1. Introduction
Direct energy deposition (DED) stands out among additive manufacturing (AM) technologies due to its high productivity of geometries with near-to-optimal shapes. The capability of multi-axis material delivery as powder or wire enables the creation and repair of complex geometries, large-scale parts, and multi-grade materials, aligning with the demands of aerospace applications [
1,
2,
3]. This advantage of material delivery in DED comes with significant challenges. Unlike powder bed processes, where the powder is laid statically, the DED material’s dynamic delivery complicates the heat dissipation [
4,
5]. The continuous and localized addition of material generates varying heat intensities and gradients, leading to a complex thermal profile within the heat-affected zones. This complexity in heat management can result in various defects and the absence of consistent and standardized process output characteristics. The non-uniform cooling, the heat accumulation, and the re-melting of built layers during the disposition of new ones lead to micro and macro defects such as geometric and dimensional distortion, surface and internal cracks, and porosity formation [
6]. Consequently, a large body of literature focuses on developing different monitoring and control systems to improve the reliability and repeatability of DED processes [
7].
Humping is a phenomenon that significantly reduces the geometrical accuracy of the produced products.
Figure 1a shows a severe manifestation humping, demonstrating the formation of crests and valleys that contribute to the characteristic wavy structure. During humping, the melt pool goes through a series of abnormal solidification dynamics (i.e., modes). Transitioning between these different modes depends on the humping severity, as shown in
Figure 1. Panels (b to f) showcase the different melt pool modes associated with humping, with the severity increasing progressively from (b) to (f). Additionally, within each panel, time progresses from the top to the bottom (e.g., b.1 precedes b.2). Starting with the normal mode, in
Figure 1b.1 and 1.b.2, the melt pool (MP) shows a temporally invariant shape. This temporal invariant shape implies that the solidification front (SF) speed matches the laser speed. Thus, the relative velocity between the laser and solidification front at the melt pool tail is almost zero. The initial stage of humping starts with the MP elongation mode. In this mode, the MP shows cyclic behavior, alternating between long (
Figure 1c.1) and short melt pools (
Figure 1c.2). This variation in melt pool size indicates inconsistent solidification front velocity direction (SFD), which is the direction of the relative velocity between the solidification front and the scanning speed, as shown by the orange arrows in
Figure 1c. A negative SFD means that the solidification front is moving away from the laser, and the liquid is accumulating at the MP tail, as shown in
Figure 1c.1. Conversely, a positive SFD indicates liquid solidifing at the tail, causing a shorter MP. Despite this fluctuation in the SFD, the degradation of geometric accuracy is minimal during the early humping stage (i.e., elongation mode).
As the severity of humping intensifies, the process transitions from the elongation mode to the swelling mode. A significant volume of liquid accumulates at the MP’s tail (
Figure 1d.1) and solidifies locally, leading to crest formation at the tail (
Figure 1d.2). When the elongation is excessive, the detachment mode is activated. The MP tail is detached and forms an isolated liquid volume (
Figure 1e.2), further contributing to crest formation (
Figure 1e.3).
During swelling mode, the continuous formation of these crests deteriorates the printed part’s geometrical accuracy rendering it wavy (
Figure 1f.1). When the surface is wavy, late humping symptoms (i.e., tilting mode) are observable. The MP follows a distorted path (i.e., wavy trajectory); thus, it starts to tilt; see the change in the MP orientation indicated by the blue line in
Figure 1f.2 to
Figure 1f.4.
