Press Tools
9.Fine
Blanking
9.Fine
Blanking
9.1 FINE-EDGE BLANKING AND PIERCING
Fine-edge
Blanking (also known as fine blanking, smooth-edge blanking, or fine-flow
blanking) produces precise blanks in a single operation without the fractured
edges characteristically produced in conventional blanking and piercing. In
fine-edge blanking, a V-shape impingement ring (Fig. 9-1) is forced into the
stock to lock it tightly against the die and to force the work metal to flow
toward the punch, so that the part can be extruded out of the strip without
fracture or die break. Die clearance is extremely small, and punch speed much
slower than in conventional blanking.
Fine-edge piercing can be done either separately or at the same time as fine-edge blanking. In piercing shall holes, an impingement ring may not be needed.

No further finishing or machining operations are necessary to obtain blank or hole edges comparable to machined edges, or to those that are conventionally blanked or blanking a simple shape.pierced and then shaved. A quick touchup on an abrasive belt or a short treatment in a vibratory finisher may be used to remove the small burr on the blank.
Specially designed single-operation or compound blanking and piecing dies are generally used for the process.
9.2 PROCESS
CAPABILITIES
Holes
can be pierced in low-carbon steel with a diameter as small as 50% of stock
thickness. In high-carbon steel, the smallest hole diameter is about 75% of
stock thickness. Holes can be spaced as close to each other, or to the edge of
the blank, as 50 to 75% of stock thickness. Total tolerances obtainable are:
0.0125 mm. on hole diameter and for accuracy of blank outline; 0.025 mm. on
hole location with respect to a datum surface and 0.025 mm. on flatness.
No
die break shows on the sheared surface of the hole. Blank edges may be rough
for a few thousandths of an inch of thickness on the burr side of the part when
the width of the part is about twice the stock the stock thickness or less.
Finish on the sheared edge is governed by the condition of the die edge and the
land within the die. Parts fine-edge blanked from stainless steel will have a
surface finish of 1.3 micro-mm. or better. Smooth edges also are produced on
spheroidize-annealed steel parts. Burr formation increases rapidly during a
run, necessitating frequent grinding of the cutting elements.
Chamfers
can be coined around holes and on edges. Forming near the cut edge, or forming
offset parts with a bend angle up to 30°, is possible under restricted
conditions.
Metals
up to 3.2 mm. thick having a tensile strength of 6,000 to 8,000 Kg. / sq. cm.
are easily blanked. Parts up to 13 mm. thick can be blanked if press capacity
is available. Material thicker than 3.2 mm., especially steel having a carbon
content of 0.25% or more, requires an impingement ring on the die so that the
corners on the part will not break down. The edges of parts made of 1018 steel
work harden as much as 7 to 12 points Rockwell C during blanking.
In
tests on 0.60% carbon spring steel with a hardness of Rockwell C 37 to 40, the
surface finish on the sheared edges was 32 micro-in. or better, but punch life
was only 6000 pieces. The cutting speed for fine-edge blanking is 7.6 mm. to
15.2 mm. per sec.
9.3 WORK
METALS
Low-carbon
and medium-carbon steels (1008 to 1035), annealed or half-hard, give good
blanked edges and normal tool wear. High-carbon steels in the
spheroidize-annealed condition can be blanked easily; blanking of steel with
0.35% carbon or higher is recommended only when it is spheroidize-annealed.
Steels quenched and tempered to about Rockwell C 30 are well suited to
fine-edge blanking, because they do not require subsequent heat treatment,
which could result in deformation.
High-carbon
steels and alloy steels such as 4130, 4140, 8620 and 8630 cause considerably
higher tool wears than low-carbon plain carbon steels, but surface finish is
smoother. Leaded steels are not suitable for fine-edge blanking because of
their low deformability.
Parts
made of stainless steels of types 301, 302, 303, 304, 316, 416 and 430 in the
form of bright rolled fully annealed strip, have good blanked edges, but cause
higher tool wear than steels of low and medium carbon content.
Good
results have been experienced with aluminum alloys 1100 (all tempers), 5052-O
to 5052-H38, 6061-O to 6061-T6 and others having similar yield strength and
elongation. Blanked edges on parts made of aluminum alloy 2024 generally are
rougher than edges on other aluminum alloys. Brasses containing more than 64%
copper are especially suitable. Nickel alloys, nickel silver, beryllium copper
and god and silver also are easily fine-edge blanked.
9.4 BLANK
DESIGN
Limitations
on blank size depend on stock thickness, tensile strength and hardness of the
work metal, and available press capacity. For example, perimeters of
approximately 63.5 cm. can be blanked in 3.2 mm. thick low-carbon steel (1008
or 1010). It is possible to blank smaller parts from low-carbon or
medium-carbon steel about 12.7 mm. thick.
