A FILLER ALLOY AND ITS PRODUCTION METHOD FOR USE IN VACUUM SOLDERING.
The modified Ag-Cu-In-Ti or Ag-Cu filler alloy with Ti6Al4V and TiH₂ powders addresses the challenges of high-temperature brazing by enhancing wetting and interface strength, ensuring reliable bonding at lower temperatures and maintaining microstructural integrity for Ti6Al4V alloy with SiO₂(f)/SiO₂ composite.
Patent Information
- Application Number
- TR202612791
- Authority / Receiving Office
- TR · TR
- Patent Type
- Applications
- Current Assignee / Owner
- Filing Date
- 2026-07-29
- Publication Date
- 2026-08-21
AI Technical Summary
Existing vacuum brazing processes for Ti6Al4V alloy with SiO₂(f)/SiO₂ composite face issues such as high temperatures leading to phase transformations, grain growth, and reduced bond strength due to brittle reaction phases and thermal expansion mismatches, resulting in cracks and limited mechanical integrity.
A modified filler alloy system comprising Ag-Cu-In-Ti or Ag-Cu with Ti6Al4V and TiH₂ powders is used to enhance wetting behavior and interface strength, allowing bonding at lower temperatures (below 900 °C) through controlled heating and cooling, with TiH₂ reacting to form a stronger bond and Ti6Al4V powder improving mechanical properties.
The modified filler alloy achieves high interfacial strength and preserves microstructural integrity, preventing phase transformations and grain growth, resulting in a mechanically reliable metal-composite connection suitable for service temperatures exceeding 450 °C.
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Abstract
Description
1 TARIFF A FILLER ALLOY FOR USE IN VACUUM SOLDERING. PRODUCTION METHOD Technical Area 5 The invention describes the formation of a composite of Ti6Al4V alloy with SiO₂(f) / SiO₂ by vacuum brazing. The invention relates to the filler alloy used in its assembly and the manufacturing method. Joining technologies for engineering materials, especially vacuum brazing and It is located in the field of metal-ceramic composite bonding techniques. It also includes fillers. Alloy modification and optimization of the interface microstructure are also technical aspects of the invention. It is part of the area. State of the Art Brazing is the process of joining two or more metal parts without melting the base materials. a filler metal with a lower melting point placed between them 15 It is the process of joining materials together. In this process, the base materials remain in a solid state. The solder alloy simply melts, wetting the surfaces, and the bonding occurs through capillary action. It spreads to the region, and after cooling, a metallurgical bond forms. Soldering is generally such as copper, brass, steel, stainless steel, aluminum, nickel alloys, and titanium. It is applied between metals. Furthermore, with appropriate interlayer and surface preparation, it can reach 20. It can also be used in ceramic-metal or composite-metal combinations. Especially in electronic circuits, heat exchangers, automotive and aerospace components, Soldering in systems requiring sealing and in precise assembly applications. It is a critical joining method. This method has lower costs compared to welding techniques. This is carried out at a temperature of 25°C. Thus, the geometric accuracy of the parts is preserved. and the risk of deformation in thin-section or heat-sensitive components is reduced. Soldering includes low-temperature soft soldering and high-temperature hard soldering. types such as brazing and those performed at even higher temperatures They are separated. Also, depending on atmospheric conditions, open atmosphere soldering, shielding gas There are also subclassifications such as atmospheric soldering and vacuum soldering. Among the advantages of soldering are the ability to join different metals. ensuring a smooth and leak-proof connection, suitability for mass production, and relatively low cost. While thermal stress is a factor, some disadvantages include reduced bond strength. 2 Lower cost compared to other welding methods, high sensitivity to surface cleaning. and the main material properties during high-temperature processing. There is a risk of change. Vacuum brazing is a brazing process performed in a low-oxygen, partial-pressure environment. This is achieved by, in particular, preventing surface oxidation and ensuring high purity. It is preferred in order to obtain homogeneous bonds. This method is used with titanium and titanium alloys (e.g., Ti6Al4V), nickel-based superalloys, stainless steels, among carbides, ceramic-metal combinations and advanced composite materials It is widely used to achieve high-performance connections. Vacuum 10 Thanks to its medium, there is no need to use flux. Thus, especially required in aviation, defense, medical implant and high temperature applications. Clean and controlled connections are ensured. Furthermore, the vacuum soldering process... This requires furnace systems with