Laser Directed Energy Deposition of an AlMgScZr-Alloy in High-Speed Process Regimes

Aluminum-magnesium-scandium-zirconium (AlMgScZr) alloys need to be rapidly cooled from the liquid state to obtain a high degree of solute supersaturation that helps to exploit the precipitation hardening potential of the material. While AlMgScZr alloys have been successfully used in laser powder bed fusion (LPBF) processes, there has been little research in the field of laser directed energy deposition (DED) of the material. The limited previous studies have shown that the performance of AlMgScZr parts fabricated with DED only reached about 60% of that of the parts fabricated with LPBF. In view of breaking through the limitation associated with the process conditions of conventional DED, this work demonstrates the DED of AlMgScZr alloys in high-speed process regimes and elucidates the mechanism of enhancing the hardness and tensile strength of AlMgScZr alloys by increasing the cooling rate by one to two orders of magnitudes, as well as reducing the track overlapping and the porosity of the specimens during the process. A maximum average hardness of nearly 150 HV0.1 and a max. tensile strength of 407 MPa are obtained by using an energy per unit length of 5400 J/m and a powder feed rate per unit length of 0.25 g/m.


Introduction
5xxx series aluminum alloys (AlMg(Mn)) are lightweight structural materials with an excellent corrosion resistance and weldability. The strength of 5xxx series Al alloys increases with the increase of magnesium (Mg) and manganese (Mn) content; complemented by work hardening, for example, tensile strengths of nearly 400 MPa can be obtained in 5083 (AlMg4.5Mn0.7) Al alloy [1]. Another way to strengthen 5xxx series Al alloys is to supersaturate the material by adding hardly soluble transition elements (TE), such as scandium (Sc), zirconium (Zr), titanium (Ti) etc., allowing the precipitation of fine Al 3 TE dispersoids in solid solution during post-process ageing [2]. Sc is a proven modifier for Al alloys due to its well-studied ability to produce dispersive distributed, L1 2 -structured, and thermal stable Al 3 Sc precipitates that are almost perfectly coherent with the Al matrix [3]. Those secondary Al 3 Sc precipitates which are obtained from the solid Al matrix by ageing and are nano-scale can effectively induce precipitation strengthening and improve the resistance to recrystallisation of the material [4]. When the Sc solute content is greater than that of the eutectic composition (about 0.60 wt% [5] or 0.52 wt% [6]), primary Al 3 Sc precipitates will grow in solidifying liquid and function as heterogenous nuclei which can efficiently refine the microstructure [7]. The nucleation rate of both the primary [8] and secondary precipitates [9] can be further enhanced by supplementing Zr to the alloy. Zr is cheaper and can substitute up to 50% of Sc by forming Al 3 (Sc,Zr) without altering the L1 2 -structure of the phase [10]. The Al 3 (Sc,Zr) phase is thermally more stable than Al 3 Sc from approx. 10 K/s to 10 K/s depending on the selected parameters and the material to be processed [36][37][38]. Comparative studies of the two processes of AlMgScZr alloys have shown that the strength obtained in DED is only about 60% of that in LPBF [39]. Critical cooling rates for suppressing the nucleation of primary precipitates of an Al-3.3Mg-0.68Mn-xSc-yZr alloy are roughly estimated at 110 K/s for a low (0.25Sc-0.12Zr) and at 3 × 10 4 K/s for a high (0.50Sc-0.21Zr) Sc/Zr content. Since 3 × 10 4 K/s is already near the aforementioned upper limit, a hardness of only 105 HV0.2 (after 4 h ageing at 325 °C) with a very weak ageing response (about 10 HV0.2) is obtained in DED under normal process settings even with the high Sc/Zr content [40]. The 3D-parts in DED are built up by stacking of layers which are formed by a lateral overlap of deposition tracks. Preliminary studies on ageing response of DED tracks of AlMgScZr alloys show a nonuniform hardness distribution with soft fringes and hard cores on track cross-sections [41]. The layer stacking and track overlapping results in the harder core of previous tracks being covered by the softer fringe of following tracks, leading to a low overall hardness level at high overlap rates [42].
In view of breaking through the limitation associated with the cooling condition of DED, it is considered necessary to expand the scope of research by increasing the travel speed from the conventional (about 1 m/min) to high-speed (about 20 m/min or more) regime. While enhancing the strengthening potential of individual tracks in this way, more harder track cores need to be preserved to improve the multi-layer performance overall. DED parts have been successfully built with scan speeds up to 40 m/min, but defects like high porosity still point to room for improvement [43]. By addressing these issues in the experiment, this work studies, in more detail, methods to improve the reachable hardness and strength of AlMgScZr alloys in DED, as shown in the approach in Figure 1.

Powder
A commercially available gas-atomized AlMgScZr alloy powder with the composition of Al-4.55Mg-0.65Sc-0.30Zr (wt%) was used in the experiments. A SEM (scanning electron microscopy) (LEO 1455 EP of Carl Zeiss AG, Oberkochen, Germany) image of the powder is shown in Figure 2a. The particle size fraction of the powder with D10% = 23.27 µm, D50% = 38.28 µm, D90% = 57.42 µm is shown in Figure 2b. The chemical composition of the powder according to the data sheet offered by the supplier is shown in Figure 2c. The content of Al and of the main alloy element Mg, Sc, and Zr checked by ICP-OES (SPECTROBLUE of SPECTRO Analytical Instruments GmbH, Kleve, Germany) (inductively coupled plasma optical emission spectroscopy) of a small amount sampled

Powder
A commercially available gas-atomized AlMgScZr alloy powder with the composition of Al-4.55Mg-0.65Sc-0.30Zr (wt%) was used in the experiments. A SEM (scanning electron microscopy) (LEO 1455 EP of Carl Zeiss AG, Oberkochen, Germany) image of the powder is shown in Figure 2a. The particle size fraction of the powder with D 10% = 23.27 µm, D 50% = 38.28 µm, D 90% = 57.42 µm is shown in Figure 2b. The chemical composition of the powder according to the data sheet offered by the supplier is shown in Figure 2c. The content of Al and of the main alloy element Mg, Sc, and Zr checked by ICP-OES (SPECTROBLUE of SPECTRO Analytical Instruments GmbH, Kleve, Germany) (inductively coupled plasma optical emission spectroscopy) of a small amount sampled from the powder are shown in Figure 2d. The composition data are consistent with each other.

Experimental Setup
Two types of specimens, namely single tracks and hollow-cylindrical shap parts were produced. The single tracks were fabricated in large quantities to iden influence of variation of main process parameters (laser power P, travel speed v, p feed rate ṁ) across conventional and high-speed process regimes on the ratio of m deposition to melt pool dilution by measuring the geometry of the cross-section tracks (more details see Section 2.5). Representative parameters were selected an used to build 3D-parts.
For fabricating single tracks, 5083 alloy tubes were used as substrates (250 mm 33.4 mm outer diameter, 3.38 mm wall thickness, at room temperature) that were c on a chuck and rotated with the spindle, as shown in Figure 3a (above). The nozzle moved in the direction parallel to the spindle axis and with 10 mm (i.e., distance) stand-off distance to the substrate surface. Powder particles were conve Ar (i.e., conveying gas) in a conical beam to the substrate surface and melted by a co aligned laser beam, along which there was an additional Ar flow (i.e., shielding enhancing the shielding performance. Materials were deposited in a melt pool with the travel speed relative to the substrate. Maximum 15 helical tracks co fabricated on one tube-shaped substrate. The tracks were spaced to prevent thermal influences, as shown in Figure 3a (below). For fabricating the 3D-parts time, a piece of substrate (5083 Al alloy, 12 mm thickness) was fixed in the cente end face of a cylindrical aluminum block (5083 Al alloy, pre-cooled by ice water Ø 200 mm, 200 mm height) which rotated along an axis parallel to the powder nozz as shown in Figure 3b. The powder nozzle translated in the radial direction diameter = 28 mm, outer diameter = 44 mm) of the rotation back and forth. The la on while the nozzle was moving from the inner to the outer radius. The rotation was automatically adjusted to the radial position of the nozzle to ensure a constan speed (i.e., the travel speed) between the nozzle and the substrate surface. As a spiral tracks that build layers were formed. The distance between the nozzle tip growing specimen was adjusted after each layer was formed. For material a (Section 2.5) on cross-sections, small pieces of samples were cut from the specim

