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<p>  </p> <p>  In this study, whey protein isolate (WPI) and high gellan gum (HAGG) were selected as natural ingredients to produce food-grade biopolymer particles for stabilizing the air-water interface. To achieve this, different mixing ratios of WPI and HAGG were employed, and heat treatment was implemented at different pH levels under the same concentration based on investigations of the pH-driven phase behavior of the WPI/HAGG complex system. The resulting WPI/HAGG complex particles were then evaluated for their ability to stabilize air-water interfaces by measuring their foaming properties.</p> <p><br></p> <p>  Foams generated using 0.1% (wt/wt) WPI/HAGG complex particles, heated at pH 5 with the mixing ratio 2:1 has demonstrated enhanced stability over a period of 30 hours compared to the WPI alone. The unique properties of these complex particles, including their smaller size (around 500nm), greater negative charge (more negative than -30 mV), and compact spherical core-shell structure, along with the higher viscosity in the continuous phase as well as the presence of small protein particles and gellan chains at the interface, collectively contribute to their superior performance as foam stabilizers. This allows for the creation of aerated food products with desirable characteristics, including product handling, enhanced texture, and prolonged shelf life in food industry.</p>

Syfte  Syftet med föreliggande studie var att undersöka hur böjhållfastheten på zirkonia påverkas av värmebehandling, ytbehandlingar vid re-cementering och långtidsförvaring i cirka två år. Material och metod I en tidigare studie av A.Cervenka och H. Ekdahl (7) designades 30 stycken zirkoniahättor, med måtten 6 mm i tjocklek och 14 mm i ⌀(Z-CAD, HTL, Metoxit), i ett CAD-program (3shape) och frästes (DATORN 5).  Zirkoniahättorna delades in i tre grupper med tio provkroppar i varje grupp, beroende på ytbehandling: kontrollgrupp (C), sandblästring med aluminiumoxid (A) och skrapning (S). Zirkoniahättorna cementerades på titandistanser. Grupp S och grupp A utsattes för värmebehandling, för att kunna lossa hättorna från titandistanserna. Överskottet av cement avlägsnades genom två olika ytbehandlingar innan recementering (A respektive S). Samtliga grupper termocyklades i 5000 cykler (5° till 55°) innan de utsattes för ett draghållfasthetstest. När föreliggande studie genomfördes hade zirkoniahättorna förvarats torrt i rumstemperatur i cirka två år. Zirkoniahättornas underdel slipades ner till 2,9 mm i tjocklek i en slipmaskin (Phoneix 4000) för att tillverka provkroppar lämpade för utförande av ett biaxialt böjhållfasthetstest. Resultaten analyserades med One-way ANOVA, Tukey’s test med en signifikansnivå på α =0,05.   Resultat Det biaxiala böjhållfasthetstestet påvisade att grupp C hade högst medelvärde och S hade lägst medelvärde. Det fanns inte någon signifikant skillnad mellan grupperna, p&gt;0,05.  Slutsats Inom ramen för föreliggande studie kan följande slutsats dras:  Böjhållfastheten på zirkoniahättor som har långtidsförvarats i cirka två år påverkas inte av tidigare genomförd värmebehandling och olika ytbehandlingar vid recementering / Purpose The purpose of the present study was to investigate how the flexural strength of zirconia is affected by heat treatment, various surface treatments during re-cementation, and long term storage for about two years. Material and method In a previous study by A.Cervenka and H. Ekdahl (7), 30 zirconia copings, measuring 6 mm in thickness and 14 mm in ⌀ (Z-CAD, HTL, Metoxit), were designed in a CAD-program (3shape) and milled (DATORN 5). Zirconia copings were divided into three groups with ten specimens in each group, depending on different surface treatment: control group (C), aluminum oxide abrasion group (A) and scraping (S). Zirconia copings were cemented on titanium abutments. Group S and group A were subjected to heat treatment in order to be able to detach the zirconia copings from titanium abutments. The excess cement was removed by two various surface treatments before the recementation (A respective S). All groups were thermocycled for 5000 cycles (5 ° to 55 °) before being subjected to a tensile strength test. At the time of the present study zirconia copings had been stored dry at room temperature for about two years. The lower part of the zirconia copings was reduced to 2.9 mm in thickness using a grinding machine (Phoneix 4000)in order to produce specimens suitable to performe a biaxial flexural strength test. The results were analyzed with One-way ANOVA, Tukey's test with a significance level of α = 0.05.. Results The biaxial flexural strength test showed that group C had the highest mean and S had the lowest mean. There was no significant difference between the groups, p&gt; 0.05.  Conclusion Within the limitations of this study, the following conclusion can be drawn: The flexural strength of zirconia copings that have been stored for about two years is not affected by previously heat treatment performed during recementation and various surface treatments during recementation.