high investment costs, and process parameters (temperature, time, pressure) requires precise control and the filler used 15 Depending on the alloy, this can be achieved at temperatures exceeding 900 °C. These high temperatures cause phase transformations and grain changes in alloys such as Ti6Al4V. This can affect mechanical properties by causing growth. Therefore, most In order to prevent critical changes in the microstructure during the application, the processing time is one hour. It is kept short. On the other hand, silica-based materials such as SiO₂(f) / SiO₂ composites 20 It is more sensitive to high temperatures and becomes amorphous at temperatures above 870 °C. A transformation from the structural phase to the crystalline tridymite phase can occur. This phase transformation... significantly improves the mechanical strength and thermal expansion behavior of silica. It changes the material selection, temperature-time in vacuum soldering. This necessitates careful process design in terms of optimization and microstructural stability. 25 It makes it possible. The study by Huang et al., which is part of the state of the art, uses pulsed Nd:YAG. Addition of Zr to AgCu28-4.5Ti based active solder (AgCu28- The interface structure and its effect on performance in 4.5Ti-4Zr) Ti Gr.1–AISI 1045 joints 30 It examines them comparatively. The study includes both zirconium and non-zirconium products. Direct comparison of systems, combining SEM / EDS / XRD + hardness + tribology tests. Its use and the addition of Zr increase element diffusion and excessive brittle phases such as Cu3Ti. By reducing its formation, it provides more homogeneous hardness / interface and better ductility. 3 However, brittle reaction phases (especially Cu3Ti) are clearly observed in the study. It is being discussed, and there are signs of micro-crack risk and interface-related weaknesses. In addition, the bond strength (tensile / shear) and fracture starting from the interface There are also shortcomings in mechanical fracture tests that directly prove that it has not started. There are 5. In the current technique, high soldering temperatures are used, and these high temperatures... The resulting residual thermal stresses between SiO₂f / SiO₂ composite and Ti-6Al-4V The risk of cracks due to the mismatch in the coefficient of thermal expansion occurs at the interface. Brittle reaction phases, limited bond strength, and frequent joint fractures are common in 10 years. Due to issues such as starting in the interface region, there is a need for development in this area. It has been deemed necessary to do so. Brief Description and Objectives of the Invention The invention describes a silver-copper-indium-titanium, Ag-Cu-In-Ti, alloy system and silver-copper, 15 Ag-Cu, alloy system filler alloys weak on SiO₂(f) / SiO₂ composite Modification with Ti6Al4V and TiH₂ powders to improve wetting behavior It is explained that the soldering process aims to preserve the properties of the main material. This is carried out under controlled heating and cooling profiles. The main objective of the invention is to create composite materials of Ti6Al4V alloy with SiO₂(f) / SiO₂. reliable, with high interface strength and preserved microstructural integrity. a filler alloy with improved properties that enables such bonding The aim is to provide this. To this end, silver-copper-indium-titanium (Ag-Cu-In-Ti) alloy system and silver-copper (Ag-Cu) alloy system, based on a modified filler 25 The structure is formed using SiO₂(f) / SiO₂ composite filler alloys. to improve the limited wetting behavior on it and more at the metal-ceramic interface In order to develop effective reaction mechanisms, these alloys Ti6Al4V and TiH₂ powders It is enriched with additives. Thanks to its powder-added structure, the solder filler alloy... The spreading capability is increased, and controlled Ti-based reaction phases are formed at the interface. 30 by creating a more homogeneous solder layer and a stronger metal-composite A bonding region is obtained. The main function of the TiH2 compound here is to bind to SiO2. By undergoing a chemical reaction on its surface, the oxide-metal interface is more easily formed. The aim is to create a composite structure in the solder alloy. The effect of Ti6Al4V powder is to create a composite structure in the solder alloy. 