Experimental Setup
Two types of specimens, namely single tracks and hollow-cylindrical shaped 3Dparts were produced. The single tracks were fabricated in large quantities to identify the influence of variation of main process parameters (laser power P, travel speed v, powder feed rateṁ) across conventional and high-speed process regimes on the ratio of material deposition to melt pool dilution by measuring the geometry of the cross-sections of the tracks (more details see Section 2.5). Representative parameters were selected and then used to build 3D-parts.
For fabricating single tracks, 5083 alloy tubes were used as substrates (250 mm length, 33.4 mm outer diameter, 3.38 mm wall thickness, at room temperature) that were clamped on a chuck and rotated with the spindle, as shown in Figure 3a (above). The powder nozzle moved in the direction parallel to the spindle axis and with 10 mm (i.e., nozzle distance) stand-off distance to the substrate surface. Powder particles were conveyed by Ar (i.e., conveying gas) in a conical beam to the substrate surface and melted by a coaxially aligned laser beam, along which there was an additional Ar flow (i.e., shielding gas) for enhancing the shielding performance. Materials were deposited in a melt pool moving with the travel speed relative to the substrate. Maximum 15 helical tracks could be fabricated on one tubeshaped substrate. The tracks were spaced to prevent mutual thermal influences, as shown in Figure 3a (below). For fabricating the 3D-parts, every time, a piece of substrate (5083 Al alloy, 12 mm thickness) was fixed in the center of the end face of a cylindrical aluminum block (5083 Al alloy, pre-cooled by ice water to 0 • C, Ø 200 mm, 200 mm height) which rotated along an axis parallel to the powder nozzle axis, as shown in Figure 3b. The powder nozzle translated in the radial direction (inner diameter = 28 mm, outer diameter = 44 mm) of the rotation back and forth. The laser was on while the nozzle was moving from the inner to the outer radius. The rotation speed was automatically adjusted to the radial position of the nozzle to ensure a constant linear speed (i.e., the travel speed) between the nozzle and the substrate surface. As a result, spiral tracks that build layers were formed. The distance between the nozzle tip and the growing specimen was adjusted after each layer was formed. For material analysis (Section 2.5) on cross-sections, small pieces of samples were cut from the specimens, as shown in Figure 3c  The experiment was carried out in an EHLA (acronym of extreme high-speed laser metal deposition) system, which integrated a lathe-like CNC machine (max. spindle speed 775 rpm, Hornet Laser Cladding BV) with the laser cladding optics (laser spot Ø 1.3 mm, BEO D70, Trumpf GmbH + Co. KG) and powder-feeding assembly (Nozzle of Fraunhofer.ILT, Germany; powder feeder TWIN-150 of Oerlikon Mecto AG, Switzerland). High travel speed was achieved by combining the nozzle translation and the high-speed spindle rotation. The spindle axle is perpendicular or parallel to the nozzle axis, thus creating the single tracks or 3D-parts, respectively, as shown in Figure 4a-c. Since sufficient shielding gas flow is observed to improve the build quality of 3D-parts in DED [43], and considering that the nozzle's own shielding gas flow can be inadequate under open atmosphere when the travel speed is high, several shielding concepts were compared. For this, an additional shielding gas flow, a shielding sleeve, a smoke exhaust flue, an Al curtain, and a protective box were used, as shown in Figure 4d-i. It should be noted that because of the difficulty of sealing due to the spindle rotation, the process was done out of chamber, and none of the methods could guarantee an absolute inert atmosphere around the meld pool. Some examples of the specimens are shown in Figure  5. The experiment was carried out in an EHLA (acronym of extreme high-speed laser metal deposition) system, which integrated a lathe-like CNC machine (max. spindle speed 775 rpm, Hornet Laser Cladding BV) with the laser cladding optics (laser spot Ø 1.3 mm, BEO D70, Trumpf GmbH + Co. KG) and powder-feeding assembly (Nozzle of Fraunhofer.ILT, Germany; powder feeder TWIN-150 of Oerlikon Mecto AG, Switzerland). High travel speed was achieved by combining the nozzle translation and the high-speed spindle rotation. The spindle axle is perpendicular or parallel to the nozzle axis, thus creating the single tracks or 3D-parts, respectively, as shown in Figure 4a-c. Since sufficient shielding gas flow is observed to improve the build quality of 3D-parts in DED [43], and considering that the nozzle's own shielding gas flow can be inadequate under open atmosphere when the travel speed is high, several shielding concepts were compared. For this, an additional shielding gas flow, a shielding sleeve, a smoke exhaust flue, an Al curtain, and a protective box were used, as shown in Figure 4d-i. It should be noted that because of the difficulty of sealing due to the spindle rotation, the process was done out of chamber, and none of the methods could guarantee an absolute inert atmosphere around the meld pool. Some examples of the specimens are shown in Figure 5. Most of the 3D-parts like that shown in (c) were made with additional shielding concepts: (d) an additional shielding gas flow "Ad", (e) a shielding sleeve "Ri", (f) a smoke exhaust flue "Ex", (g) a combination of the sleeve and the flue "RE", (h) an Al curtain "Fo", and (i) a protective box "Bo". The designators in quotation marks are the short forms used in Table 1. "Bo" has a larger interior space and is thus more heat resistant than "Fo". The letters in quotation marks are specimen designations (see Table 1).

Figure 5.
Exterior views of specimens of (a) single tracks, (b) 3D-parts with about 5 mm height and used for hardness tests, and (c) 3D-parts with about 50 mm height and used for tensile tests. The black bars indicate a length of 50 mm.   Table 1. "Bo" has a larger interior space and is thus more heat resistant than "Fo". The letters in quotation marks are specimen designations (see Table 1).  Figure 4. Photos of the basic experimental setup for fabricating (a) single tracks and (b) 3D-parts "Or". Most of the 3D-parts like that shown in (c) were made with additional shielding concepts: (d) an additional shielding gas flow "Ad", (e) a shielding sleeve "Ri", (f) a smoke exhaust flue "Ex", (g) a combination of the sleeve and the flue "RE", (h) an Al curtain "Fo", and (i) a protective box "Bo". The designators in quotation marks are the short forms used in Table 1. "Bo" has a larger interior space and is thus more heat resistant than "Fo". The letters in quotation marks are specimen designations (see Table 1).

Process Variables
During the DED process, a millimeter-sized melt pool moves along the relative motion trajectory between the powder nozzle and the substrate. Under the simplifying assumptions that (a) the material physical properties are independent of temperature, (b) travel speed and heat input are constant, (c) a point heat source, (d) the heat flow around the heat source is in quasi-stationary state, (e) the substrate is thick and can be treated as semi-infinite, (f) no phase transition enthalpy, and (g) the surface heat losses can be ignored, the cooling rate [K/s] at the solidification front on the central line of the moving melt pool is given by Rosenthal's equation [44] as follows: where k is the material thermal conductivity [W/(m·K)], α is the absorption rate [1], v is the travel speed [m/s], P is the laser power [W], T l is the liquidus temperature [K], and T 0 is the initial temperature of the solid part [K]. For a given material, the cooling rate at the solidification front can be increased by decreasing T 0 or increasing v/P. The term is also known as E' or energy per unit length [J/m]. The cooling rate in different process regimes can be roughly estimated by inserting the values k = 120 W/(m·K) (at 20 • C) and T l = 875.15 K (638 • C) for the 5083 Al alloy [45], α = 0.24 for the 5251 Al alloy (AlMg2Mn0.3, surface roughness S a = 0.28 µm, at 20 • C, 1053 nm wavelength) [46], and the different T 0 , v, and P into Equation (1). For the investigated values of high-speed DED, e.g., T 0 = 273.15 K (0 • C), v = 0.33 m/s (20 m/min), and P = 1800 W, the cooling rate is estimated to 2.34 × 10 5 K/s, which is much higher than that in conventional DED with the values of, e.g., T 0 = 293.15 K (20 • C), v = 0.0083 m/s (0.5 m/min), and P = 600 W, with an estimated cooling rate of 1.67 × 10 4 K/s, or T 0 = 373.15 K (100 • C), v = 0.015 m/s (0.9 m/min), and P = 1800 W, with an estmated cooling rate of only 7.58 × 10 3 K/s. As a result of this estimation, the cooling rates in the high-speed process regime are one to two orders of magnitude higher than in conventional DED. It is important to note that the ideal parameter values for increasing the cooling rate must be able to guarantee the real material deposition. To figure out the feasible maximum of v/P and considering that the powder feed rateṁ should have influence on the track overlapping, process parameters for fabricating single tracks were selected in a large range of settings that covers P from 800 W to 4000 W, v from 5 m/min to 32 m/min,ṁ from 0.125 g/min to 8 g/min, as shown in Figure 6. Values of E' = P/v of some parameter sets are given in Figure 6a. Another value, powder feed rate per unit length [g/m], which is defined as m' =ṁ/v, will be used later in the Results Section. Representative values of the parameters were then selected for fabricating 3D-parts, as shown in Table 1. For the specimens Or1 and Ad1-Ad5, material deposition occurred when the nozzle moved in both directions between the inner and outer diameter of the specimen; for the other specimens, the laser was switched on, and thus the material deposition occurred only when the nozzle moved from the inner diameter to the outer diameter. parameters were then selected for fabricating 3D-parts, as shown in Table 1. For the specimens Or1 and Ad1-Ad5, material deposition occurred when the nozzle moved in both directions between the inner and outer diameter of the specimen; for the other specimens, the laser was switched on, and thus the material deposition occurred only when the nozzle moved from the inner diameter to the outer diameter.

