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March 2005
Laminar gas flows ensure 'clean sweep' in sintering
Metal injection moulding can provide design engineers with
economic solutions to otherwise apparently insoluble part
production problems. But although MIM's 'can-do' abilities
open the way to design freedom, care is needed at all stages
of the process. The debinding and sintering of parts are critical
steps…
Powder injection moulding (PIM) is a manufacturing technique
that encompasses metal powder injection moulding (MIM), ceramic
powder injection moulding (CIM) and cemented carbide powder
injection moulding (CCIM). All three processes combine the
attributes of plastic injection moulding with the engineering
and performance properties of metals, ceramics, and cemented
carbides.
In this article Claus Joens of PVA MIMtech's Elnik Systems
looks at some of the problems associated with the thermal
debind and sinter technology of metal injection moulded parts
- and their solutions.
MIM is a process where fine metal powders are mixed with
a variety of binders to create thermoplastic feedstocks that
can be injection moulded. They are then debound and sintered
to full densities to attain the desired mechanical and physical
properties.
The advantages of MIM are:
• Excellent shaping possibilities;
• Complex shaped parts can be manufactured with very
little secondary finishing. For example, undercuts in parts,
which are not possible with conventional sintering processes,
can be easily achieved;
• Excellent surface quality when compared to precision
cast parts. Finishing and polishing costs can be eliminated
or greatly reduced;
• Excellent material properties;
• Parts reach densities of 96 per cent to 100 per cent
of the theoretical material density;
• Very close tolerances. Parts are dimensionally accurate
by a range of better than +/- 0.05 per cent; and
• A wide material selection. The great variety of metal
powders and binders available cater for a broad spectrum of
design needs. The harder it is for a part to be machined,
the more advantageous the MIM process becomes.
The MIM process exhibits great cost effectiveness in producing
complex parts. In fact, the more complex the part, the more
suited this process becomes (and therefore the greater the
cost savings.) Additionally, this process allows mixing of
different metal powders with binders so that it is possible
to engineer a part with very specific thermal, wear, magnetic
and strength properties.
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Figure 1. Critical issues in thermal debinding
- Debinding takes place by diffusion and permeation
of the vapourised binder via the pores.
- The thermal debinding process converts the binder
to a vapour.
- The transport distance 'L' of the vapourised binder
to the surface increases over time.
- Laminar gas flow ensures an even binder evolution
and no redeposition of binder on the part.
- The thickest sections of the part limit the debind
cycle time
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The MIM process also yields net shape components with little
or no secondary operations. This simplifies production, increasing
yields and lowering the manufactured cost of the part.
The MIM process has four key manufacturing elements:
• The creation of the feedstock;
• The injection moulding cycle;
• The solvent/chemical debind cycle; and
• The thermal debind and sinter cycle.
During thermal debind and sinter, the component part is heated
and may be subjected to undesired binder reactions with the
powder along with shrinkage and thermal stresses. These are
contributors to cracked, warped, chemically incorrect parts
with poor density and of varying and incorrect sizes because
the entire process requires very accurate and repeatable control.
The goal of the thermal debind step is to remove the majority
of the binder which evaporates at low temperatures, leaving
the backbone polymer to hold the powder particles in place
so that the part can be sintered. This backbone polymer evaporates
when the furnace goes up to sintering temperatures, then the
part starts to sinter just before it densifies.
The thermal debind process converts the binder to a vapour
that diffuses and permeates through the pores to the surface
of the part. The critical issue here is an even binder evolution
and a sweep of gas flow around the part to ensure no re-deposition
of binder on the part.
An even flow all around that part ensures that all of the
binder is extracted; during the sinter phase, when the pores
begin to close, there is no binder left behind. With no excess
binder to contaminate or distort the part no unwanted physical
effects such as blistering are seen and no difficulties arise
with density and chemical composition, such as carbon control
in stainless steel.
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Figure 2. The process gas flows from the
gas distribution holes across the shelves and parts
to the centre of the furnace. It is preheated by heating
elements and flows into the furnace at a higher temperature
than the internal furnace temperature. The design
ensures short gas flows to the centre of the furnace
giving a constant clean gas flow across the parts.
The centre area where gas is evacuated through the
manifold vacuum ports is a few degrees colder, guiding
the gas across the parts.
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In the early days of MIM processing it was quite usual to
thermally debind the part in an air, vacuum or atmospheric
nitrogen or hydrogen oven, depending on the material and the
binder.
Today, there is another binder material which catalytically
erodes the polyacetal used as the binder via nitric acid vapour.
This requires a specially designed oven. The process works
from the outside of the part to the inside, unlike the wax/polymer
binder. However, both debinding times are a direct function
of the thickness of the part. This means that the thickest
part governs the total cycle time.
The problem with the ovens used originally was that there
was no even gas flow. They also exhibit large thermal gradients.
Both conditions create poorly debound parts through re-deposition
of binder components on the parts and also contribute to contamination
on the inside of the furnace.
This is not a problem with polyacetal binders since their
removal is a chemical reaction. This binder is not offered
for some metal powders and its removal requires a special
catalytic debind oven. Parts after catalytic debinding are
very fragile and their brown strength is a critical issue
not found with wax/polymer binders. Damage to the brown parts
during their transfer to the sinter furnace is an issue that
merits consideration.
The double debind-sinter cycle is time consuming and expensive
in terms of power used, since the parts area heated to debind
temperature, cooled, then transferred to the sinter furnace,
heated again to sinter temperature and cooled.
To overcome the problems of long process cycle times and
breakage, a furnace with partial pressure operation in the
range of 1 to 760 Torr was built to combine the thermal debind
and sinter cycle in one step. This furnace design, with built-in
retort and gas management system allows processing the injection
moulded part under "laminar gas flow". This eliminates
the contamination issues associated with the debind ovens
of earlier days.
