrs at 1500°F (816°C)
|
140.2(967)a 146.7(1012)c
|
85.6(590)a 96.3(664)c
|
12a 5c
|
37a 40
|
Plate 0.625 in.
(15.9 mm),thick
|
Solution
Heat-treated* Aged 3 hrs at 1500°F (816°C)
|
135.5(935)a 141.5(976)c
|
86.4(596)c 92.6(638)c
|
11a 6c
|
36a 41d
|
a - Average of 27-31
tests b - Average of 23 tests c - Average fo 22-24 tests d -
Average of 9 tests *Solution heat-treated at 2250°F (1232°C),
air cooled.
Average
Tensile Data*
Alloy
|
Form
|
Test Temp., °F
(°C)
|
Ultimate Tensile Strength, Ksi
(MPa)
|
Yield Strength at
0.2% offset, Ksi (MPa)
|
Elongation in
2 in., (50.8mm), percent
|
No.
6B
|
0.063
in. (1.6 mm), Sheet
|
Room
1500 (816) 1600 (871) 1800 (982) 2000 (1093) 2100
(1149)
|
146.0
(1007) 73.9 (509) 55.8 (385) 32.6 (225) 19.5
(134) 13.3 (92)
|
91.6
(632) 45.4 (313) 39.2 (270) 19.8 (137) 10.9 (75) 7.7
(53)
|
11 17 18 36 44 22
|
1/2-in.
(12.7 mm), Plate
|
Room
1000 (538) 1250 (677)
|
148.0
(1020) 133.0 (917) 115.0 (793)
|
88.0
(607) 58.5 (403) 60.6 (418)
|
7 9 9
|
5/8-in.
(15.9 mm), Bar
|
Room
600 (316) 1000 (538) 1500 (816) 1600 (871)
|
154.1
(1063) 147.8 (1019) 129.1 (890) 75.4 (520) 58.3 (402)
|
92.6
(638) 74.5 (514) 67.3 (464) 46.5 (321) 37.9 (261)
|
17** 30** 28** 38** 34**
|
No. 6K
|
0.063 in
(1.6mm), Sheet
|
Room 1200
(649) 1500 (816) 1800 (982) 2000 (1093)
|
176.5 (1217) 146.0
(1007) 70.2 (484) 34.1 (235) 17.4 (120)
|
102.7 (708) --- 44.5
(307) 19.3 (133) 8.6 (59)
|
4 8 17 28 53
|
1/2-in. (12.7
mm) and 7/6-in. (22.2 mm), Plate***
|
Room 600
(316) 1000 (538)
|
146.2 (1008) 113.9
(785) 105.7 (729)
|
108.2 (746) 80.5
(555) 75.0 (517)
|
1** 2** 3**
|
* Solution heat-treated
at 2250°F (1232°C), air cooled. **Elongation, percent in 1
in. (25.4 mm) ***Test bars cut transverse to rolling direction.
Average
Stress Rupture and Creep Data
Alloy
|
Test Temp., °F
(°C)
|
Stress, Ksi
(MPa)
|
Initial Elongation, percent
|
Life,
hrs.
|
Time
in Hours for Total Elongation, % of:
|
Elongation at
Rupture, percent
|
0.5
|
1.0
|
2.0
|
No. 6B, 0.063 in.
(1.6 mm), Sheet**
|
1000 (538) 1200
(649) 1400 (760) 1500 (816) 1600 (871) 1700
(927) 1800 (982) 2000 (1093)
|
60 (414) 50
(345) 35 (241) 25 (172) 19 (131) 12 (83) 8 (55) 2
(14)
|
0.70 0.45 0.35 0.35 0.10 0.19 0.05 0.004
|
192.8* 361.4 59.3 70.6 57.9 104.0 113.4 116.7
|
--- 0.5 0.4 0.2 0.5 1.8 5.1 4.4
|
--- 113.8 3.8 4.3 2.2 20.9 22.7 ---
|
--- --- 16.3 19.9 11.1 89.9 57.6 ---
|
0.8 3.0 5.1 4.7 4.3 2.6 5.5 13.3
|
* Test discontinued
before rupture. **Specimens were solution heat-treated at 2250°F
(1232°C) and air cooled prior to testing.