Heat Treatment
An optimum ageing heat treatment should be addressed in AlMgScZr alloys to control the precipitation hardening to acquire the desired high-performance mechanical properties. Ageing at low temperatures of about 300 °C is suggested to allow the formation of coherent and homogeneously distributed Al3Sc precipitates in Al-0.2Sc (wt%) alloy [14]. Casted Al-0.41Sc (wt%) alloy is found to be peak-age hardened by heating the material at temperatures between 300 °C and 350 °C for about 3 h [47]. As for AlMgSc(Zr) alloys, results of previous studies on optimum heat treatment strategies leading to the highest tensile strength or hardness are shown in Table 2. To study the process-related ageing response (i.e., the precipitation hardening potential), specimens in this work were sampled, as shown in Figure 3d, and aged at 300 °C, 325 °C, or 350 °C for 3, 4, 5, 7, or 9 h and then air-cooled for comparison. Considering the result and for ease of comparison with previous studies, "4 h at 325 °C + air cooling" was then selected and used to treat the specimens to study the influence of other factors like porosity and layer overlap ratio on the hardness.

Heat Treatment
An optimum ageing heat treatment should be addressed in AlMgScZr alloys to control the precipitation hardening to acquire the desired high-performance mechanical properties. Ageing at low temperatures of about 300 • C is suggested to allow the formation of coherent and homogeneously distributed Al 3 Sc precipitates in Al-0.2Sc (wt%) alloy [14]. Casted Al-0.41Sc (wt%) alloy is found to be peak-age hardened by heating the material at temperatures between 300 • C and 350 • C for about 3 h [47]. As for AlMgSc(Zr) alloys, results of previous studies on optimum heat treatment strategies leading to the highest tensile strength or hardness are shown in Table 2. To study the process-related ageing response (i.e., the precipitation hardening potential), specimens in this work were sampled, as shown in Figure 3d, and aged at 300 • C, 325 • C, or 350 • C for 3, 4, 5, 7, or 9 h and then air-cooled for comparison. Considering the result and for ease of comparison with previous studies, "4 h at 325 • C + air cooling" was then selected and used to treat the specimens to study the influence of other factors like porosity and layer overlap ratio on the hardness.  Supersaturated Mg in Al alloys can precipitate forming the phase transforming from Guinier-Preston zones, to β" phase, then to β' phase and finally to β phase [50]. The β' (Al 3 Mg 2 ) phase is semi-coherent and found to be the main hardening phase. The formation of β' phase starts, according to the study on Al-8Mg and Al-12Mg (wt%) alloy, already at 100 • C and can be accelerated (i.e., tens of hours) at 150 • C [51]. Since Mg in Al-4.55Mg (wt%) (Al-5Mg at%) alloy will dissolve into the matrix at above 235 • C [52], which is much lower than the 325 • C ageing temperature (for Sc/Zr precipitation), Mg cannot be fully utilized by a single one-stage ageing. Therefore, double-stage ageing strategies were also attempted. Specimens were firstly aged at 325 • C for 4 h, then water-cooled, and finally aged at 150 • C for 1-4 h, or at 70 • C for 2-30 h.

Material Analysis
Specimens of single tracks and 3D-parts were cut as shown in Figure 3c,d, allowing the analysis on track cross-sections. The specimens were cold embedded. The cross-sections were wet ground until using 1200 grid SiC sandpaper and then polished (18 N for 20 min) with 1 µm diamond suspension. The polished cross-sections of the single tracks were additionally etched with a sodium hydroxide solution (NaOH, 10%). The microstructural details were thus visible on the microscope and dimensions like track width w, track height h, melt pool depth d, and the cross-sectional area of the deposition zone A DE (i.e., the melting part above the substrate surface) and of the dilution zone A DI (i.e., the melting part below the substrate surface), as shown in Figure 7a. Some samples cut from the 3D-parts were also etched so that the thickness of the layers formed by overlapped tracks could be measured, as shown in Figure 7b. H2 represents the remaining visible height of the second last layer when it is partially remelted by the last layer. H3 represents the remaining visible height of the third last layer when it is partially remelted by the second last layer. The overlap between the last and the second last layer is thus 1 − (H2/H1), and the overlap between the second last and the third last layer is 1 − (H3/H1) (assuming a constant layer height of H1). The average of the two values is defined in this work as the layer overlap ratio O L . With the help of contrast difference due to illumination, cross-sectional porosities P C were measured, as shown in Figure 7c. The porosity was defined as the ratio between the sum of the dark pore areas to the total cross-sectional area of the specimen. Microhardness measurements were carried out according to Vickers with the test load of 100 g (HV0.1). One measurement consisted of 20-30 indentations with a point spacing of approx. 0.2 mm centrally along the specimen. The indentation positions were created as one line and then slightly shifted to the dense zone when the points encountered pores, as shown in Figure 7d (right). A pico/nanoindenter was used to draw hardness mapping diagrams of the last several layers of some specimens. Each measurement was performed in a 36 × 41 (700 µm × 800 µm) matrix with a total of 1476 indentations, as shown in Figure 7d  cross-sectional porosities PC were measured, as shown in Figure 7c. The porosity was defined as the ratio between the sum of the dark pore areas to the total cross-sectional area of the specimen. Microhardness measurements were carried out according to Vickers with the test load of 100 g (HV0.1). One measurement consisted of 20-30 indentations with a point spacing of approx. 0.2 mm centrally along the specimen. The indentation positions were created as one line and then slightly shifted to the dense zone when the points encountered pores, as shown in Figure 7d (right). A pico/nanoindenter was used to draw hardness mapping diagrams of the last several layers of some specimens. Each measurement was performed in a 36 × 41 (700 µm × 800 µm) matrix with a total of 1476 indentations, as shown in Figure 7d

Dilution Zone of Single Tracks
Results of the dimension measurements (i.e., h, d, w, ADE, and ADI, according to Figure  7a) of the single tracks fabricated with different sets of P, v, and ṁ (according to Figure 6) are plotted against E', as shown in Figure 8 (plot directly against P is shown in in Appendix A). It is apparent from the diagrams that h and ADE, which refer to the size of the deposition zones, are not much influenced by E', but slightly increase with m', as shown in Figure 8a,d. When E' increases, w exhibits only a weak tendency to increase, as shown in Figure 8c. Significant proportional are d and E', as well as ADI and E', as shown in Figure 8b,e. This indicates that the increase in ADI (since ADI~d × w) caused by the increase in E' is more related to the increase in d. In the low values E' region and thus low energy input, as marked by the dashed box in Figure 8a,d, h and ADE decrease faster, implying a reduction in material catch rate. Although a lower E' value (thus a higher v/P) leading to higher cooling rates is desired, the minimum threshold of E' to ensure the material deposition at current process settings in single tracks is about 5500 J/m (corresponding to d ≈ 300 µm, ADI ≈ 3.26 × 10 5 µm 2 ).