The current literature offers various contradictory mechanisms that trigger the elongation and swelling mode. Some hypothesize a relation between powder density gradients in the gas-powder jet and humping creation. They assume that the powder gradient can cause protrusion growth [
9]. Such protrusions are similar to the swelling in
Figure 1d.1 and thus can also lead to the formation of the humping wavy surface in
Figure 1. (a). However, humping is not exclusive to powder-based AM processes but is also common in non-power-based processes such as welding [
10,
11,
12]. In welding literature, humping is often related to factors such as strong forward flow momentum and limited backfilling. The process conditions that trigger these factors are still unclear. In keyhole printing, with high energy intensity and deep depression in the laser-material interaction zones, some hypothesize that the lateral oscillation of the keyhole triggers humping [
13,
14]. However, humping is not exclusive to the high-energy-intensity keyhole printing mode but is also observed for conduction-mode welding with lower energy intensity and shallow melt pools. Gullipalli et al., 2023 have even recently shown that reducing heat input in DED (i.e., moving from keyhole to conduction mode printing conditions) can aid in activating humping [
15]. These contradictory recommendations and explanations arise from the complex non-linear interaction of physics in metal welding and printing. Thus, generalizations of these explanations or guidelines will always be doubtful, reducing the reliability of offline energy input optimization and emphasizing the need for real-time printing monitoring systems.
Instead of energy input optimization, the industry adopts energy management optimization. Energy management can be done by active cooling [
16,
17], or interlayer dwelling, with the latter being the more common strategy. Interlayer dwells pause the printing for a predetermined dwell time (DT) after a predetermined continuous deposition time (CDT), allowing the part to cool down and reach a predetermined temperature before resuming printing [
18,
19]. If achieved, optimal energy management is capable of keeping the melt pool in its normal state (
Figure 1b), effectively preventing humping. However, predetermining DT and CDT is a considerable optimization problem. For example, it has been shown that the optimal CDT varies depending on the printed part geometry and the current build height [
20]. Frequent stopping or unnecessarily prolonged dwell reduces productivity and subjects the part to unnecessary thermal cycles, potentially degrading quality [
21,
22]. Conversely, excessive delays in stopping (i.e., too long CDT) may lead to irreversible geometric inaccuracies, rendering the part as scrap unless hybrid additive-subtractive manufacturing techniques are available. Therefore, identifying the optimal stopping time that maximizes the CDT is crucial, highlighting the need for advanced real-time monitoring technologies.
While there are numerous studies dedicated to online monitoring solutions for detecting humping onset in additive manufacturing, the majority are reactive rather than proactive. This is because they have focused on humping late spatial symptoms rather than early spatiotemporal dynamics [
23,
24,
25]. For instance, [
24] detects humping when the melt pool is spatially detached into two separate liquid volumes (i.e., the detachment mode illustrated in
Figure 1e.2). At this stage, geometric inaccuracies caused by humping have already manifested and may lead to part scraping. Therefore, proactive monitoring of humping is crucial to provide enough time to take action to prevent irreversible geometric defects.
The principle contribution of this study is detecting the early elongation mode of humping. In contrast to the detachment mode, the elongation detection necessitates the simultaneous consideration of spatial and temporal (i.e., spatiotemporal) dynamics. In other words, in contrast to monitoring the swelling state illustrated in
Figure 1e.2, This work aims at simultaneously investigating the spatiotemporal dynamic of elongation mode to detect humping (i.e., the variation between
Figure 1c.1 and c.2). The distinct elongation and swelling modes physics is at the core of the proposed approach novelty, allowing it to:
Transform from reactive to proactive humping detection.
Transform humping detection from spatial (i.e., detachment) to spatiotemporal (i.e., elongation) abnormalities.
Practically track the variability in solidification front dynamics.
The structure of this study is organized as follows:
Section 2 describes the experimental setup and test matrix utilized for collecting the infrared videos.
Section 3 focuses on interpreting and processing the data to calculate the proposed humping indicator (VIMPS).
Section 4 empirically confirms the superiority of VIMPS compared to current state-of-the-art approaches.
2. Experimental Setup
Experiments were done on a 3kW TRUMPF TruDiode laser integrated with a six-axis CNC gantry. This system incorporated Reis Lasertec optics, an ILT powder nozzle, and a Sulzer-Metco TWIN-10 feeder. A 125 mm collimation lens, a 150 mm focal lens, a 600
µm fiber, a laser of wavelength of 950 nm, and a spot size of
D = 2.6 mm were used.
