Printing of three-dimensional metal structures with a sacrificial support
US-10633758-B2 · Apr 28, 2020 · US
US11618953B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11618953-B2 |
| Application number | US-202117303940-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 10, 2021 |
| Priority date | Nov 23, 2016 |
| Publication date | Apr 4, 2023 |
| Grant date | Apr 4, 2023 |
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Official abstract text for this publication.
A system for laser-driven propulsion, system comprising a laser source and a target comprising an accelerating part and a projectile part, the accelerating part comprising a metal layer and a porous layer pressed against the metal layer; wherein the laser source is selected to emit pulse beams directed to the metal layer at a fluence below the plasma ablation threshold of the material of the metal layer.
Opening claim text (preview).
The invention claimed is: 1. A system, comprising: a metal layer having a first surface and a second opposite surface; a porous layer having a first surface and a second opposite surface; the porous layer being positioned with the first surface thereof in direct contact with the second surface of the metal layer, and a projectile, said projectile being positioned on the second surface of the porous layer; and a laser source; wherein said laser source is selected to irradiate the first surface of the metal layer with laser pulses of a fluence between 1 J/cm 2 and 3 J/cm 2 to temperatures below the liquefaction and ionization thresholds of the metal, thereby generating a pressure wave in the metal layer; the pressure wave propagates and compacts pre-compacted powder of the porous layer, thus creating a cavity; and the cavity transfers momentum to the projectile. 2. The system of claim 1 , wherein a thickness of the metal layer is selected with a thickness in a range between 1 μm and 50 μm and a thickness of the porous layer in a range between 10 μm and 100 μm. 3. The system of claim 1 , wherein said laser source is selected to emit pulse beams of a duration in a range between 10 ps and 50 ns at the fluence in the range between 1 J/cm 2 and 3 J/cm 2 . 4. The system of claim 1 , wherein said target comprises a transparent layer at the first surface of the metal layer irradiated by said laser source. 5. The system of claim 1 , wherein said target comprises a transparent layer at the first surface of the metal layer irradiated by said laser source, said metal layer having a thickness in a range between 1 μm and 50 μm, said porous layer having a thickness in a range between 10 μm and 100 μm and said transparent layer having a thickness in a range between 500 μm and 1 cm. 6. The system of claim 1 , wherein the pre-compacted powder is selected with a selected pre-compaction density. 7. The system of claim 1 , wherein the metal layer and the porous layer are in materials selected for shock impedance matching. 8. The system of claim 1 , wherein the porous layer is part of the projectile. 9. The system of claim 1 , wherein the projectile is an array of micro-dots. 10. The system of claim 1 , wherein the projectile is a foam.
Arrangements or adaptations of propulsion systems · CPC title
Solid propellant rocket engines · CPC title
using absorbing layers on the workpiece, e.g. for marking or protecting purposes · CPC title
by laser shock processing · CPC title
by shot-peening or the like · CPC title
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