Dilution Zone of Single Tracks
Results of the dimension measurements (i.e., h, d, w, A DE , and A DI , according to Figure 7a) of the single tracks fabricated with different sets of P, v, andṁ (according to Figure 6) are plotted against E', as shown in Figure 8 (plot directly against P is shown in in Appendix A). It is apparent from the diagrams that h and A DE , which refer to the size of the deposition zones, are not much influenced by E', but slightly increase with m', as shown in Figure 8a,d. When E' increases, w exhibits only a weak tendency to increase, as shown in Figure 8c. Significant proportional are d and E', as well as A DI and E', as shown in Figure 8b,e. This indicates that the increase in A DI (since A DI~d × w) caused by the increase in E' is more related to the increase in d. In the low values E' region and thus low energy input, as marked by the dashed box in Figure 8a,d, h and A DE decrease faster, implying a reduction in material catch rate. Although a lower E' value (thus a higher v/P) leading to higher cooling rates is desired, the minimum threshold of E' to ensure the material deposition at current process settings in single tracks is about 5500 J/m (corresponding to d ≈ 300 µm, A DI ≈ 3.26 × 10 5 µm 2 ). Important indices that control the overlapping of adjacent tracks within a layer or between layers are the ratio of h/d and of ADE/ADI. A higher ratio of h/d or of ADE/ADI indicate that less of the deposited material (i.e., that of last track or layer) will be remelted relative to the material being deposited. The two indices increase as E' decreases until it reaches the threshold of about 6000 J/m. They can be increased to about 40% or 32%, respectively, by the increase in m' (here, to 0.30 g/m), as shown in Figure 9a,b. The sum of ADE and ADI decreases as E' decreases, as shown in Figure 9c, which means that the total heat input is reduced.

Deposition Zone of Single Tracks
The influence of powder feed rate and travel speed on the dimensions (i.e., h, d, w, ADE, and ADI, according to Figure 7a) of single tracks (fabricated according to Figure 6b) are more clearly seen by plotting the data against m', as shown in Figure 10. The influence of m' and E' on d, ADI and w, as shown in Figure 8, is also depicted in Figure 10b,c,e. h and ADE strongly increase as a function of m', whereas E' has only a minor influence, as shown Important indices that control the overlapping of adjacent tracks within a layer or between layers are the ratio of h/d and of A DE /A DI . A higher ratio of h/d or of A DE /A DI indicate that less of the deposited material (i.e., that of last track or layer) will be remelted relative to the material being deposited. The two indices increase as E' decreases until it reaches the threshold of about 6000 J/m. They can be increased to about 40% or 32%, respectively, by the increase in m' (here, to 0.30 g/m), as shown in Figure 9a,b. The sum of A DE and A DI decreases as E' decreases, as shown in Figure 9c, which means that the total heat input is reduced. Important indices that control the overlapping of adjacent tracks within a layer or between layers are the ratio of h/d and of ADE/ADI. A higher ratio of h/d or of ADE/ADI indicate that less of the deposited material (i.e., that of last track or layer) will be remelted relative to the material being deposited. The two indices increase as E' decreases until it reaches the threshold of about 6000 J/m. They can be increased to about 40% or 32%, respectively, by the increase in m' (here, to 0.30 g/m), as shown in Figure 9a,b. The sum of ADE and ADI decreases as E' decreases, as shown in Figure 9c, which means that the total heat input is reduced.

Deposition Zone of Single Tracks
The influence of powder feed rate and travel speed on the dimensions (i.e., h, d, w, ADE, and ADI, according to Figure 7a) of single tracks (fabricated according to Figure 6b) are more clearly seen by plotting the data against m', as shown in Figure 10. The influence of m' and E' on d, ADI and w, as shown in Figure 8, is also depicted in Figure 10b,c,e. h and ADE strongly increase as a function of m', whereas E' has only a minor influence, as shown

Deposition Zone of Single Tracks
The influence of powder feed rate and travel speed on the dimensions (i.e., h, d, w, A DE , and A DI , according to Figure 7a) of single tracks (fabricated according to Figure 6b) are more clearly seen by plotting the data against m', as shown in Figure 10. The influence of m' and E' on d, A DI and w, as shown in Figure 8, is also depicted in Figure 10b,c,e. h and A DE strongly increase as a function of m', whereas E' has only a minor influence, as shown in Figure 10a,d. This indicates that the deposition zone becomes slender (since A DE~w × h) as m' increases. At a value of E' of 7500 J/m (i.e., the lowest in the diagrams), both h and A DE reach a plateau of about 80 µm and 8 × 10 4 µm 2 , respectively, as m' increases between 0.25 g/min and 0.35 g/min. This plateau indicates that while decreasing E' to obtain high cooling rates and small dilution zones, increasing m' to obtain large deposition zones is limited by an insufficient melting of powder. The plateau can also be seen in the diagram of the ratio of h/d and of A DE /A DI , as shown in Figure 11a,b. Although the trend of the sum of A DE + A DI as a function of m' is nearly horizontal, as shown in Figure 11c, d or A DI cannot be arbitrarily increased just by increasing m'. in Figure 10a,d. This indicates that the deposition zone becomes slender (since ADE ~ w × h) as m' increases. At a value of E' of 7500 J/m (i.e., the lowest in the diagrams), both h and ADE reach a plateau of about 80 µm and 8 × 10 4 µm 2 , respectively, as m' increases between 0.25 g/min and 0.35 g/min. This plateau indicates that while decreasing E' to obtain high cooling rates and small dilution zones, increasing m' to obtain large deposition zones is limited by an insufficient melting of powder. The plateau can also be seen in the diagram of the ratio of h/d and of ADE/ADI, as shown in Figure 11a,b. Although the trend of the sum of ADE + ADI as a function of m' is nearly horizontal, as shown in Figure 11c, d or ADI cannot be arbitrarily increased just by increasing m'.  A summary of the data of the influence of E' and m' on ADE/ADI and ADE + ADI is shown in Figure 12a,b. The influence can be represented schematically in the diagram shown in Figure 12c. As E' increases, more energy is transferred into the dilution part. With increasing m', higher tracks are realized, and more energy is absorbed by the deposition part. A low E' allows a high cooling rate and a high m' allows a high deposition rate. However, ideal tracks that enable high-rate deposition having little heat effect on previous layers and are cooled quickly (i.e., type c4) are difficult to fabricate due to limitations like in Figure 10a,d. This indicates that the deposition zone becomes slender (since ADE ~ w × h) as m' increases. At a value of E' of 7500 J/m (i.e., the lowest in the diagrams), both h and ADE reach a plateau of about 80 µm and 8 × 10 4 µm 2 , respectively, as m' increases between 0.25 g/min and 0.35 g/min. This plateau indicates that while decreasing E' to obtain high cooling rates and small dilution zones, increasing m' to obtain large deposition zones is limited by an insufficient melting of powder. The plateau can also be seen in the diagram of the ratio of h/d and of ADE/ADI, as shown in Figure 11a,b. Although the trend of the sum of ADE + ADI as a function of m' is nearly horizontal, as shown in Figure 11c, d or ADI cannot be arbitrarily increased just by increasing m'.  A summary of the data of the influence of E' and m' on ADE/ADI and ADE + ADI is shown in Figure 12a,b. The influence can be represented schematically in the diagram shown in Figure 12c. As E' increases, more energy is transferred into the dilution part. With increasing m', higher tracks are realized, and more energy is absorbed by the deposition part. A low E' allows a high cooling rate and a high m' allows a high deposition rate. However, ideal tracks that enable high-rate deposition having little heat effect on previous layers and are cooled quickly (i.e., type c4) are difficult to fabricate due to limitations like A summary of the data of the influence of E' and m' on A DE /A DI and A DE + A DI is shown in Figure 12a,b. The influence can be represented schematically in the diagram shown in Figure 12c. As E' increases, more energy is transferred into the dilution part. With increasing m', higher tracks are realized, and more energy is absorbed by the deposition part. A low E' allows a high cooling rate and a high m' allows a high deposition rate. However, ideal tracks that enable high-rate deposition having little heat effect on previous layers and are cooled quickly (i.e., type c4) are difficult to fabricate due to limitations like insufficient melting or possible defective binding. A feasible combination of a low E' (e.g., 6000 J/m) and a relative high m' (e.g., 0.25 g/m) can be found that leads to an A DE /A DI ratio of about 30% and a sum of A DE + A DI of about 4 × 10 5 µm 2 , as shown in Figure 12a,b. During the fabrication of 3D-parts, the conditions change dynamically as the substrate temperature rises or the heat dissipation conditions change. Nevertheless, a qualitative approach to choose proper parameter values is given by the diagrams, as well as the understanding of how the geometry of single tracks is influenced by the parameters. insufficient melting or possible defective binding. A feasible combination of a low E' (e.g., 6000 J/m) and a relative high m' (e.g., 0.25 g/m) can be found that leads to an ADE/ADI ratio of about 30% and a sum of ADE + ADI of about 4 × 10 5 µm 2 , as shown in Figure 12a,b. During the fabrication of 3D-parts, the conditions change dynamically as the substrate temperature rises or the heat dissipation conditions change. Nevertheless, a qualitative approach to choose proper parameter values is given by the diagrams, as well as the understanding of how the geometry of single tracks is influenced by the parameters.