Average
Cavitation-Erosion Data
Alloy
|
Test Duration,
hrs.
|
Weight
loss, mg
|
Alloy No. 6B Type 304 Stainless Steel
|
100 7
|
42.3 39.9
|
Average
Abrasive Wear Data
Alloy
|
Condition
|
Volume Loss, mm(3)
|
Hardness, Rockwell
|
Wear Coefficient*
|
Alloy No. 6B Alloy 6B Alloy 6B Alloy 6K Haynes alloy No. 25 1090 Steel Type 316
Stainless Steel Type 304 Stainless Steel
|
Mill
annealed 10% cold-reduced 18.5% cold reduced Mill
annealed Mill annealed 1 hr. at 1600°F (871°C),
water quenched + 4 min. at 900°F (482°C) As received
sheet As received sheet
|
8.2 7.5 7.8 13.3 53.0 37.2 81.4 102.1
|
C-38 C-44 C-47 C-46 C-24 C-55 B-86 B-92
|
0.471
x 10(-3) 1.00 x 10(-3) 1.00 x 10(-3) 0.946 x
10(-3) 2.00 x 10(-3) 8.00 x 10(-3) 2.00 x 10(-3) 3.00
x 10(-3)
|
Average
Abrasive Wear Data **
Alloy
|
Condition
|
Ring
Alloy
|
Volume Loss,
mm(3)
|
Wear Coefficient*
|
Alloy No. 6B Alloy 6B Alloy
6K Haynes alloy No. 25 1090 Steel
|
Mill
annealed 10% cold-reduced Mill annealed Mill
annealed 1 hr. at 1600°F (871°C), water quenched + 4
min. at 900°F (482°C)
|
4620
Steel 4620 Steel 4620 Steel 4620 Steel 4620
Steel
|
0.293 0.347 0.561 0.285 0.293
|
3.70
x 10(-3) 5.10 x 10(-3) 8.73 x 10(-3) 2.50 x
10(-3) 6.00 x 10(-3)
|
Average
Coefficients of Static Friction For Some Common Materials
Material
Against
|
Alloy No. 6B
|
Cast
Iron
|
Bronze
|
Aluminum
|
Lead
|
Alloy No. 6B Cast Iron Bronze Aluminum Lead
|
0.119 0.123 0.125 0.138 0.119
|
0.123 0.199 0.245 0.213 0.225
|
0.125 0.245 0.231 0.257 0.249
|
0.138 0.213 0.257 0.213 0.328
|
0.119 0.225 0.249 0.328 0.290
|
Coefficient represents
tangent of angle of repose. Tests made on dry surfaces having better
than 120 grit finishes. All Values based on averages and are to be
used comparatively and not as absolute values. **Average of two or
more tests against a case-hardened SAE 4620 steel ring (Rockwell
C-63) *The wear coefficient (K) was calculated using the equation:
V= KPL/3h where V= Wear Volume (mm(3)) P = Load (kg) L =
Sliding distance (mm) h = Diamond pyramid hardness A
combination of a low wear coefficient and a high hardness is
desirable for good wear resistance.
Fusion
Welding
Alloys No. 6B and 6K can be welded by
gas tungsten-arc (TIG) with an argon flow of 25 CFH, gas metal-arc
(MIG), shielded metal-arc (coated electrode), and oxy-acetylene in
this order of preference. The oxy-acetylene method should be used
with discretion and care in that alloys No. 6B and 6K will "boil"
during welding which may cause porosity. Use a 3X reducting flame to
minimize oxidation, penetration and inter-alloying. Alloy 6B and 6K should be preheated and maintained at 1000°F (538°C)
minimum to prevent cracking during welding and then still air-cooled.
Fixturing which would chill the weld rapidly should not be used.
Standard weld joints are recommended. Haynes alloy No. 25 or
Hastelloy alloy W filler metals are recommended for joining alloy No.
6B to softer materials such as carbon steel or stainless steel, while
the harder cobalt-based filler metals such as Alloy 6, No.
6B, and No. 21 are recommended for joining alloy No. 6B to itself,
especially if wear resistance is required in the weld areas. In the
latter case, Haynes No. 25 or Hastelloy alloy W may be used for the
root passes and then be overlayed with the harder materials. Gas
shielding of the root side of the gas tungsten-arc weldments is not
mandatory, but it is recommended in order to improve weld penetration.
Brazing
Alloys No. 6B and 6K are readily
joined to other materials by brazing. All forms of surface dirt such
as paint, ink, oil, chemical residues, etc., must be removed from the
mating parts by etching, solvent scrubbing, degreasing, or other
means. In addition, fluxing will be required during torch brazing
operations when using silver brazing filler metal, to help clean the
joint and allow the filler metal to flow more freely over the mating
surfaces. Brush joining areas generously with brazing filler metal
melts, the source of heat should be removed and the parts positioned.