4 as a component, it contributes to the structure both mechanically and ultimately in a mechanical sense. by increasing the percentage of titanium element in the filler alloy, the alloy's oxide The aim is to increase the wetting ability of the surface. Thus, thermal expansion. reducing stress concentrations that may result from incompatibility and unification The aim is to increase its strength. The performance of the developed filler alloy is 5 This has been verified through hardness and mechanical strength tests. The interface microstructure was determined using SEM and... The connection, which was examined using EDS analyses, has both mechanical and microscopic aspects. Its effectiveness is demonstrated from a structural perspective. Another objective of the invention is to produce SiO₂-based composites with Ti6Al4V alloy in vacuum 10°C. which makes it possible to join at low temperatures using the soldering method and at the same time The goal is to provide an optimized filler alloy that offers high interfacial strength. Thanks to the filler alloy described in this invention, the soldering process can be carried out at temperatures below 900 °C. Phase transformation and grain growth in Ti6Al4V alloy are achieved by performing this procedure. is limited. In SiO₂-based composites, the crystalline phase is affected by high temperatures. Changes are prevented. In addition, the composition of the filler alloy and the powder subject to the invention... wetting behavior by systematically optimizing the additive ratios is being improved, the interface microstructure is being created in a controlled manner, and the merging is taking place. Its strength is increased. Thus, both the microstructural integrity of the main materials is preserved. a metal-composite 20 that provides both protection and maximum mechanical performance The connection structure is obtained. Explanation of the Figures Figure 1: SEM image taken from the interface between the filler alloy and SiO2 after the process. Figure 2: Post-processing filler alloy and SiO2 EDS mapping image 25 Detailed Description of the Invention The invention describes the low-temperature vacuum brazing of Ti6Al4V alloy with SiO₂(f) / SiO₂ composite. Modified filler alloy and production method for effectively bonding with It is related to the following: Ti6Al4V and TiH₂ powder are added to the filler alloy, which is the subject of the invention, in specific proportions. By doing this, the wetting and bonding strength is increased. The aforementioned filler alloy... Mechanical performance has been verified by shear tests, and interface formation is microstructural. It has been examined through analyses. Titanium-6Aluminum-4Vanadium (Ti6Al4V) alloy with Silicon Dioxide Fiber Used in vacuum brazing of reinforced silicon dioxide (SiO₂(f) / SiO₂) composite. filler alloy, Ag-Cu-In-Ti alloy system and Ti6Al4V-titanium dihydride (TiH2) powder mixture or Ag-Cu alloy system and Ti6Al4V-TiH2 powder mixture 5 It includes. In other words, the final filler alloy, Ti6Al4V alloy as the bonding material, Ag-Cu filler as the interface matrix alloy, Ti6Al4V powder as interface additive and bonded material 10 as SiO2(f) / SiO2 or Ti6Al4V alloy as the bonding material, Ag-Cu-In-Ti as the interface matrix filler alloy, Ti6Al4V powder as interface additive and combined SiO2(f) / SiO2 composite as a material It includes. 15 In one application of the invention, the filler alloy 85-95% by weight Ag-Cu-In-Ti alloy system and 5-15% by weight Ti6Al4V-TiH2 powder mixture or 85-95% by weight Ag-Cu alloy system and 5-15% by weight Ti6Al4V-TiH2 powder 20 mixture It includes. In another application of the invention, the filler alloy 90% by weight Ag-Cu-In-Ti alloy system and 10% by weight Ti6Al4V-TiH2 powder 25 mixture or 90% by weight Ag-Cu alloy system and 10% by weight Ti6Al4V-TiH2 powder mixture It includes. Another application of the invention involves the aforementioned Ag-Cu-In-Ti alloy system, weighing 30 grams. An alloy containing 59.0% Ag, 27.25% Cu, 12.5% In, and 1.25% Ti (commercially known as Incusil ABA). It is a system. Another application of the invention is the aforementioned Ag-Cu alloy system. It is an alloy system containing 72% Ag and 28% Cu by weight (commercially known as BAg-8). The invention 6 In one application, the system in which the Ag-Cu filler alloy is used is Ti6Al4V alloy. (joined material), Ag-Cu filler alloy (interface matrix), Ti6Al4V powder (interface It contains additive material and SiO2(f) / SiO2 composite (bonded material). In one application of the invention, a system using Ag-Cu-In-Ti alloy filler alloy is employed. Ti6Al4V alloy (joint material), Ag-Cu-In-Ti filler alloy (interface matrix) 5 Ti6Al4V powder (interface additive) and SiO2(f) / SiO2 composite (bonded material) It contains TiH2, which melts at 400 °C, therefore it is present in the structures at the end of the process. It does not receive. The modification of the filler material in the invention involves the filler alloy, specifically oxide 10. because it aims to increase its activity on a ceramic in the structure, other than SiO2. It can be used for other oxides (Al2O3, ZrO2, etc.). The basic principle here is: Titanium and hydrogen have high stability in oxygen reduction reactions. the elements are present in the structure during the process and bond with the oxide surface the goal is to increase its potential. 