Ageing of 3D-Parts
The values of parameter P and v have been chosen so that the E' (=P/v) is within the low value range according to Figure 12. The powder feed rate was set to ṁ = 5 g/min so that m' (0.20 g/m, 0.25 g/min) was in the zone with a relative high ADE/ADI and low ADE + ADI. The hardness profiles of five specimens fabricated under the same conditions by varying only the laser power P and travel speed v are shown in Figure 13. The profiles exhibit hardness data of the specimens in an as-built state and of the specimens that were aged at 300 °C, 325 °C, or 350 °C for 3 to 9 h. It is noticeable that Ad1, whose E' is the lowest (i.e., 5400 J/m), has the lowest hardness in the as-built state (102 HV0.1) but obviously the highest ageing response (max. 149 HV0.1, 47 HV0.1, 5 h at 325 °C), as shown in Figure 13a. The other specimens also have a relative high level of hardness (in comparison with that in Table 2), but the peak hardness (about 130 HV0.1) is lower and the ageing response (about 15 HV0.1) is weaker than that of Ad1, as shown in Figure  13b-e. One more thing learnt is that the hardness plateaus for all specimens were obtained after 4 h at the latest. A longer aging time up to 9 h could not produce a further increase in hardness.

Ageing of 3D-Parts
The values of parameter P and v have been chosen so that the E' (=P/v) is within the low value range according to Figure 12. The powder feed rate was set toṁ = 5 g/min so that m' (0.20 g/m, 0.25 g/min) was in the zone with a relative high A DE /A DI and low A DE + A DI . The hardness profiles of five specimens fabricated under the same conditions by varying only the laser power P and travel speed v are shown in Figure 13. The profiles exhibit hardness data of the specimens in an as-built state and of the specimens that were aged at 300 • C, 325 • C, or 350 • C for 3 to 9 h. It is noticeable that Ad1, whose E' is the lowest (i.e., 5400 J/m), has the lowest hardness in the as-built state (102 HV0.1) but obviously the highest ageing response (max. 149 HV0.1, ∆ 47 HV0.1, 5 h at 325 • C), as shown in Figure 13a. The other specimens also have a relative high level of hardness (in comparison with that in Table 2), but the peak hardness (about 130 HV0.1) is lower and the ageing response (about ∆15 HV0.1) is weaker than that of Ad1, as shown in Figure 13b-e. One more thing learnt is that the hardness plateaus for all specimens were obtained after 4 h at the latest. A longer aging time up to 9 h could not produce a further increase in hardness.

Cross-Sectional Porosity of 3D-Parts
Cross-sections of the specimens listed in Table 1 were sampled and prepared for comparing their cross-sectional porosity with each other, as shown in Figure 14a. Except for the specimens Ad1-Ad5, other specimens were uniformly fabricated with a travel speed v of 20 m/min and a lower level of laser power P (i.e., 1800 W-2500 W). Although overall porosity of each sample is still high (i.e., up to about 5%), the difference in the effect of shielding and exhausting measures on porosity can be seen. The active exhaust was used to prevent more soot from settling on the specimen surface being cladded. The porosities of the specimens (i.e., Ex1-5 and Re1) fabricated with the exhaust, however, are apparently higher, perhaps because the local shielding atmosphere was destroyed by the exhaust airflow. Specimens fabricated with the shielding sleeve (i.e., Ri1-2 and Ex1-5) have a more rounded cross-sectional profile in addition to a higher porosity, as shown in Figure 14b-e. Although the same cooling unit was used, the narrow shielding sleeve may have induced a stronger laser reflection onto the specimen and therefore caused these specimens to be overheated (thus lower cooling rates) in the process. Other shielding measures with more spacious conditions have been observed to allow the fabrication of samples (i.e., Ad4-5, Fo2 and Bo1-2) having significantly lower porosity (i.e., about 2%) than the reference specimen fabricated with the original setting (i.e., Or1). However, specimens with about 4-5% porosity were also observed, indicating that the shielding measures alone were still insufficient to ensure the fabrication of fully dense specimens (further discussion in Section 3.7.
Nevertheless, the benefits of reducing porosity for increasing hardness can be seen by plotting hardness versus porosity of the specimens, as shown in Figure 14f-g. Hardness indentations were placed so that each individual value was measured in an area that was dense in the cross section but might still be influenced by surrounding pores. Since each specimen was fabricated with different thermal conditions, a direct comparison between the as-built hardness is not necessarily meaningful. However, as mentioned in Section 3.3 hardness plateaus that eliminate the influence of the previous thermal history can be reached after 4 h ageing. In the aged specimens, an increase in hardness with a decrease in porosity can be clearly observed. The standard deviation of the hardness values measured on each specimen also varies with porosity with a roughly increasing

Cross-Sectional Porosity of 3D-Parts
Cross-sections of the specimens listed in Table 1 were sampled and prepared for comparing their cross-sectional porosity with each other, as shown in Figure 14a. Except for the specimens Ad1-Ad5, other specimens were uniformly fabricated with a travel speed v of 20 m/min and a lower level of laser power P (i.e., 1800 W-2500 W). Although overall porosity of each sample is still high (i.e., up to about 5%), the difference in the effect of shielding and exhausting measures on porosity can be seen. The active exhaust was used to prevent more soot from settling on the specimen surface being cladded. The porosities of the specimens (i.e., Ex1-5 and Re1) fabricated with the exhaust, however, are apparently higher, perhaps because the local shielding atmosphere was destroyed by the exhaust airflow. Specimens fabricated with the shielding sleeve (i.e., Ri1-2 and Ex1-5) have a more rounded cross-sectional profile in addition to a higher porosity, as shown in Figure 14b-e. Although the same cooling unit was used, the narrow shielding sleeve may have induced a stronger laser reflection onto the specimen and therefore caused these specimens to be overheated (thus lower cooling rates) in the process. Other shielding measures with more spacious conditions have been observed to allow the fabrication of samples (i.e., Ad4-5, Fo2 and Bo1-2) having significantly lower porosity (i.e., about 2%) than the reference specimen fabricated with the original setting (i.e., Or1). However, specimens with about 4-5% porosity were also observed, indicating that the shielding measures alone were still insufficient to ensure the fabrication of fully dense specimens (further discussion in Section 3.7.

Layer Overlap Ratio of 3D-Parts
Specimens which have relatively low porosities and were fabricated with a stepwise variation of the energy per unit length E' (=P/v) as well as the same travel speed and scan strategy were selected. Layer thickness was measured on etched specimen cross-sections to calculate the layer overlap ratio OL (defined in Figure 7b), as shown in Figure 15a-e. The relationships between E' and OL as well as the hardness (after ageing at 325 °C for 4 h) are shown in Figure 15f-h. The relationship between the calculated OL and the corresponding E' is shown in Figure 15f. A lower OL or E' correlates with a higher hardness level, as shown in Figure 15g-h, so that the average hardness value of Bo1 (147 HV0.1) is about 17 HV0.1 higher than that of Bo3. The deviation of the hardness values is consistent with that observed in Figure 14 regarding the porosity. Nevertheless, the benefits of reducing porosity for increasing hardness can be seen by plotting hardness versus porosity of the specimens, as shown in Figure 14f-g. Hardness indentations were placed so that each individual value was measured in an area that was dense in the cross section but might still be influenced by surrounding pores. Since each specimen was fabricated with different thermal conditions, a direct comparison between the as-built hardness is not necessarily meaningful. However, as mentioned in Section 3.3 hardness plateaus that eliminate the influence of the previous thermal history can be reached after 4 h ageing. In the aged specimens, an increase in hardness with a decrease in porosity can be clearly observed. The standard deviation of the hardness values measured on each specimen also varies with porosity with a roughly increasing trend. These data points are distributed in a discrete manner, indicating that other factors besides porosity can affect hardness.