Figure 2 shows the laser profile used. In this study, austenitic nickel-chromium stainless steel powder was used; it has a nominal particle size distribution between -45 and +11 µm and a chemical composition of Fe 17Cr 12Ni 2.5Mo 2.3Si 0.03C. Circular builds of 25 mm in both height and diameter were constructed under varied printing conditions, as detailed in
Table 1. Three parts were printed using combinations of two laser powers
P, and two traverse speeds
v. All prints were made with an 8 g/min powder flow rate.
For melt pool monitoring, a med-wave infrared MWIR camera (i.e., FLIR SC8300) is used. The MWIR option was selected to ensure the capture of low-temperature regions, such as the melt pool tail, which cannot be captured by a normal
VIS camera (i.e., a camera only sensitive to visible light). This is because visible light is mainly emitted by objects at extremely high temperatures [
26]. The camera was equipped with a 50 mm focal lens with a 1-inch extension tube to achieve the desired field of view (FOV) of 5 mm x 3.5 mm. The camera was operated at a frame rate of 233 Hz and a resolution of 256 x 180 pixels. These settings were selected so that the sampling frequency was adequate to capture the humping dynamics. To allow for continuous monitoring and to negate any relative movement between the melt pool and the camera, the camera was directly mounted on the laser head, as shown in
Figure 3b. The table was rotated while the head moved in the positive Z direction, as shown in
Figure 3. The combined head and table motion leads to a continuous helical printing path. After printing, the as-printed parts are imaged using a ZEISS Smartzoom 5 automated digital microscope to assess the geometrical accuracy qualitatively (i.e., topography).
Figure 1.
(a) real image of severe humping redrawn from [
8] showing the crests and valleys forming the wavy structure. Each column (i.e., from b to f) shows different melt pool modes with humping’s severity increasing from b to f. Within each column, time progresses from top to bottom.
Figure 1.
(a) real image of severe humping redrawn from [
8] showing the crests and valleys forming the wavy structure. Each column (i.e., from b to f) shows different melt pool modes with humping’s severity increasing from b to f. Within each column, time progresses from top to bottom.
Figure 2.
Laser profile used.
Figure 2.
Laser profile used.
Figure 3.
(a) Schematic (b) actual view of the experimental setup.
Figure 3.
(a) Schematic (b) actual view of the experimental setup.
Figure 4.
The melt pool and the approximate contour of the heat-affected zone (HAZ).
Figure 4.
The melt pool and the approximate contour of the heat-affected zone (HAZ).
Figure 5.
The progression of melt pool solidification after the laser was turned off. Note t = 303.75 sec corresponds to the moment at which the laser was turned off.
Figure 5.
The progression of melt pool solidification after the laser was turned off. Note t = 303.75 sec corresponds to the moment at which the laser was turned off.
Figure 6.
(d) API variations during the accumulation (a→b) and solidification (b→c) through one elongation mode cycle.
Figure 6.
(d) API variations during the accumulation (a→b) and solidification (b→c) through one elongation mode cycle.
Figure 7.
As printed parts, (a & d) Test-1. (b & e) Test-2, and (c & f) Test-3. (d, e & f top-view with an elevation map (i.e., topography). Yellow regions are higher than blue regions by 1 mm, as shown in the scale in (f). Note that the variations in (e) and (f) are mainly due to the helical printing path, while in (d), the variations are dominated by the humping-induced crests.
Figure 7.
As printed parts, (a & d) Test-1. (b & e) Test-2, and (c & f) Test-3. (d, e & f top-view with an elevation map (i.e., topography). Yellow regions are higher than blue regions by 1 mm, as shown in the scale in (f). Note that the variations in (e) and (f) are mainly due to the helical printing path, while in (d), the variations are dominated by the humping-induced crests.
Figure 8.