15 Titanium-6Aluminum-4Vanadium (Ti6Al4V) alloy with Silicon Dioxide Fiber In vacuum brazing of reinforced silicon dioxide (SiO₂(f) / SiO₂) composite Production method of filler alloy for use i. Pure Ag-Cu-In-Ti alloy system 20, supplied in paste form. or the Ag-Cu alloy system is placed in a clean container and measuring its weight, ii. Pouring the TiH2 and Ti6Al4V powder into the container according to the measured weight. iii. Ethyl alcohol is added to the container to ensure more effective mixing of the components. and stirring by hand for 5 minutes, 25 iv. Then, ultrasonic probe equipment is inserted into the additive mixture. by immersing the additive in the paste for 30-90 seconds. Obtaining a paste-like filler alloy by dispersion to be done It includes the steps of the process. 30 7 An application of the method of producing the alloy described in the invention, i. Pure, 85-95% Ag-Cu- by weight, supplied in paste form. In-Ti alloy system or 85-95% by weight Ag-Cu alloy system, placed in a clean container, ii. Add 5-10% by weight TiH2 and 5-10% by weight Ti6Al4V powder to the container 5 spilling, iii. Ethyl alcohol is added to the container to ensure more effective mixing of the components. and mechanically stirring the mixture for 5 minutes, iv. Then, ultrasonic probe equipment is inserted into the additive mixture. 10 by immersing for 30-90 seconds so that the additive remains in the paste. Obtaining a paste-like filler alloy by dispersion to be done It includes the steps involved in the process. Another application of the production method described in the invention is 15 i. Pure, 90% by weight Ag-Cu-In- supplied in paste form. A clean Ti alloy system or a 90% by weight Ag-Cu alloy system. placed inside the container, ii. 5% by weight TiH2 and 5% by weight Ti6Al4V powder into the container spillage, 20 iii. Ethyl alcohol is added to the container to ensure more effective mixing of the components. and mechanically stirring the mixture for 5 minutes, iv. Then, ultrasonic probe equipment is inserted into the additive mixture. by immersing the additive in the paste for 30-90 seconds. The paste-like filler alloy obtained by dispersion is 25 to be done It includes the steps involved in the process. Additional components are used to effectively apply the paste-form alloy, which is the subject of the invention, to surfaces. The resulting ethyl alcohol is applied to the bonding surfaces before it completely evaporates. 30 In one application of the production method described in the invention, in process step (iii) 50 Ten drops of ethyl alcohol are added for each gram of alloy. In one application of the invention (iv) In step number [number], if the volume to be mixed is large, the mixing time... It is being enhanced and optionally equipped with equipment such as mixers. The invention 8 In another application, if the volume to be mixed is high in step (v) of the process The duration is increased and the ultrasonic probe / ultrasonic equipment is adjusted according to the volume being treated. is used. In the current technique, ready-made paste-form fillers are available. There are also filler alloys. However, filler alloys supplied in paste form, It contains binding polymer components in specific proportions (as specified by the manufacturer 5 (It is formulated in a ready-made form). When the procedures described in the method are applied The risk of losing the functionality provided by these readily available components. It is also present. Ethyl alcohol is used to aid in the mixing. As the addition evaporates over time, the paste-like mixture becomes excessive. It is observed to solidify and becomes unusable for application to the surface. Therefore, each application requires 10 The filler alloy addition processes for this are carried out from scratch. The subject of the invention... The filler alloys are applied to the surfaces immediately after preparation (within 15 minutes). is being implemented. Filler 15 used in vacuum brazing of Ti6Al4V alloy with SiO₂(f) / SiO₂ composite. Application method of the alloy, i. Ag-Cu-In-Ti alloy in paste form or Ag-Cu alloy Ti6Al4V-TiH2 Adding the powder mixture, ii. Adding ethyl alcohol to the paste and powder mixture and ultrasonically injecting it into the mixture. Modified by mixing and dispersing the powders through immersion of the probe device 20 obtaining the prepared paste mixture, iii. the SiO2(f) / SiO2 composite and Ti6Al4V alloy forming the pair of combinations, sanding with sandpaper, iv. 99.95% of SiO2(f) / SiO2 composite and Ti6Al4V alloy after grinding. immersion in pure ethyl alcohol and ultrasonic cleaning, 25 v. SiO2(f) / SiO2 composite and Ti6Al4V alloy in a drying oven. drying, vi. The modified paste mixture obtained in step (ii) on the surface of the dried SiO2(f) / SiO2 composite with the help of a brush implementation, 30 vii. Modified on the surface of Ti6Al4V alloy in process step (vi). a paste mixture is applied to the SiO2(f) / SiO2 composite surface Obtaining the combination pair by inserting them, 9 viii. The resulting pair of components is subjected to heat treatment in a brazing