Layer Overlap Ratio of 3D-Parts
Specimens which have relatively low porosities and were fabricated with a stepwise variation of the energy per unit length E' (=P/v) as well as the same travel speed and scan strategy were selected. Layer thickness was measured on etched specimen cross-sections to calculate the layer overlap ratio O L (defined in Figure 7b), as shown in Figure 15a-e. The relationships between E' and O L as well as the hardness (after ageing at 325 • C for 4 h) are shown in Figure 15f-h. The relationship between the calculated O L and the corresponding E' is shown in Figure 15f. A lower O L or E' correlates with a higher hardness level, as shown in Figure 15g-h, so that the average hardness value of Bo1 (147 HV0.1) is about 17 HV0.1 higher than that of Bo3. The deviation of the hardness values is consistent with that observed in Figure 14 regarding the porosity. To understand the effect of OL and E' on the hardness, hardness mapping performed in matrices covering several track cross-sections each in the top (i.e., the deposited) layers of the specimen Bo1, Bo2, and Bo3, as shown in Figure 16. The pro parameters of the specimens differ only in the laser power. The test load used was 10 (i.e., ~1/100 of HV0.1), allowing densely arranged (20 µm distance) µm-sized indenta as shown in Figure 16, so that the local hardness of the material among pores ca precisely measured without the interference of pores like that observed in microhard tests (Figures 14 and 15). The material at the boundaries of the tracks after ageing generally softer (about 130-150 HV10 mN) than in the cores (about 160-180 HV10 mN), so fan-shaped patterns were also observed in the color-coded contour maps of the hard distributions, as shown in Figure 16b-d. In the specimen with the highest OL (i.e., 74.4 as shown in Figure 16b, the harder cores of the tracks of previous layers were all rem and covered by the softer boundaries of following layers, so that the fan-shaped pa is only recognizable in the uppermost layer. On the contrary, fan-shaped patterns alternating but overall increased hardness values are seen over the layers in the specim with the lower OL (i.e., 70.39% and 65.95%), as shown in Figure 16c-d. More of the cores have been preserved instead of being covered and have undergone a more r cooling that is beneficial for hardening. Although the hardness measured at boundaries is lower than that measured in the cores, it is still higher than that (about 130 HV10 mN) of the materials in the as-built state, as shown in Figure 16e-g. To understand the effect of O L and E' on the hardness, hardness mapping was performed in matrices covering several track cross-sections each in the top (i.e., the last deposited) layers of the specimen Bo1, Bo2, and Bo3, as shown in Figure 16. The process parameters of the specimens differ only in the laser power. The test load used was 10 mN (i.e.,~1/100 of HV0.1), allowing densely arranged (20 µm distance) µm-sized indentations as shown in Figure 16, so that the local hardness of the material among pores can be precisely measured without the interference of pores like that observed in microhardness tests (Figures 14 and 15). The material at the boundaries of the tracks after ageing are generally softer (about 130-150 HV 10 mN ) than in the cores (about 160-180 HV 10 mN ), so that fan-shaped patterns were also observed in the color-coded contour maps of the hardness distributions, as shown in Figure 16b-d. In the specimen with the highest O L (i.e., 74.44%), as shown in Figure 16b, the harder cores of the tracks of previous layers were all remelted and covered by the softer boundaries of following layers, so that the fan-shaped pattern is only recognizable in the uppermost layer. On the contrary, fan-shaped patterns with alternating but overall increased hardness values are seen over the layers in the specimens with the lower O L (i.e., 70.39% and 65.95%), as shown in Figure 16c-d. More of the track cores have been preserved instead of being covered and have undergone a more rapid cooling that is beneficial for hardening. Although the hardness measured at the boundaries is lower than that measured in the cores, it is still higher than that (about 120-130 HV 10 mN ) of the materials in the as-built state, as shown in Figure 16e

Double-Stage Ageing of 3D-Parts
Double-stage ageing strategies were applied to attempt to further enhance the material. Unlike the aforementioned aged specimens which were held at a certain temperature for several hours and then cooled in air, the double-stage aged specimens were, after the first-stage heating, cooled in water and then heated again and held at a lower temperature (i.e., 150 °C or 70 °C) for several hours and finally cooled in water, as shown in Figure 17a. However, no significant further enhancement was found in these specimens compared to the single-stage aged specimens, as shown in Figure 17b,c. Although slightly higher average hardness values ( 5-7 HV0.1) were measured in the specimens (i.e., Ex1, Fo2) aged at 70 °C in the second stage, the increase cannot be ruled out as a statistical coincidence, since the measurement values themselves deviate considerably, as shown in Figure 17b. In another specimen (i.e., Bo1), several values that were obviously smaller (i.e., <100 HV98 mN) than the average hardness were trimmed to exclude the influence of pores on the statistics. There are still not many differences seen between the specimens, as shown in Figure 17c. This indicates, however, a good tolerance of the material in the exposure to this temperature range.

Double-Stage Ageing of 3D-Parts
Double-stage ageing strategies were applied to attempt to further enhance the material. Unlike the aforementioned aged specimens which were held at a certain temperature for several hours and then cooled in air, the double-stage aged specimens were, after the first-stage heating, cooled in water and then heated again and held at a lower temperature (i.e., 150 • C or 70 • C) for several hours and finally cooled in water, as shown in Figure 17a. However, no significant further enhancement was found in these specimens compared to the single-stage aged specimens, as shown in Figure 17b,c. Although slightly higher average hardness values (∆ 5-7 HV0.1) were measured in the specimens (i.e., Ex1, Fo2) aged at 70 • C in the second stage, the increase cannot be ruled out as a statistical coincidence, since the measurement values themselves deviate considerably, as shown in Figure 17b. In another specimen (i.e., Bo1), several values that were obviously smaller (i.e., <100 HV 98 mN ) than the average hardness were trimmed to exclude the influence of pores on the statistics. There are still not many differences seen between the specimens, as shown in Figure 17c. This indicates, however, a good tolerance of the material in the exposure to this temperature range.

Tensile Test of 3D-Parts
Two specimens (i.e., Bo4 and Bo5) of about ten times the height of the previous ones were prepared for tensile tests. The process parameters used were the same as those for the specimen (i.e., Bo1) with the highest hardness. Considering the repeated heating during the process (i.e., intrinsic heat treatment [53]) and the heat dissipation becomes difficult as the specimen height increases, the two specimens were cooled in two different ways. For Bo4, the process was suspended after the 150th and the 220th layer, respectively, and was restarted after cooling the specimen and the cooling unit to room temperature. The temperature near the top layers of the specimen (i.e., about 3 mm) before cooling was about 300 °C. For Bo5, to ensure the temperature near the top layers did not exceed 120 °C, the process was suspended for cooling the specimen and the cooling unit to room temperature after every 3 to 4 layers. The stress-strain curves of Bo4 in the as-built (i.e., Bo4-A) and aged (i.e., Bo4-B) state are nearly identical and have a tensile strength of about 300 MPa, as shown in Figure 18a. On the contrary, Bo5 has a significantly higher tensile strength increment from 334 MPa to higher than 400 MPa by ageing. As observed in the hardness test, there is little difference between the curves of a single-stage aged (i.e., Bo5-B) and double-stage aged (i.e., Bo5-E) Bo5 sample. A high-level cross-sectional porosity of 6.05% was measured in Bo4, and two zones with fewer pores were observed near where the process was suspended, as shown in Figure 18b. The cross-sectional porosity (i.e., 1.56%) of Bo5 as a whole is generally as low as that of the low porosity zones of Bo4, only slightly higher at the top of the upper part, as shown in Figure 18c, where heat dissipation is less. Although the porosity is still high, the tensile strength of Bo4 after ageing is about 10% higher than that of specimens fabricated by conventional DED, as shown in Figure  18a. Since some specimens (e.g., Ad1 and Bo1) in this work have an average hardness of nearly 150 HV0.1 despite the high porosity, much better tensile performance would be obtained, if the process is applied to alloys (e.g., AlCaScZr [54]) that are less prone to generate pores or if the cooling and inert gas shielding conditions can be further improved.