Sharp
corner and fillet radii should be avoided when possible. A radius of 10 to 20%
of stock thickness is preferred, particularly on parts over 3.2 mm. thick or
those made of alloy steel. External angles should be at least 90°. The radius
should be increased on sharper corners or on hard materials.
Parts
with tiny holes or narrow slots to be pierced or with narrow teeth or
projections to be blanked may be unsuited to fine-edge blanking. The ratio of
hole diameter, slot width, or projection width to metal thickness should be at
least 0.7 for reasonably efficient blanking, although a ratio as small as 0.5
has been successful with some parts. The spacing, between holes or between a
hole and the edge of the blank should not be less than 0.5 to 0.7 times metal
thickness. In order to maintain the quality of hole-wall and blank-edge
surfaces, and to avoid distortion.
These
limitations have been exceeded. For instance, a 16-mm. dia. hole was pierced in
each end of a 1018 steel link 25 mm. wide and 8 mm. thick. Since the part had a
12 mm. radius on each end the wall thickness was 5mm. The part was offset 2.5
mm. in the same die. In a part made of 4 mm. thick aluminum alloy 5052-H34, 3.2
mm. dia. holes were pierced leaving a wall thickness of 0.1 mm. A 15.8 mm. dia.
hole was pierced in the same part.
The
sheared faces of holes pierced during fine-edge blanking are usually break,
provided the maximum hole dimensions are not more than a few times the stock
thickness. As in conventional piercing, there is a slight radius around the
punch side of the hole, but there are no torn edges on the die side of the
blank. A rough sheared surface on the blank may be caused by too great a
punch-to-die clearance or improper location and height of the impingement ring
for the material being blanked. On parts blanked to a small width-to-thickness
ratio, a small rough surface may be noticeable, but may not be detrimental (see
Example 1).
9.5 PRESSES
A
triple-action hydraulic press or a combination hydraulic and mechanical press
is used for fine-edge blanking. The action is similar to that of a
double-action press working against a die cushion. An outer slide holds the
stock firmly against the die ring and forces a V-shape impingement ring into
the metal surrounding the outline of the part. The
stock is stripped from the punch during the upstroke of the inner and outer
slides. An inner slide carries the
blanking punch. A lower slide furnishes the counteraction to hold the blank
flat and securely against the punch. This slide also ejects the blank.
The
stripping and ejection actions are delayed until after the die has opened at
least to twice the stock thickness, to prevent the blank from being forced into
the strip, or slugs from being forced into the blank. Because loads are high
and clearance between punch and die is extremely small, the clearance between
the gibs and press slides must be so close that they are separated by only an
oil film.
Force
requirements for fine-edge blanking presses are influenced not only by the work
metal and the part dimensions, but also by the special design of the dies and
pressure pads used for fine-edge blanking. Depending on part size and shape, a
100-ton press can blank stock up to 8 mm. thick; a 250-ton press, up 12 mm.
thick; and a 400-ton press, up to 13mm. thick.
The
total load on the press in fine-edge blanking is the sum of three components:
the cutting force (Lc); the lower blank holder force (LLB) or
counterforce and the clamping force on the impingement ring (LLR) on
the pressure pad. The first two components comprise the total force on the
inner slide, and the third component is the force on the outer slide.
The
cutting force, in Kgs., is calculated from the equation: Lc = 0.8 S lB
t
Where
0.8 is an experimentally determined constant; S is the tensile strength of the
work metal, kg/cm.²; lB is the total length of cut (sum of
perimeters of blank and holes pierced in blank), cm. and t is the thickness of
the work metal, cm.
The
counterforce, or lower blank-holder force, in pounds, is calculated from the
equation: LLB = Pc
A
Where Pc is the counter pressure on the lower side of the blank, psi; and A is the area of the blank, sq. in. The counter pressure usually is about 10% of the tensile strength of the work metal. The clamping force on the impingement ring on the pressure pad, in pounds, can be obtained from: L IR = Lr l IR

Where LI is the force to embed a 1-in. Length of the impingement ring into the work metal, lb; and l IR is the total length of the impingement ring, in. The force L I for different work metals, as determined by experience in fine-edge blanking, is given in Fig. 9-2. When impingement rings are used on both the pressure pad and the die, the calculation of force is still based only on the pressure-pad impingement ring.
The
reduced height of impingement rings when used in pairs allows the use of a
lower clamping force, and thereby reduces the over-all load on the press. This
is because the lower impingement ring is impressed into the work piece by the
reaction force.
If
coining, embossing or other forming is done during the blanking, the additional
force required for those operations must be added to the force requirements as
calculated above.