furnace. to be left It includes the steps involved in the process. Another application of the aforementioned filler alloy's application method is 5 i. Ag-Cu-In-Ti alloy or Ag-Cu alloy in paste form with 5% by weight. Addition of Ti6Al4V-TiH2 powder mixture, ii. Add 10 drops of ethyl alcohol to 50 grams of paste and powder mixture and let the mixture... by immersing an ultrasonic probe device in it for 30-60 seconds and mixing it. Obtaining a modified paste mixture by dispersing the powders, 10 iii. the SiO2(f) / SiO2 composite and Ti6Al4V alloy forming the pair of combinations, sanding with sandpaper, iv. Alcohol treatment of SiO2(f) / SiO2 composite and Ti6Al4V alloy after grinding. immersion in it and cleaning by ultrasonic method, v. Drying of SiO2(f) / SiO2 composite and Ti6Al4V alloy at 80-100 °C 15 drying in the oven for 90-120 minutes, vi. The modified paste mixture obtained in step (ii) on the surface of the dried SiO2(f) / SiO2 composite with the help of a brush implementation, vii. Modified 20 on the surface of Ti6Al4V alloy in process step (vi). a paste mixture is applied to the SiO2(f) / SiO2 composite surface Obtaining the combination pair by inserting them, viii. The resulting pair of components is brazed in a brazing furnace at 800-825 °C. Heat treatment for 15-45 minutes It includes the steps of the process. 25 Another application method of the aforementioned filler alloy is, i. a paste-like substance containing 85-95% by weight of Ag-Cu-In-Ti alloy or by weight 85-95% Ag-Cu alloy with 5-15% by weight Ti6Al4V-TiH2 powder mixture addition, 30 ii. Adding ethyl alcohol to the paste and powder mixture and ultrasonically injecting it into the mixture. The probe device is immersed for 90 seconds, stirred, and the powders are dispersed. Obtaining a modified paste mixture, iii. the SiO2(f) / SiO2 composite and Ti6Al4V alloy forming the pair of combinations, sanding with sandpaper, iv. Alcohol treatment of SiO2(f) / SiO2 composite and Ti6Al4V alloy after grinding. immersion in it and cleaning by ultrasonic method, v. Drying of SiO2(f) / SiO2 composite and Ti6Al4V alloy at 80-100 °C 5 drying in the oven for 90-120 minutes, vi. The modified paste mixture obtained in step (ii) on the surface of the dried SiO2(f) / SiO2 composite with the help of a brush implementation, vii. Modified 10 on the surface of Ti6Al4V alloy in process step (vi). a paste mixture is applied to the SiO2(f) / SiO2 composite surface Obtaining the combination pair by inserting them, viii. The resulting pair of components is brazed in a brazing furnace at 800-825 °C. Heat treatment for 15-45 minutes It includes the steps of the process. 15 The application method of the filler alloy subject to the invention is Ti6Al4V alloy with SiO₂(f) / SiO₂ the composite will be able to operate reliably under service conditions exceeding 450 °C and the same at 900 °C in a way that preserves the microstructural integrity of the base materials over time 20 modified filler alloy that enables joining by vacuum brazing underneath. It is aimed at the application. For this purpose, the process primarily involves the use of paste-like material. silver-copper-indium-titanium (Ag-Cu-In-Ti) or silver-copper (Ag-Cu) filler It begins with the addition of a powder mixture of Ti6Al4V and TiH₂ to the alloy; this step is technically... Its superiority lies in increasing the active titanium content of the filler metal, thereby improving the ceramic surface. Improvement of wettability and the reducing effect of TiH₂ thanks to 25 Si–O bonds The aim is to ensure more efficient fracture, thus enabling low-temperature melting systems. The disadvantage of poor wetting is overcome. Then alcohol is added to the paste-powder mixture. homogeneous distribution is ensured with an ultrasonic probe; this step ensures that the powders are evenly distributed. by preventing agglomeration, a controlled and even distribution of microorganisms within the filling alloy. It allows for the creation of a structure and, thanks to the fact that it can be carried out at room temperature, 30 an industrial-scale, low-energy, practical, and quickly implementable modification. The process involves sanding the joint surfaces to control surface roughness. by increasing mechanical interlocking and metallurgical contact area; subsequently in alcohol 11 Ultrasonic cleaning removes oxide, oil, and particulate residues from the surface. It ensures that interface reactions occur in a controlled manner. In the drying oven. The drying step performed leaves no moisture or solvent residue on the surface. It reduces the risk of gas formation and porosity in a vacuum environment. Modified paste. Applying the mixture to the SiO₂(f) / SiO₂ composite surface with a brush, filling thickness 5 It allows for controlled adjustment and creates a homogeneous interlayer; this This provides a more even stress distribution and increased interface strength. Ti6Al4V The combination formed by depositing the alloy onto this surface is vacuum hardened. It undergoes heat treatment in a soldering furnace at below 900 °C; this step is technically... Its superiority lies in Ag-Cu-In-Ti or Ag-Cu systems above 720 °C and 780 °C, but only 10 By taking advantage of melting ranges below 900 °C, we can achieve both low processing temperatures. This ensures both phase transformation and grain growth in Ti6Al4V, based on SiO₂. In ceramic matrix composites, the goal is to prevent phase changes due to high temperatures. The resulting coupling exhibits enhanced wetting ability and controlled interfacial reaction. Higher bond strength thanks to its phases and optimized microstructure. 