Tensile Test of 3D-Parts
Two specimens (i.e., Bo4 and Bo5) of about ten times the height of the previous ones were prepared for tensile tests. The process parameters used were the same as those for the specimen (i.e., Bo1) with the highest hardness. Considering the repeated heating during the process (i.e., intrinsic heat treatment [53]) and the heat dissipation becomes difficult as the specimen height increases, the two specimens were cooled in two different ways. For Bo4, the process was suspended after the 150th and the 220th layer, respectively, and was restarted after cooling the specimen and the cooling unit to room temperature. The temperature near the top layers of the specimen (i.e., about 3 mm) before cooling was about 300 • C. For Bo5, to ensure the temperature near the top layers did not exceed 120 • C, the process was suspended for cooling the specimen and the cooling unit to room temperature after every 3 to 4 layers. The stress-strain curves of Bo4 in the as-built (i.e., Bo4-A) and aged (i.e., Bo4-B) state are nearly identical and have a tensile strength of about 300 MPa, as shown in Figure 18a. On the contrary, Bo5 has a significantly higher tensile strength increment from 334 MPa to higher than 400 MPa by ageing. As observed in the hardness test, there is little difference between the curves of a single-stage aged (i.e., Bo5-B) and double-stage aged (i.e., Bo5-E) Bo5 sample. A high-level cross-sectional porosity of 6.05% was measured in Bo4, and two zones with fewer pores were observed near where the process was suspended, as shown in Figure 18b. The cross-sectional porosity (i.e., 1.56%) of Bo5 as a whole is generally as low as that of the low porosity zones of Bo4, only slightly higher at the top of the upper part, as shown in Figure 18c, where heat dissipation is less. Although the porosity is still high, the tensile strength of Bo4 after ageing is about 10% higher than that of specimens fabricated by conventional DED, as shown in Figure 18a. Since some specimens (e.g., Ad1 and Bo1) in this work have an average hardness of nearly 150 HV0.1 despite the high porosity, much better tensile performance would be obtained, if the process is applied to alloys (e.g., AlCaScZr [54]) that are less prone to generate pores or if the cooling and inert gas shielding conditions can be further improved. The specimen "Con-aged (5 h at 300 °C, air cooled)" and "Con-as-built" are reference specimens fabricated by conventional DED using the laser power of 620 W, travel speed of 550 mm/min, powder feed rate of 0.18 g/min, and other settings according to [41] (more details is shown in Figure A2 in Appendix B).

Process Regimes of DED
A moving point heat source problem can be treated as a problem in which the heat source stays stationary and the substrate has a backward movement, which causes an advection of heat in the substrate in addition to the heat conduction effect [55]. The Péclet number (Pe) represents the ratio of the heat transport rate by the conduction, and the advection and can be rewritten [55] as a Rykalin number (Ry) [56], interpreting the moving source problem: where v is the travel speed, α is the laser absorption rate, P is the laser power, a is the thermal diffusivity, k is the thermal conductivity, Tl is the melting temperature, T0 is the room temperature, and L = αP/[4πk(Tl−T0)] is the characteristic length as related to the temperature gradient at the fusion line induced by the heat source. If the DED process is considered as a simplified problem of a moving point heat source, the combination of the process parameter v and P, as shown in Figure 19a, determines the Ry of the DED process.
In moving point heat source problems, an Ry of 0.7359 is proposed as the divider between the high-speed regime (more precisely, if Ry ≥ 5.2611) and low-speed regime (more precisely, if Ry ≤ 0.1161) [55], which are well consistent with the process regimes of DED defined in this work, as shown in Figure 19b. The specimen "Con-aged (5 h at 300 • C, air cooled)" and "Con-as-built" are reference specimens fabricated by conventional DED using the laser power of 620 W, travel speed of 550 mm/min, powder feed rate of 0.18 g/min, and other settings according to [41] (more details is shown in Figure A2 in Appendix B).

Process Regimes of DED
A moving point heat source problem can be treated as a problem in which the heat source stays stationary and the substrate has a backward movement, which causes an advection of heat in the substrate in addition to the heat conduction effect [55]. The Péclet number (Pe) represents the ratio of the heat transport rate by the conduction, and the advection and can be rewritten [55] as a Rykalin number (Ry) [56], interpreting the moving source problem: where v is the travel speed, α is the laser absorption rate, P is the laser power, a is the thermal diffusivity, k is the thermal conductivity, T l is the melting temperature, T 0 is the room temperature, and L = αP/[4πk(T l − T 0 )] is the characteristic length as related to the temperature gradient at the fusion line induced by the heat source. If the DED process is considered as a simplified problem of a moving point heat source, the combination of the process parameter v and P, as shown in Figure 19a, determines the Ry of the DED process. In moving point heat source problems, an Ry of 0.7359 is proposed as the divider between the high-speed regime (more precisely, if Ry ≥ 5.2611) and low-speed regime (more precisely, if Ry ≤ 0.1161) [55], which are well consistent with the process regimes of DED defined in this work, as shown in Figure 19b. Melting efficiency ηm characterizes the fraction of energy used to melt the material as a percentage of the total energy input: where ρ is the density, cp is the specific heat capacity, and A is the cross-sectional area of the fusion zone [57]. In DED, the area A can be treated as the sum of the cross-sectional area of the deposition zone ADE and the cross-sectional area of the dilution zone ADI.
In moving point heat source problems, the ηm has a theoretical maximum of 36.79%, since the fusion zone center must be overheated [57]. Taking the measured ADE and ADI shown in Figure 8d,e into (4), the ηm of this work can be calculated. It is noted that the practice of DED processes, because of the influence of laser beam shape, powder feeding and the temperature related material properties, etc., deviates from the simplified situation. However, as the travel speed increases, the calculated ηm converges also to an asymptote, and a higher ηm will be achieved, if the powder feed rate per unit length increases, as shown in Figure 19c. Two ηm can be compared using By taking a value obtained in the low-speed regime as the 100% reference point, the max. ηm obtained in the high-speed regime is about 60 times higher, as shown in Figure  19d. Melting efficiency η m characterizes the fraction of energy used to melt the material as a percentage of the total energy input: where ρ is the density, c p is the specific heat capacity, and A is the cross-sectional area of the fusion zone [57]. In DED, the area A can be treated as the sum of the cross-sectional area of the deposition zone A DE and the cross-sectional area of the dilution zone A DI .
In moving point heat source problems, the η m has a theoretical maximum of 36.79%, since the fusion zone center must be overheated [57]. Taking the measured A DE and A DI shown in Figure 8d,e into (4), the η m of this work can be calculated. It is noted that the practice of DED processes, because of the influence of laser beam shape, powder feeding and the temperature related material properties, etc., deviates from the simplified situation. However, as the travel speed increases, the calculated η m converges also to an asymptote, and a higher η m will be achieved, if the powder feed rate per unit length increases, as shown in Figure 19c. Two η m can be compared using By taking a value obtained in the low-speed regime as the 100% reference point, the max. η m obtained in the high-speed regime is about 60 times higher, as shown in Figure 19d.
More precise heat flow calculations are performed based on a simulation tool developed for DED processes [58,59]. The temperature-dependent heat capacity of the material is measured by DSC (differential scanning calorimetry), as shown in Figure 20a. The thermal conductivity and the density are given by the material supplier, as shown in Figure 20b,c. The solidus (574 • C) and liquidus temperature (638 • C) are adopted from those of 5083 Al-alloy. The heat of fusion (10.79 kJ/mol) and temperature-dependent surface tension (γ(T) = 993 − 0.127T mN/m) are adopted from those of Al. The laser power intensity has a Gaussian distribution. The laser spot diameter is 1.3 mm. Material absorptivity, considering the influence of power conveying, is set at 38%. The heat flow is in quasistationary state. The temperature field and the cooling rate on the solidification front of 605 • C isotherm of single tracks are then simulated by changing the travel speed v, laser power P, power feed rateṁ, and the substrate temperature in the low-speed regime, as shown in Figure 21a,b, and in the high-speed regime (Figure 21c,d). It is seen that the cooling rates at high travel speeds, even with an increased substrate temperature, are still one to two orders of magnitude higher than at low travel speeds. More precise heat flow calculations are performed based on a simulation tool developed for DED processes [58,59]. The temperature-dependent heat capacity of the material is measured by DSC (differential scanning calorimetry), as shown in Figure 20a. The thermal conductivity and the density are given by the material supplier, as shown in Figure 20b,c. The solidus (574 °C) and liquidus temperature (638 °C) are adopted from those of 5083 Al-alloy. The heat of fusion (10.79 kJ/mol) and temperature-dependent surface tension (γ(T) = 993 − 0.127T mN/m) are adopted from those of Al. The laser power intensity has a Gaussian distribution. The laser spot diameter is 1.3 mm. Material absorptivity, considering the influence of power conveying, is set at 38%. The heat flow is in quasi-stationary state. The temperature field and the cooling rate on the solidification front of 605 °C isotherm of single tracks are then simulated by changing the travel speed v, laser power P, power feed rate ṁ, and the substrate temperature in the low-speed regime, as shown in Figure 21a,b, and in the high-speed regime (Figure 21c,d). It is seen that the cooling rates at high travel speeds, even with an increased substrate temperature, are still one to two orders of magnitude higher than at low travel speeds.  Results of the simulation of the temperature fields (a-d) and the corresponding cooling rates Ṫ on the solidification front of 605 °C isotherm (e-h) by changing the travel speed v, laser power P, power feed rate ṁ, and the substrate temperature.

