Unterschiede
Hier werden die Unterschiede zwischen zwei Versionen angezeigt.
| Beide Seiten der vorigen RevisionVorhergehende ÜberarbeitungNächste Überarbeitung | Vorhergehende Überarbeitung | ||
| en:berechnungen:druckverlauf [2024/10/17 20:04] – [Pressure profile] neelest | en:berechnungen:druckverlauf [2025/07/03 13:34] (aktuell) – cschall | ||
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| ======Pressure profile====== | ======Pressure profile====== | ||
| - | ===== Pressure profile ===== | + | -> [[en: |
| - | In order to calculate the pressure profile | + | To calculate the pressure profile, the same conditions as for throughput and dosing |
| - | as for the throughput calculation of both the throughput and the metering | + | |
| - | calculation. This also applies | + | |
| - | [[en: | + | |
| [[en: | [[en: | ||
| - | and [[en: | + | and [[en: |
| - | Additionally, | + | Additionally, |
| - | profile | + | The same equations as those used in the throughput calculation are applied. |
| - | The pressure profile is calculated back to the point of melt pool formation | + | The pressure profile is calculated |
| - | possible to determine the point of melt pool formation on account of missing data, | + | |
| - | REX/PSI will calculate | + | |
| - | edge of the hopper to the last point calculated is reflected by a logarithmic | + | |
| - | formulation. | + | |
| - | The pressure profile calculation | + | The pressure profile calculation |
| - | used to determine | + | |
| - | added to the previous absolute pressure. | + | |
| - | screw tip) results from the adjusted impact | + | |
| - | The pressure profile is calculated isothermally at the melt temperature | + | ==== Pressure Profile Calculation |
| - | and is subsequently multiplied by a correction factor. This correction factor has in | + | |
| - | physical terms the effect that the calculation performed at a temperature that permits | + | |
| - | the pressure and throughput behavior to coincide. This is necessary, since the | + | |
| - | throughput has to be calculated on the basis of a mixed isothermal/ | + | |
| - | formulation while the pressure profile has to be calculated either isothermally or nonisothermally. | + | |
| - | ==== Pressure | + | === Assumption of Equal Pressure |
| + | Barrier screws can only be calculated analytically under the simplifying assumption of an equal pressure gradient in the melt and solid channels. Although this allows for rapid calculation, | ||
| - | In order to calculate the barrier screw in the way described a constant pressure | + | === Network Calculation / Matrix |
| - | gradient has to be assumed. However, since every additional assumption increases | + | |
| - | inaccuracy, the so-called "Matrix | + | |
| - | assumption. Its calculation method is similar to the FEM calculation method. | + | |
| - | Here, single intervals are built for barrier flight, solid and melt channel and for each | + | To eliminate |
| - | section between | + | |
| - | means of a linear equation. These equations form a linear system of equations. The | + | |
| - | equations only describe the development of the flow in the direction of the channel, | + | |
| - | which means that the mesh of the division of the geometry into the required intervals | + | |
| - | corresponds to constant conditions. | + | |
| - | {{ : | + | This method is optionally available for barrier screws as an alternative to the equal pressure gradient assumption but is always used for wave screws. |
| - | Before | + | A network is generated from the screw geometry, consisting of simple geometries (rectangular channels). For each of these simple geometries, a //voltage source// (drag flow) and a resistance (pressure flow) are defined. From the network of voltage sources and resistances, |
| - | to solve linear equation systems, it is first necessary to reduce | + | |
| - | reduction is achieved by allowing boundary conditions. | + | |
| - | {{ :en: | + | {{ : |
| - | In the closed barrier | + | To solve the resulting system of equations, it must be reduced by incorporating boundary conditions. |
| - | last node in the channel direction, | + | For a closed barrier |
| - | barrier section | + | |
| - | in order to be able to calculate this design. Because | + | |
| - | separation, the pressure difference between the first and last nodes of the solids and | + | |
| - | melt channel | + | |
| - | For a clear-cut solution of the system it is necessary to know about the mass flow. | + | {{ : |
| - | Here an iterative calculation helps, i.e. in the first step, the pressure-throughput | + | |
| - | behavior of the standard sections is calculated for a known pressure at the screw tip | + | |
| - | without considering the barrier section. In the second step, this throughput is taken to | + | |
| - | solve the equation system for the barrier section. Since the overall pressure | + | |
| - | requirement for the screw is equal to the sum of the pressure requirements of the | + | |
| - | individual screw sections, the calculated pressure requirement for the barrier section | + | |
| - | can be added to the pressure requirement of the remaining screw sections that was | + | |
| - | calculated in the first step. | + | |
| - | + | ||
| - | + | ||
| - | ==== Druckverlaufsberechnung für Wave-Schnecken ==== | + | |
| - | + | ||
| - | ToDo: Anpasssen wenn MA Gödeke fertig ist | + | |
| + | ===Further topics=== | ||
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