15 It offers; and also operates effectively at service temperatures exceeding 450 °C. a functional, microstructural stable and mechanically reliable metal-composite It creates an interface structure. The invention relates to the alloy of Ti6Al4V (Titanium-6Aluminum-4Vanadium alloy) with SiO₂(f) / SiO₂ 20 components of the composite (Silicon Dioxide Fiber Reinforced Silicon Dioxide composite) a suitable vacuum soldering method taking into account the characteristics and application requirements They are joined using this method. The joining process keeps the processing temperature below 900 °C. commercially available silver-copper-indium-titanium (Ag- By using Cu-In-Ti and silver-copper (Ag-Cu) filler alloys in paste form, 25 This is being carried out. However, these filler alloys are on the SiO₂(f) / SiO₂ composite surface. Due to insufficient wetting performance, increasing bond strength. For this purpose, Ti6Al4V and TiH₂ powders were added to the alloys in different ratios. It has been modified in order to preserve the microstructural properties of the base materials. Soldering experiments were conducted in the temperature range of 750–850 °C, with different holding times, but only for 30 minutes. The process was carried out under the same heating and cooling profiles. Different powder concentrations were used. The spreading areas of the filler alloys were measured on the surfaces of the base materials; The hardness of Ti6Al4V alloy after soldering was determined. 800 on SiO₂ fibers. Tensile tests were performed after heat treatment up to °C, SiO₂(f) / SiO₂ 12 The samples were subjected to compression tests after each soldering operation. The joint... The strength of the region was determined by compression-shear tests, and 10% by weight of powder. In processes carried out at 800 °C using this combination, Ag-Cu-In-Ti alloy With a holding time of 15 minutes for [specific type] and 30 minutes for Ag-Cu, the pressure is approximately 16 MPa. Maximum bond strength was achieved at level 5. Mechanical test results show... This was supported by microstructural analyses of the connection interfaces and by SEM and EDS. This has been evaluated through analysis. Figure 1 shows a SEM image taken from the interface between the filler alloy and SiO2 after the process. It is located there. From Figure 1, it can be seen that the Ti6Al4V powder added to the filler alloy has a 10% interface. The physical effect is visible. The sample examined underwent destructive cutting examination. The sample was taken from a cross-section of the part after testing. The Ti6Al4V particle was dispersed. The alloy has a composite structure due to its physical structure within the filler alloy. It is seen to have formed. Also, the SiO2 layer located at the top of the image. an optimal bond layer (1-3 µm) exists between the filler alloy and the filler alloy. 15 This is observed. Figure 2 shows the interface between the filler alloy and SiO2 after the process. EDS mapping image of titanium element representing the same region as 1. Figure 2 shows the Ti6Al4V particles found in the filler alloy. This image shows the distribution of titanium element within the filler alloy. Titanium element dissolves into the filler alloy matrix from Ti6Al4V particles. 20 and diffuses within the structure. This allows the titanium in the filler alloy to penetrate. Its density is increasing and its activity on the oxide surface is enhanced. Process because its temperature is well above the melting point of TiH2 compound (~400˚C) The particle completely melts during the process and is physically detectable in these images. It cannot be done. 25 13 REFERENCES [1] Huang Y, Liang G, Lv M, Al-Nehari M, Liu D, Li G, Xiao. “Comparative study on the joining performance of TiH2 and ZrH2 modified AgCu28 brazing alloys with pulsed laser welding-brazing”. Journal of Manufacturing Processes, 41 (2019) 56-65. 10 20 30
Claims
14 REQUESTS 1. Titanium-6Aluminum-4Vanadium (Ti6Al4V) alloy with Silicon Dioxide Fiber In vacuum brazing of reinforced silicon dioxide (SiO₂(f) / SiO₂) composite It is a filler alloy intended for use and its characteristic is 5. Ag-Cu-In-Ti alloy system and Ti6Al4V-titanium dihydride (TiH2) powder mixture or Ag-Cu alloy system and Ti6Al4V-TiH2 powder mixture It includes.