The VIMPS variation over for different prints.
Figure 8.
The VIMPS variation over for different prints.
Figure 9.
(a) VIMPS overlayed over the as-printed part surface topography, (b) Side view of the as-printed part highlighting the scanned whose surface topography is shown in subfigure (a) in the same Figure.
Figure 9.
(a) VIMPS overlayed over the as-printed part surface topography, (b) Side view of the as-printed part highlighting the scanned whose surface topography is shown in subfigure (a) in the same Figure.
Figure 10.
Manually annotated melt pool at the detachment mode. (a-b) From Test #1 and (c-d) from Test #3. (a,c) show the first instances of the detachment mode in the corresponding test, and (b,d) shows the second instance.
Figure 10.
Manually annotated melt pool at the detachment mode. (a-b) From Test #1 and (c-d) from Test #3. (a,c) show the first instances of the detachment mode in the corresponding test, and (b,d) shows the second instance.
Figure 11.
(a) API during tilting in Test#1 (i.e., layer-32 to layer-44) and (b) the FFT analysis of the API- APIRM.
Figure 11.
(a) API during tilting in Test#1 (i.e., layer-32 to layer-44) and (b) the FFT analysis of the API- APIRM.
Figure 12.
micro-protrusion during Test #2.
Figure 12.
micro-protrusion during Test #2.
Figure 13.
(a) Early (b) late infrared images from test#1 and (c) late test#2. The accumulation step begins in (x.1) and ends in (x.2), and the solidification step starts in (x.2) and ends in (x.3). Subplots x.4 show the pixel intensity increase during the solidification (i.e., the pixel-wise difference between (x.3) and (x.2). Subplots x.5 show the API and VIMPS variation during the elongation cycle.
Figure 13.
(a) Early (b) late infrared images from test#1 and (c) late test#2. The accumulation step begins in (x.1) and ends in (x.2), and the solidification step starts in (x.2) and ends in (x.3). Subplots x.4 show the pixel intensity increase during the solidification (i.e., the pixel-wise difference between (x.3) and (x.2). Subplots x.5 show the API and VIMPS variation during the elongation cycle.
Table 1.
Experimental test matrix.
Table 1.
Experimental test matrix.
Test No. |
P (W) |
V (mm/min) |
1 |
650 |
600 |
2 |
650 |
360 |
3 |
850 |
360 |
Table 2.
Variation of different physical quantities during the elongation mode.
Table 2.
Variation of different physical quantities during the elongation mode.
|
MP size |
SFD |
API |
Accumulation in Figure 1c.1. |
Increasing |
Negative |
Decreasing |
Solidification in Figure 1c.2. |
Decreasing |
Positive |
Increasing |
Table 3.
Pseudocode for Physics-Based Indicator methodology.
Table 3.
Pseudocode for Physics-Based Indicator methodology.
Line |
Pseudo Code |
1 |
Define Region of Interest (ROI) |
2 |
do: |
3 |
Calculate Average Pixel Intensity (API) as per Equation 1 |
4 |
Calculate API’s Rolling Mean (APIRM) as per Equation 2 |
5 |
Calculate API’s Rolling Variance (APIRV) as per Equation 3 |
6 |
Calculate APIRVxM as per Equation 4 |
7 |
Calculate (VIMPS) as per Equation 5 |
8 |
End For |
Table 4.
Comparative analysis of humping detection methods; all values are in seconds.
Table 4.
Comparative analysis of humping detection methods; all values are in seconds.
Metric |
VIMPS |
SOTA’s Theoretical Upper bound |
Test # |
1 |
3 |
1 |
3 |
Detection Time |
200 |
170 |
219 |
200 |
T*Geo Time |
210 |
180 |
210 |
180 |
Detection Lead |
10 |
10 |
-9 |
-20 |
Consistency |
High |
Low |
Complexity |
Low |
High |
Principle |
Spatiotemporal |
Spatial |
Mode |
Elongation |
Detachment |