The assembly should then be pressed together to squeeze out the
excess flux and still air-cooled. The part should not be
quenched. Other brazing filler metals (i.e., gold, palladium, or
nickel-based alloys) are satisfactory for joining alloys No. 6B and
6K. Brazing filler metal selection depends on the service conditions
expected. A close fit of the mating surfaces is recommended. The
finished joints will have greater strength if the filler metal is
very thin, generally 0.001-0.005" (0.03-0.14 mm) thick. Brazing,
with high-temperature filler materials, is generally performed in a
furnace. Induction and resistance heating with salt-bath and
metal-bath dip brazing have limited application. Vacuum furnaces held
at less than one micron pressure or controlled atmosphere furnaces,
having adequate moisture control at brazing temperatures (less than
-60°F (-51°C) dew point), produce the most satisfatory
results. Controlled atmospheres such as hydrogen or cracked ammonia
are suitable for brazing alloys No. 6B and 6K base materials.
Machining
Alloys No. 6B and 6K are machined
with tungsten-carbide tools. Carbide inserts are used with a 5-degree
(0.09 rad.) negative tool holder and a 30-degree (0.52 rad.) or
45-degree (0.79 rad.) lead angle. Tools for facing or boring are
essentially the same except for greater clearances where needed. For
best results in drilling, the drill web should be kept thin. Screw
machine length, carbide tipped drills should be used. In reaming, a
45-degree (0.79 rad.) cutting lead angle should be used. High speed
tabs are not recommended for alloys No. 6B and 6K, but threads can be
produced by EDM techniques. For better surface finish, these alloys
should be ground. The table which follows gives some general
information which may be used as a guide in machining alloys No. 6B
and No. 6K.
Guide
for Machining Alloys No. 6B and No. 6K
Operation
|
Speed SFPM
(m/s)
|
Roughing
|
Finishing
|
Feed per rev. in.
(mm)
|
Depth of cut in.
(mm)
|
Feed per rev. in.
(mm)
|
Depth of cut in.
(mm)
|
Turning*
|
50- (0.25-) 70
(0.35)
|
0.008- (0.20-) 0.012
(0.28)
|
0.050- (1.27-) 0.200
(5.08)
|
0.002- (0.05-) 0.005
(0.13)
|
0.025- (0.63-) 0.007
(0.18)
|
Facing*
|
50- (0.25-) 70
(0.35)
|
0.008- (0.20-) 0.012
(0.28)
|
0.050- (1.27-) 0.100
(2.54)
|
0.006- (0.15-) 0.010
(0.25)
|
0.025 (0.63) or
less
|
Boring*
|
50- (0.25-) 60
(0.30)
|
Depends on bar and
size of tool 0.005- (0.13-) 0.008 (0.20)
|
0.025-
(0.63-) 0.100 (2.54)
|
0.005-
(0.13-) 0.003 (0.08)
|
0.025-
(0.63-) 0.007 (0.18)
|
Drilling**
|
30- (0.15-) 35
(0.18)
|
---
|
---
|
Depends on size of
drills 0.001- (0.03-) 0.005 (0.13)
|
---
|
Reaming***
|
40- (0.20-) 50
(0.25)
|
0.001- (0.03-) 0.005
(0.13) per tooth
|
0.015- (0.38-) 0.030
(0.76)
|
0.001- (0.03-) 0.004
(0.10) per tooth
|
0.007- (0.18-) 0.025
(0.63) (based on dia.)
|
Threading
|
Using single point C-3 tungsten carbide tools. 10-25 SFPM
(0.05-0.13 m/s) based on number of threads per inch (mm).
|
*Use C-3 tungsten
carbide tools. Coolant-water base fluid diluted 15 parts water to one
part fluid. Tools for facing and boring are basically the same as
turning tools except for greater clearance where needed. **C-2
tungsten carbide twist drills with drill web kept as thin as
possible. Coolant - same as item * above ***C-2 tungsten carbide
tools. Reamers should have a 45-degree (0.79 rad.) side cutting edge
angle. Coolant - same as item * above.
Grinding
Whenever close tolerances are
required, grinding is recommended for finishing Alloys No.
6B and 6K. Honing can be used to finish inside diameters. Recommended
wheels and coolants are listed in the table below.