2. It is a filler alloy according to claim 1, and its property is 10 85-95% by weight Ag-Cu-In-Ti alloy system and 5-15% by weight Ti6Al4V- TiH2 powder mixture or 85-95% by weight Ag-Cu alloy system and 5-15% by weight Ti6Al4V-TiH2 powder mixture It includes. 15 3. It is a filler alloy according to claim 1, and its properties are: 90% by weight Ag-Cu-In-Ti alloy system and 10% by weight Ti6Al4V-TiH2 powder mixture or 90% by weight Ag-Cu alloy system and 10% by weight Ti6Al4V-TiH2 powder mixture 20 It includes.
4. It is a filler alloy according to Claim 1, and its properties are those of the aforementioned Ag-Cu-In-Ti alloy. The alloy system contains 59.0% Ag, 27.25% Cu, 12.5% In and 1.25% Ti. It is the fact that.
5. It is a filler alloy according to Claim 1, and its property is the aforementioned Ag-Cu alloy 25 The system is an alloy system containing 72% Ag and 28% Cu by weight.
6. Titanium-6Aluminum-4Vanadium (Ti6Al4V) alloy with Silicon Dioxide Fiber In vacuum brazing of reinforced silicon dioxide (SiO₂(f) / SiO₂) composite The method of producing filler alloy for use, its characteristic feature i. Pure Ag-Cu-In-Ti alloy system 30, supplied in paste form. or the Ag-Cu alloy system is placed in a clean container and measuring its weight, ii. Pouring the TiH2 and Ti6Al4V powder into the container according to the measured weight. iii. Ethyl alcohol is added to the container to ensure more effective mixing of the components. and stirred manually for 5 minutes, iv. Then, ultrasonic probe equipment is inserted into the additive mixture. by immersing the additive in the paste for 30-90 seconds. The dispersion of the filler alloy, which is in paste form and modified with additives, results in 5 to be done It includes the steps of the process.
7. A method of producing a filler alloy according to claim 6, and its characteristics are: i. Pure, 85-95% Ag-Cu by weight, supplied in paste form. In-Ti alloy system or 85-95% by weight Ag-Cu alloy system, 10 placed in a clean container, ii. 5-10% by weight of TiH2 and 5-10% by weight of Ti6Al4V powder into the container spilling, iii. Ethyl alcohol is added to the container to ensure more effective mixing of the components. and mechanically mixing the mixture for 5 minutes, 15 iv. Then, ultrasonic probe equipment is inserted into the additive mixture. by immersing the additive in the paste for 30-90 seconds. Obtaining a paste-like filler alloy by dispersion to be done It includes the steps of the process. 20 8. A method of producing a filler alloy according to claim 7, and its characteristics are: i. Pure, 90% by weight Ag-Cu-In- supplied in paste form. A clean Ti alloy system or a 90% by weight Ag-Cu alloy system. placed inside the container, ii. Add 5% by weight TiH2 and 5% by weight Ti6Al4V powder to the container 25 spilling, iii. Ethyl alcohol is added to the container to ensure more effective mixing of the components. and mechanically stirring the mixture for 5 minutes, iv. Then, ultrasonic probe equipment is inserted into the additive mixture. 30 seconds by immersing the additive in the paste. Obtaining a paste-like filler alloy by dispersion to be done It includes the steps of the process. 16 9. A method for producing a filler alloy according to any of claims 6-8. The feature is that in the aforementioned step (iii), 10 is added for every 50 grams of paste. The addition of a few drops of ethyl alcohol.
