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Near Net Shape Manufacturing of CuCr Vacuum Switching Contacts ...

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WS 15/8 17th Plansee Seminar 2009, Vol. 3 Feist, Oberbreyer et al.<br />

(5)<br />

q<br />

(3)<br />

d<br />

(4)<br />

tan β<br />

1<br />

p a<br />

ferent level <strong>of</strong> triaxiality is used (e.g. a four-point bending test, Fig. 3a, (5)) determination <strong>of</strong> the strength<br />

parameters becomes over-determine which can help reducing potential errors by means <strong>of</strong> least-squareroot<br />

minimization. Alternatively, a higher order shear-failure surface could be determined from these test.<br />

¥<br />

p b<br />

(1)<br />

p<br />

(2)<br />

d<br />

d 2<br />

d 3<br />

d1 ¥0<br />

¥2<br />

¥3¥th<br />

(a) (b)<br />

Figure 3: Mechanical powder-characterization: (a) experimental determination <strong>of</strong> cap- and shear-failure surface parameters,<br />

(b) density dependence <strong>of</strong> cohesive strength d.<br />

The obtained shear-failure surface (in terms <strong>of</strong> d and β) is only valid for the given density-level ρ1 (Fig. 3).<br />

In order to determine the density-dependence <strong>of</strong> the strength parameters similar tests must be conducted<br />

at various other density levels ρ2, ρ3 . . . (Fig. 3b) relevant for PM production purposes. The obtained discrete<br />

values d1, d2 . . . and β1, β2 . . . for simulation purposes will be fitted using an appropriate regressionfunction<br />

(9b, c) (see Fig. 3b in case <strong>of</strong> cohesion d), which will be used to interpolate or extrapolate the<br />

strength parameters at any density ρ.<br />

Analytical assessment <strong>of</strong> PM-processed parts<br />

When designing the process-plan for a component to be produced on the PM manufacturing route the<br />

designer is mainly confronted with the question on how to arrive at the final nominal geometry. In particular<br />

he has to determine all relevant process-parameters like the geometry <strong>of</strong> the die, the fill-height <strong>of</strong><br />

the powder-body, the required powder mass, the tools, their travel during compaction, the remaining axial<br />

force during ejection etc. This in most <strong>of</strong> the cases is done on a combined basis <strong>of</strong> experience and trialand-error<br />

approaches.<br />

In this respect, finite element analyses based on the described mathematical model can only help in accelerating<br />

the iterative trial-and-error procedure by virtually conducting the required experiments. However,<br />

also for the numerical simulations the process-parameters as given above have to be explicitly estimated<br />

or prescribed, respectively. This follows from the fact that the described mathematical model exactly<br />

represents the manufacturing process and follows the direction <strong>of</strong> its work-flow.<br />

In this context it is desirable to obtain appropriate initial estimates for the process-parameters serving as<br />

a valid initial guess for numerically simulated or experimentally conducted process-experiments. These<br />

initial estimates in principle should be obtained by starting from the nominal geometry <strong>of</strong> the component<br />

and stepping the entire process-chain right back to the fill-state. Through the irreversible character <strong>of</strong> the<br />

mathematical relationships employed for describing the constitutive state both in the compaction and sintering<br />

step, this however is only possible for very simple geometries based on analytical solutions under<br />

some assumptions:

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