Supervised autonomous robotic system for complex surface inspection and processing
US-9796089-B2 · Oct 24, 2017 · US
US11625514B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11625514-B2 |
| Application number | US-202117614569-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 18, 2021 |
| Priority date | Aug 13, 2020 |
| Publication date | Apr 11, 2023 |
| Grant date | Apr 11, 2023 |
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The present disclosure provides a numerical simulation method of pulsed laser paint removal and a use thereof. This method establishes a three-dimensional (3D) temperature field model by ANSYS software to perform a numerical simulation of nanosecond pulsed laser paint removal. A high-speed moving pulsed laser is loaded on a surface of the model in a form of heat flux, and a coordinate system is moved to realize loading on different paths. A special surface mesh screening method is used to realize loading on any surface, and it ensures that laser energy distribution on a material surface is in line with reality. In addition, an element birth/death technology is combined to remove an element that exceeds a threshold, so as to intuitively present the surface morphology after laser paint removal. The present disclosure can realize the prediction of the contour of a paint layer ablated by a pulsed laser.
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What is claimed is: 1. A numerical simulation method of pulsed laser paint removal, comprising the following steps: step 1: establishing a two-layer three-dimensional (3D) solid model of a paint layer and a substrate, and conducting meshing, wherein in the 3D solid model, a selected element type is an 8-node hexahedral thermal element; step 2: setting an initial condition of a temperature field of the model to an ambient temperature, and setting a load option to transient analysis and a load mode to step load; step 3: establishing a coordinate system with a center of a single-pulse spot on an upper surface of the paint layer as an origin, taking an axial incident direction of a laser as a z-axis, taking the origin of the coordinate system as a pulsed laser loading position, and defining the upper surface of the paint layer as a z=0 plane; step 4: selecting nodes having a perpendicular distance not exceeding a radius of the spot from the z-axis in the 3D solid model to form a laser irradiation coverage zone, and selecting nodes with less than 8 surviving elements attached, among the nodes in the laser irradiation coverage zone, to form a laser irradiated surface; step 5: loading a pulsed laser onto a surface of the model in a form of heat flux, the elements attached to the nodes at the laser irradiated surface being laser irradiated elements; and calculating an energy load q received by a node on an upper surface of a laser irradiated element whose center has a distance of h from the z-axis: q ( h , t ) = 12 · aP f τ · π d 2 · exp ( - 12 · h 2 d 2 ) · ( t τ ) 7 exp [ 7 ( 1 - t τ ) ] ( 1 ) wherein, a is an absorption rate of laser energy by a material, P is a laser output power, f is a laser repetition frequency, d is a spot diameter, τ is a laser pulse width, and t is a time, 0<t<τ; step 6: performing iterative solution in a form of time integration according to a heat conservation law of a heat transfer theory, to calculate an instantaneous temperature of each of the nodes; and step 7: defining an instantaneous temperature of the surviving elements reaching a threshold temperature or above as a condition for an element birth/death operation, and killing a surviving element whose instantaneous temperature exceeds the threshold temperature, to obtain morphology after the removal of the paint layer by a single pulsed laser. 2. The numerical simulation method of pulsed laser paint removal according to claim 1 , wherein the threshold temperature is a vaporization temperature of a material of the paint layer. 3. The numerical simulation method of pulsed laser paint removal according to claim 1 , wherein the heat conservation law of the heat transfer theory is that a temperature change of the material subjected to laser irradiation satisfies: ∂ T ∂ t = k ( ∂ 2 T ∂ x 2 + ∂ 2 T ∂ y 2 + ∂ 2 T ∂ z 2
using finite element methods [FEM] or finite difference methods [FDM] · CPC title
taking account of the properties of the material involved · CPC title
by shaping pulses · CPC title
Numerical modelling · CPC title
Design optimisation, verification or simulation (optimisation, verification or simulation of circuit designs G06F30/30) · CPC title
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