In this furnace design, the process gas flows from the distribution
holes across the parts to the centre of the retort through
the gas manifold with its inlet and outlet passage ways.
The gas is preheated by the heating elements, which guarantees
the flow to the center of the retort.
While the physical attributes of the furnace are important
in directing the gas flow, the type of flow is critical to
the success of the laminar gas flow design. The three different
principal gas flows are turbulent, laminar and molecular.
At an atmospheric pressure of 760 Torr, (typical for air
or controlled gas ovens) the gas molecules flow at high pressure
and velocity, colliding with each other. This creates uneven
flow and shadow effects on the parts with consequent uneven
debinding.
At a molecular flow of 1 Torr or less, (typical for vacuum
ovens) the gas molecules collide with each other randomly
and gas flow becomes unpredictable. The gas flow also escapes
to the cold walls of the oven, creating random flow on the
parts and contamination inside the furnace.
At a laminar flow of around 300 Torr, the gas molecules flow
at sufficient velocity to flow smoothly and evenly over surface
irregularities. This creates an even flow and no shadow effects,
much as if the parts were submerged in a liquid.
What exactly is laminar gas flow, and what are the benefits?
Figure 3 shows turbulent flow, which results in greatly separated
flow at the back side of the part. This uneven flow creates
an uneven temperature distribution on the part resulting in
different debinding and sinter results.
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Figure 3. Low gas velocity results in a high
Reynolds number (indicating turbulence) and greatly
separated flow.
An uneven gas or temperature distribution at the product
leads to different debinding results, most common
in vacuum furnaces with a sweep gas option.
Only even flow round the product causes a continuous
and even debinding as shown in Figure 5.
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Figure 4 shows that by lowering the density of the gas via
partial pressure, we provide a greater chance of laminar flow
with less separation at the back side of the part. This can
be measured by calculating the Reynolds number, indicative
of turbulence, which decreases under partial pressure. And
by lowering the density, we achieve a higher gas velocity.
This in turn creates a thinner viscous boundary layer, which
allows for greater thermal transfer.
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Figure 4. Lowering the density of the gas
via partial pressure results in a lower Reynolds number,
providing a greater chance of laminar flow with less
separation. Higher gas velocity creates thinner viscous
boundary layers that allow for greater thermal transfer
and a lower Reynolds number.
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Figure 5 shows the ideal laminar flow, which guarantees an
even and continuous debinding of the part, since all gas moves
in a predictable way. Additionally, laminar gas flow moves
the process gas to the centre of the retort. This is where
the binder contaminant is pulled through the gas manifold,
ending up in an easily cleanable debind trap. The binder contaminants
cannot redeposit on either the parts or the cold walls of
the furnace as in atmospheric of vacuum furnaces. The advantage
of a furnace equipped for partial pressure operation is the
flexibility it creates. The profile parameters can be tailored
specifically to the concerns of the material. Three such concerns
are: the slow ramping during specific temperature phases,
the variation of partial pressure, and the mix of gas to obtain
surface finishes. All three contribute to the great variety
of materials such a furnace is capable of running. The range
extends from iron through steel, stainless steel, tool steel,
high-temperature alloys such as Inconel 718 and Hastelloy
X, to titanium and tungsten compounds including tungsten carbide.
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Figure 5. Lowering the Reynolds number overall
creates conditions that approach ideal laminar flow,
as shown in Figure 5, creating even and continuous
debinding.
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The heating inside this furnace is accomplished partially
by radiation and partially by convection. This depends on
the partial pressure and the resulting temperature uniformities.
The temperature uniformity varies greatly under the conditions
from vacuum to different partial pressures as well as different
temperature levels and type of gas.
The ability to change the partial pressure, gas type and
flow allows this furnace to process any MIM material with
any binder component. Some materials require a higher partial
pressure during sintering to prevent the evaporation of material
components such as copper in stainless steel.
Additionally, laminar gas flow allows different sized parts
to be processed in the same furnace envelope in the same process
run. This is because gas flows evenly from both sides to the
centre, which guarantees perfect product results every time,
regardless of whether the furnace is fully loaded with identical
parts or differently sized ones. There is no shadow effect
under laminar gas flow.
Several case studies show the benefits of laminar gas flow.
In the first case, an electronic housing was being produced
in a separate debind oven. By using a laminar flow partial
pressure furnace a cycle time reduction of 45 hours from 60
hours to 15 hours was achieved, saving considerable amounts
in terms of consumables costs - electricity and gas consumption.
At the same time, the carbon control and the dimensional characteristic
of the part were greatly improved.
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Figure 6. A typical partial pressure furnace
can handle applications up to 1650oC with six individually
controlled heating zones. The makers say this results
in temperature uniformity better than ± 3oC.
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In the second example a ring mount was made from carbon steel
made in the traditional way. It had high porosity (7.04 g/cc),
a high oxygen content (0.60 per cent), poor carbon control
(+/-0.02 per cent), and poor dimensional control and concentricity.
When the same part was made in a partial pressure furnace
under laminar gas flow conditions, that part exhibited very
low porosity (7.76 g/cc), low oxygen content (0.11 per cent),
acceptable carbon control (+/- 0.01 per cent) and excellent
dimensional control and concentricity.
Batch furnaces with laminar gas flow capability have shown
to be advantageous in all respects. It provides complete debinding.
It ensures temperature uniformity during debind and sinter.
It eliminates evaporation of key constituents of the part
and it provides versatility and flexibility in producing the
largest variety of PIM/MIM parts. And importantly, it eliminates
a separate thermal debind step. All of these benefits prove
that the batch furnace is able to improve all properties of
the part, and to re-duce cycle time and utility consumption.
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