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<p> Laser powder bed fusion (LPBF) is a rapidly emerging manufacturing technology capable of producing complex part geometries through the repeated, precise laser melting of metallic powder layers. At present, the process is primarily employed in high-value-added applications which exist in the aerospace, biomedical, and dental industries. As industrial implementation of LPBF has matured, research has focused on established materials for which there are already large bodies of literature and regulatory approval, such as Inconel 718, Inconel 625, Ti-6Al-4V, and 316 stainless steel. However, the rapid solidification process inherent to LPBF leads to vastly different microstructures with improved strength compared to these traditional materials in cast or wrought forms. In general, the high solidification velocity and thermal gradients result in cellular and dendritic solidification structures with finer grain and precipitate sizes than conventionally processed alloys. These microstructure changes warrant the exploration of new alloy systems and reevaluation of historically cast compositions with optimized microstructures, especially considering the tunability of a digitally controlled fabrication process. This work examines laser powder bed fusion of Mar-M 509, a carbide-strengthened cobalt alloy that is typically investment cast directly into complex-shaped components such as nozzle guide vanes (NGVs). NGVs are stationary components in gas turbine engines for propulsion and energy production which require strength under moderate mechanical loading at high temperatures. Investment cast microstructures have porosity defects in slower-cooled regions due to lack of liquid feed to interdendritic regions. As-printed, the cellular and dendritic Mar-M 509 LPBF microstructures lead to the formation of continuous, fiber-like, eutectic carbide structures in the intercellular and interdendritic regions, which limit macroscopic ductility. Thermo-Calc is used for calculation of phase diagrams (CALPHAD) to estimate the equilibrium transformation temperatures of MC, M23C6, and M7C3-type carbides, which informs design of isothermal heat treatments to engineer microstructures with enhanced ductility over the as-printed or cast versions of Mar-M 509 while maintaining tensile strength. Scanning and transmission electron microscopy reveals the composition and distribution of carbide phases as a function of heat treatment temperature. Lastly, heat treatment recommendations for nozzle guide vanes are made.  </p>

Manufacturing of aero engine components requires attention to residual stress and final shape of the product in order to meet high quality product standards.This sets very high demands on involved manufacturing steps to meet design requirements. Simulation of manufacturing processes can therefore be animportant tool to contribute to quality assurance.The focus in this work is on simulation of a manufacturing process chain comprising of sheet metal forming, welding and a stress relief heat treatment.Simulation of sheet metal forming can be used to design a forming tool design that accounts for the material behaviour, e.g. spring back, and avoid problems such as wrinkling, thinning and cracking. Moreover, the simulation can also show how the material is stretched and work hardened. The residual stresses after forming may be of local character or global depending on the shape that is formed. However, the heat affected zone due to welding is located near the weld.The weld also causes large residual stresses with the major component along the weld. It is found that the magnitude of the residual stresses after welding is affected by remaining stresses from the previous sheet metal forming. The final stress relieve treatment will relax these residual stresses caused by e.g. forming and welding. However, this causes additional deformations.The main focus of this study is on how a manufacturing process step affects the subsequent step when manufacturing a component of the nickel-based super alloy 718. The chosen route and geometry is a simplified leading edge of an exhaust case guide vane. The simulations were validated versus experiments. The computed deformations were compared with measurements after each manufacturing step. The overall agreement between experiments and measurement was good. However, not sufficiently accurate considering the required tolerance of the component. It was found from simulations that the residual stresses after each process affects the subsequent step. After a complete manufacturing process chain which ends with a stress relief heat treatment the residual stresses were not negligible. VIII Special experiments were performed for studying the stress relief in order to understand how the stresses evolve through the heat treatment cycle during relaxation. It was found that the stresses were reduced already during the beginning of the heating up sequence due to decreasing Young´s modulus and yield stress with increasing temperature. Relaxation due to creep starts when a certain temperature was reached which gave a permanent stress relief.