Ageing Response
The inadequate ageing response of specimens of AlMgScZr alloys fabricated with DED is considered as an important reason for their poorer mechanical properties compared to the process outcome of LPBF. The as-built specimens fabricated with conventional DED exhibit a hardness level of about 100 HV0.1, for example, the 102 HV0.1 of the specimen fabricated with 550 mm/min as shown in Figure A2e, which is close to that (e.g., 105 HV0.3 [28]) of the as-built specimens fabricated with LPBF. However, the More precise heat flow calculations are performed based on a simulation tool developed for DED processes [58,59]. The temperature-dependent heat capacity of the material is measured by DSC (differential scanning calorimetry), as shown in Figure 20a. The thermal conductivity and the density are given by the material supplier, as shown in Figure 20b,c. The solidus (574 °C) and liquidus temperature (638 °C) are adopted from those of 5083 Al-alloy. The heat of fusion (10.79 kJ/mol) and temperature-dependent surface tension (γ(T) = 993 − 0.127T mN/m) are adopted from those of Al. The laser power intensity has a Gaussian distribution. The laser spot diameter is 1.3 mm. Material absorptivity, considering the influence of power conveying, is set at 38%. The heat flow is in quasi-stationary state. The temperature field and the cooling rate on the solidification front of 605 °C isotherm of single tracks are then simulated by changing the travel speed v, laser power P, power feed rate ṁ, and the substrate temperature in the low-speed regime, as shown in Figure 21a,b, and in the high-speed regime (Figure 21c,d). It is seen that the cooling rates at high travel speeds, even with an increased substrate temperature, are still one to two orders of magnitude higher than at low travel speeds.  Results of the simulation of the temperature fields (a-d) and the corresponding cooling rates Ṫ on the solidification front of 605 °C isotherm (e-h) by changing the travel speed v, laser power P, power feed rate ṁ, and the substrate temperature.

Ageing Response
The inadequate ageing response of specimens of AlMgScZr alloys fabricated with DED is considered as an important reason for their poorer mechanical properties compared to the process outcome of LPBF. The as-built specimens fabricated with conventional DED exhibit a hardness level of about 100 HV0.1, for example, the 102 HV0.1 of the specimen fabricated with 550 mm/min as shown in Figure A2e, which is close to that (e.g., 105 HV0.3 [28]) of the as-built specimens fabricated with LPBF. However, the Figure 21. Results of the simulation of the temperature fields (a-d) and the corresponding cooling ratesṪ on the solidification front of 605 • C isotherm (e-h) by changing the travel speed v, laser power P, power feed rateṁ, and the substrate temperature.

Ageing Response
The inadequate ageing response of specimens of AlMgScZr alloys fabricated with DED is considered as an important reason for their poorer mechanical properties compared to the process outcome of LPBF. The as-built specimens fabricated with conventional DED exhibit a hardness level of about 100 HV0.1, for example, the 102 HV0.1 of the specimen fabricated with 550 mm/min as shown in Figure A2e, which is close to that (e.g., 105 HV0.3 [28]) of the as-built specimens fabricated with LPBF. However, the hardness of the specimen fabricated with conventional DED was only increased by 26 HV0.2 (i.e., 255 MPa in SI unit) by ageing at 300 • C for 5 h. The yield strength of the specimen fabricated and aged in the same way was recorded with a yield strength increase of 95 MPa, as shown in Figure 18a. Such an ageing response is only about 40% as high as that obtained in specimens fabricated with LPBF, for example, an increment of 72 HV0.3 in hardness [28] and 234 MPa in yield strength [49]. The proportional relationship between this hardness increment and the yield strength increment observed in conventional DED and LPBF roughly corresponds to the empirical Tabor's relationship [60]: where H is the hardness in SI unit and σ y is the uniaxial yield strength. The highest hardness increment observed in this work in the aged specimens fabricated with high-speed DED was 47 HV0.1 (i.e., 460.6 MPa in SI unit), as shown in Figure 13a, which according to the Tabor's relationship should correspond to a yield strength increment of about 153 MPa. The actual measured yield strength increment of 132 MPa (i.e., Bo5-E vs. Bo5-A, as shown in Figure 18a), although slightly lower than this value, is despite the higher porosity level about 40% higher than that observed in conventional DED and is further close to the outcome of LPBF.

Conclusions
This work demonstrates laser directed energy deposition (DED) of AlMgScZr alloys in high-speed process regimes and elucidates the mechanism of enhancing the hardness and tensile strength of AlMgScZr alloys by increasing the cooling rate during the process as well as reducing the track overlapping and the porosity of the specimen. The results of this study indicate that:

1.
Cooling rates of Al alloys in high-speed regimes (travel speed ≥20 m/min) can theoretically reach up to about 2.34 × 10 5 K/s. This is an increase of 1-2 orders of magnitude compared to that of conventional DED, thus increasing the overall precipitation strengthening potential of every single track.

2.
Since single tracks of AlMgScZr alloys are observed to have soft fringes and hard cores on their cross-sections, decreasing the amount of remelted area when tracks overlap can increase the percentage of the hard zones. This can be achieved by decreasing the energy per unit length E' (= Laser power P/travel speed v) and increasing the powder feed rate per unit length m' (= powder feed rateṁ/travel speed v), ultimately obtaining a high deposition-to-dilution ratio of 30%, which allows one to fabricate bulk 3D-parts having an average hardness of nearly 150 HV0.1 and a tensile strength of 407 MPa (with E' = 5400 J/m, m' = 0.25 g/m and ageing at 325 • C for 4 h).

3.
Concepts that have better cooling and Ar shielding conditions are proven effective, and these are beneficial for reducing the porosity and improving the mechanical performance of the material. Notwithstanding that the current experimental setup does not allow for more precise studies regarding the material oxidation during the high-speed DED process, the signs of trends observed in this work suggest there would be a fruitful area for further work. Funding: This research was funded by the DFG-NSFC Sino-German Research Program (project grant No. GZ 1217). The raw/processed data required to reproduce these findings can be shared after reasonable inquiry.
Institutional Review Board Statement: Not applicable.

Informed Consent Statement: Not applicable.
Data Availability Statement: Not applicable.

Conflicts of Interest:
The authors declare no conflict of interest.
Appendix A. Raw Data of Single Tracks Figure A1. Plot graphs of the data shown in Figure 8 and supplementary data of "low-speed regime" (also see Figure 19) of (a) track width w, (b) track height h, (c) cross-sectional area of the deposition zone A DE , (d) melt pool depth d, and (e) cross-sectional area of the dilution zone A DI against laser power P with different powder feed rate per unit length m'. Every point refers to the average value of three measurements. The corresponding travel speeds are marked in (a). Figure A2. Specimens made of the same material by conventional DED [41], as mentioned in Figure  18 (laser power P = 620 W, travel speed v = 550~3000 mm/min, powder feed rate ṁ = 0.18 g/min, shielding gas flow rate 9 l/min, conveying gas flow rate 5 l/min, laser spot diameter = 1.