10. Used in vacuum brazing of Ti6Al4V alloy with SiO₂(f) / SiO₂ composite. The application method of the filled alloy is its characteristic, 5 i. Ag-Cu-In-Ti alloy in paste form or Ag-Cu alloy Ti6Al4V- Addition of TiH2 powder mixture, ii. Adding ethyl alcohol to the paste and powder mixture and into the mixture by mixing the powders by immersion in an ultrasonic probe device. Obtaining a modified paste mixture by dispersing, 10 iii. the SiO2(f) / SiO2 composite and Ti6Al4V alloy forming the pair of combinations, sanding with sandpaper, iv. After grinding of SiO2(f) / SiO2 composite and Ti6Al4V alloy Immersion in 99.95% pure ethyl alcohol and ultrasonic method cleaning, 15 v. SiO2(f) / SiO2 composite and Ti6Al4V alloy in a drying oven. drying, vi. Modified paste obtained in step (ii) the mixture of dried SiO2(f) / SiO2 composite with the help of a brush application to the surface, 20 vii. The surface of the Ti6Al4V alloy, in processing step (vi) modified paste mixture applied to SiO2(f) / SiO2 composite Obtaining the combination pair by placing it on the surface, viii. The resulting pair of components is subjected to heat treatment in a brazing furnace. release 25 It includes the steps of the process.
11. It is an implementation method according to claim 10, and its characteristic is: i. Ag-Cu-In-Ti alloy or Ag-Cu alloy in paste form by weight Addition of 5-15% Ti6Al4V-TiH2 powder mixture, ii. Add 10 drops of ethyl alcohol to 50 grams of paste and powder mixture and 30 The ultrasonic probe device is immersed in the mixture for 30-60 seconds. paste modified by mixing and dispersing the powders obtaining the mixture, 17 iii. the SiO2(f) / SiO2 composite and Ti6Al4V alloy forming the pair of combinations, sanding with sandpaper, iv. Alcohol treatment of SiO2(f) / SiO2 composite and Ti6Al4V alloy after grinding. immersion in it and cleaning with an ultrasonic method, v. SiO2(f) / SiO2 composite and Ti6Al4V alloy at 80-100 °C 5 Drying in a drying oven for 90-120 minutes, vi. Modified paste obtained in step (ii) the mixture of dried SiO2(f) / SiO2 composite with the help of a brush application to the surface, vii. Ti6Al4V alloy, 10 on its surface in processing step (vi). modified paste mixture applied to SiO2(f) / SiO2 composite Obtaining the combination pair by placing it on the surface, viii. The resulting pair of components is brazed in a brazing furnace at 800-825 °C. exposed to heat treatment at degrees for 15-45 minutes It includes the steps of the process. 15 12. It is an implementation method according to claim 10, and its characteristic is: i. a paste-like substance containing 85-95% by weight of Ag-Cu-In-Ti alloy or by weight 85-95% Ag-Cu alloy with 5-15% by weight Ti6Al4V-TiH2 powder mixture addition, ii. Adding ethyl alcohol to the paste and powder mixture and adding 20 to the mixture The ultrasonic probe device is used to mix the powders by immersing them for 90 seconds. Obtaining a modified paste mixture by dispersing it, iii. the SiO2(f) / SiO2 composite and Ti6Al4V alloy forming the pair of combinations, sanding with sandpaper, iv. Alcohol 25 after grinding of SiO2(f) / SiO2 composite and Ti6Al4V alloy. immersion in it and cleaning with an ultrasonic method, v. SiO2(f) / SiO2 composite and Ti6Al4V alloy at 80-100 °C Drying in a drying oven for 90-120 minutes, vi. Modified paste obtained in step (ii) 30 of the mixture dried with the help of a brush SiO2(f) / SiO2 composite application to the surface, 18 vii. The surface of the Ti6Al4V alloy, in processing step (vi) modified paste mixture applied to SiO2(f) / SiO2 composite Obtaining the combination pair by placing it on the surface, viii. The resulting pair of components is brazed in a brazing furnace at 800-825 °C. heat treatment at degrees for 15-45 minutes 5 It includes the steps of the process. 15