For convenience, the manufacturers of grinding wheels are also
listed; however, similar wheels of other brands can also be used if
desired. Grinding speeds should be kept between 2800 and 6000
s.f.p.m (14-31 m/s). Alloys being ground dry should not be quenched,
because this may cause surface checking.
Types
of Grinding
|
Wheels
|
Wheel
Manufacturer
|
Type
of Work
|
Coolant
|
CYLINDRICAL
GRINDING Straight of Tapered O.D.'s
|
A54-M5-V 19A150-K8-V
|
Precision Norton
|
Sharp corners
and fine finish
|
Emulsifying Oil
|
Form Work,
Single-Wheel Section Method
|
19A60-J-V A100-M-V FA100-L7-V
|
Norton Precision
|
Removing stock Sharp
corner work Straight radius work
|
Emulsifying Oil
|
Form Work,
Crush-Roll Method
|
19A220-L9-VG 19A150-L8-VBE
|
Norton Norton
|
-------------------------
|
"Sultan"
B-6**
|
Centerless
|
ZA60-K9-V1 A150-05-V10 A60-N5-VBE A80-N5-V30
|
Sterling Carborundum Norton Carborundum
|
Thin-walled
material
Solid or heavy walled material
|
1 gal. "Argon"
No. 4* + 50 gal. water
|
INTERNAL
GRINDING Straight or Tapered
|
GA605-J5-V1 A150-05-V10 A60-N5-VBE A80-N5-V30
|
Carborundum Hytens Sterling Norton
|
Small
holes Medium-size holes Large holes Small counterbores
|
1 gal. "Argon"
No. 4* + 50 gal. water
|
SURFACE
GRINDING Straight-Wheel
|
38Z46-I-V 19A46-K-V 32A60-K5-VBE
|
Norton Norton Norton
|
Angles, Radii Forms
|
Emulsifying
Oil Dry Dry
|
Reciprocating
Type
|
38A46-I-V 18A60-L8-V6
|
Norton Macklin
|
Surface, angles,
forms
|
1 part "Vantrol"
523* to 60 parts water
|
Double-Opposed
|
87A46-G12-BV
|
Gardner
|
Through-feed work
|
1 gal. "Argon"
No. 4* + 50 gal. water
|
Disk Type
|
87A46-G12-BW 87A46-I-G10
|
Gardner Gardner
|
Ferris-wheel work
|
1 gal. "Argon"
No. 4* + 50 gal. water
|
Cylinder
or Segmental Type
|
29A46-F10V6 KA46-F-16-V2403
77A46-F8-V6
|
Macklin Sterling
American
|
Thin work Tool
metal Thin work, bevels and close-tolerance work
|
1 lb. Sal Soda to
50 gal. water
|
Profile Work,
Single-Wheel Section Method
|
A
100-L7-V 19A46-K-V 18A60-L8-V6
|
Norton Norton Macklin
|
--- ---
|
Dry Dry or
Emulsifying Oil
|
Profile Work,
Crush-Roll Method
|
A 200-K-V 19A
150-K8-VBE
|
Norton Norton
|
--- Forms
|
"Sultan"
B-6**
|
THREAD
GRINDING External Threads
|
A 120-W2-B7 A
120-T9-BAZ
|
Macklin Bay State
|
Test Bars ---
|
"Vantrol"
5299-M oil
|
HONING Internal
|
IC-220-M12-VL2F LC180-K12-UL2F J45
and 57 J45 or J-55
|
Bay State Bay
State Sunnen Sunnen
|
56N for
finish J45 for fast cutting Inside diameters
|
"Vantrol"
5299-A oil
|
ROUGH
GRINDING Cut-off
|
A24-S10-BKRS 8A366-T6-BB33
|
Sterling Bancroft
|
Gates Slabs
|
Dry
|
Snagging
|
A162-M10-2893 A364-L10-VB
|
Sterling Sterling
|
Welds Gates
|
Dry
|
TA36-N5-V1 IA305-L5-BG4 MTA-161-05-BLS
|
Simonds Bancroft ITT
|
---
|
Dry
|
LAPPING
|
39C180-J9-V
|
Norton
|
Flat work
|
Mixed with kerosene
|
Silicon
Carbide grits 400, 500, 600
|
---
|
Flat work
|
---
|
H-40 Coarse
|
Carborundum
|
Small holes
|
---
|
TUMBLING
|
Aluminum oxide
tumbling abrasive mixed with water and soap
|
*Or any good grade of
water soluble oil **Or any good grade of sulfur-base cutting oil
|