15-5PH stainless steel is an important alloy in the aerospace, chemical, and nuclear industries for its high strength and corrosion resistance at high temperature. Thus, this material is a good candidate for processing development in the direct metal laser sintering (DMLS) branch of additive manufacturing. The chemistry and microstructure of this alloy processed via DMLS was compared to its conventionally cast counterpart through various heat treatments as part of a characterization effort. The investigation utilized optical microscopy, scanning electron microscopy (SEM), transmission electron microscopy (TEM), X-Ray diffractometry (XRD), energy dispersive X-Ray spectroscopy (EDS) and glow discharge atomic emission spectrometry (GDS) techniques. DMLS processed samples contained a layered microstructure in which the prior austenite grain sizes were relatively smaller than the cast and annealed prior austenite grain size. The largest of the quantifiable DMLS prior austenite grains had an ASTM grain size of approximately 11.5-12 (6.7?m to 5.6?m, respectively) and the cast and annealed prior austenite grain size was approximately 7-7.5 (31.8µm to 26.7µm, respectively), giving insight to the elevated mechanical properties of the DMLS processed alloy. During investigation, significant amounts of retained austenite phase were found in the DMLS processed samples and quantified by XRD analysis. Causes of this phase included high nitrogen content, absorbed during nitrogen gas atomization of the DMLS metal powder and from the DMLS build chamber nitrogen atmosphere. Nitrogen content was quantified by GDS for three samples. DMLS powder produced by nitrogen gas atomization had a nitrogen content of 0.11 wt%. A DMLS processed sample contained 0.08 wt% nitrogen, and a conventionally cast and annealed sample contained only 0.019 wt% nitrogen. In iron based alloys, nitrogen is a significant austenite promoter and reduced the martensite start and finish temperatures, rendering the standard heat treatments for the alloy ineffective in producing full transformation to martensite. Process improvements are proposed along with suggested future research.

The focus of this master’s thesis is on the heat treatment of Ni-base alloys, specifically the risk of intermetallic σ-phases during different stages of heat treatment. The alloy studied is Sanicro®28, a super-austenitic stainless steel produced by Alleima AB. The problem at hand is that the quench-annealing stage is in high demand at the manufacturing facility, and the goal is to investigate if it can be removed from the manufacturing route. During forging, the outer surface and bar-ends can reach low temperatures, posing a high risk of σ-phase precipitation. Additionally, a necklace structure with large grains surrounded by fine re-crystallization is often observed at the surface of forged superalloys/Ni-base alloys. Today, this forged structure is re-crystallized and σ-phase dissolved during the quench-annealing stage. An alternative to quench-annealing after forging is to re-heat the bar using a Car Wagon Furnace(CWF). The thesis includes two laboratory experiments simulating two stages of heat treatment, the CWF and induction furnaces/soaking. The samples subjected to simulated CWF treatment showed re-crystallization throughout the entire structure. Annealing in CWF removes the large grains in surface positions. The time in the CWF also showed to be sufficient to dissolve σ-phase present from forging. Samples heated to the induction furnace set temperature do not contain precipitates, while temperatures below the induction set temperature induce σ precipitation to varying degrees. The key findings of the thesis are as follows: • Re-heating in a CWF right after forging is enough to dissolve σ-phase at half-radius and surface locations. • Quench-annealing stage could be removed by changing the route to a CWF after forging. • If temperatures fall below the σ-maximum stability temperature during induction furnace heating cycles, σ-phase precipitation occurs.

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In recent years, advancements in additive manufacturing (AM) technologies have paved the way for 3D-printed flexible hybrid electronics (FHE) and created opportunities for extending these gains to RF applications. However, printed metal interconnects and devices are typically characterized by high porosity and chemical impurities that significantly limit their electrical conductivity and RF performance compared to bulk equivalents. Using direct ink writing (DIW), two silver inks, a nanoflake suspension and a nanoparticle-reactive ink, were investigated to understand the relationship between free interfacial energy, sintering behavior, DC conductivity, and RF loss. The printed silver samples were characterized using scanning electron microscopy, x-ray diffraction, and x-ray photoelectron spectroscopy to monitor microstructural evolution, grain size and orientation, and chemical purity as a function of heat treatment temperature. Three heat treatments were applied to each ink: the manufacturer's recommendation, 225°C for 30 minutes, and 350°C for 30 minutes. Four-wire structures and coplanar waveguides were printed to compare the DC and RF performance up to 18 GHz, respectively. The results show that ink formulations that facilitate larger grains, high density, and good chemical purity have superior RF performance. A low resistivity of 1.4 times bulk Ag, average of 0.8% greater RF loss factor than evaporated Ag, and a maximum current density of 4.6 x 105 A/cm2 were achieved with printed structures. This work highlights the importance of engineering a high density and high purity microstructure in printed silver components necessary for high-performance printed electronics.