Classification, application and factors affecting tensile force of titanium alloy wire?

The difference between titanium powder and titanium dioxide is as follows:

1. Titanium powder is powdered metallic titanium, while titanium dioxide is powdered titanium dioxide;

2. Titanium powder can be ignited in the air, while titanium dioxide is mainly used in decoration and coating industries;

3. Titanium powder has a large gas-absorbing capacity, with a purity of about 95%. The molecular formula of titanium dioxide is TiO2, which is a polycrystalline compound with regular arrangement of particles and a lattice structure.

Therefore, the characteristics of titanium powder and titanium dioxide are completely different.
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Hot working properties and industrial application of TC4 titanium alloy

The pressure processing of titanium alloy is more similar to the processing of steel than the processing of non-ferrous metals and alloys. Many process parameters of titanium alloy during forging, volume stamping and plate stamping are close to those of steel processing. But there are also some important features that must be paid attention to when pressure working on Qin and Qin alloys.

Although it is generally believed that the hexagonal lattice contained in titanium and titanium alloys has low plasticity during deformation, various pressure processing methods used for other structural metals are also suitable for titanium alloys. The ratio of yield point to strength limit refers to one of the characteristic indexes of whether a metal can withstand plastic deformation. The larger the ratio, the worse the plasticity of the metal. For industrial pure titanium in a cooling state, the ratio is 0.72-0.87, while carbon steel is 0.6-0.65, and stainless steel is 0.4-0.5.

Perform volume stamping, free forging and other operations related to the processing of large cross-section and large-size blanks in the heated state (above the =yS transition temperature). The heating temperature range of forging and pressing is between 850-1150°C. Alloys BT; M) 0, BT1-0, OT4~0 and OT4-1 have satisfactory plastic deformation in the cooling state. Therefore, most of the parts made of these alloys are stamped from blanks that have undergone intermediate annealing without heating. When the titanium alloy is cold plastically deformed, regardless of its chemical composition and mechanical properties, the strength will be greatly improved, and the plasticity will be correspondingly reduced. For this reason, it is necessary to perform an annealing treatment between procedures.

The blade groove wear that occurs during titanium alloy processing is the local wear along the cutting depth direction of the back and the front, and it is often caused by the hardened layer left by the previous processing. The chemical reaction and diffusion of the tool and the workpiece material at a processing temperature of more than 800°C are also one of the reasons for the formation of groove wear. Because during the machining process, the titanium molecules of the workpiece accumulate in the front area of ​​the blade and are "welded" to the blade under high pressure and high temperature, forming a built-up edge. When the built-up edge is peeled from the blade, the carbide coating of the blade is taken away.

Due to the heat resistance of titanium, cooling is very important in the machining process. The purpose of cooling is to keep the blade and tool surface from overheating. Using end coolant, in this way, when performing square shoulder milling and face milling of dimples, cavities or full grooves, a good chip removal effect can be achieved. When cutting titanium metal, the chips are easy to stick to the cutting edge, causing the next round of milling cutter rotation to cut the chips again, which often causes the edge line to collapse. Each type of blade cavity has its own coolant hole/injection to solve this problem and strengthen the constant blade performance. Another clever solution is a threaded cooling hole. Long-edge milling cutters have many blades. Applying coolant to each hole requires a high pump capacity and pressure. However, it is different. It can block unnecessary holes according to needs, thereby maximizing the flow of liquid to the holes that need it.
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Technical treatment method for TC11 titanium rod/titanium alloy rod low-magnification white bright block

Titanium alloy parts have the characteristics of low density and good corrosion resistance, so they have become more ideal structural materials for aerospace engineering; however, there are also many factors that affect its machinability at the same time; this is because of the metallurgical properties of titanium alloys And material properties may have a serious impact on the cutting action and the material itself.

The clamping principle of titanium alloy parts is the key technology for titanium alloy manufacturers to process titanium alloys, as follows:

(1) The clamping force in the rough machining stage should be large to prevent the parts from loosening during the high cutting force machining process; the clamping force should be small in the finishing machining stage to prevent clamping deformation.

(2) The clamping force is applied to the place with good rigidity, and the force point should be as many as possible.

(3) Appropriate auxiliary devices should be added for thin-walled structural parts with poor rigidity to increase the rigidity of the entire processing technology system.
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Application and performance of GR5 medical titanium alloy

The internal shortcomings of titanium alloy pipe welds, lack of penetration, refers to a defect in which the workpiece and the weld metal or the part between the weld layers are not fused. Incomplete penetration weakens the welding section of the weld, causing severe stress concentration, greatly reducing the strength of the joint, and it often becomes the source of weld cracking. There is non-metallic slag in the slag inclusion weld, which is called slag inclusion. The slag inclusion reduces the working section of the weld, and constitutes a stress concentration, which will reduce the strength and impact toughness of the weld.

Usually according to the mechanism of crack occurrence, it can be divided into two types: hot crack and cold crack. Thermal cracks occur during the crystallization process from liquid to solid in the weld metal, and most of them occur in the weld metal. The main reason for its occurrence is the presence of low melting point substances (such as FeS, melting point 1193°C) in the weld, which weakens the contact between the grains. When subjected to greater welding stress effects, it simply causes cracks between the grains. . When the weldment and electrode contain a lot of impurities such as S and Cu, thermal cracking simply occurs.

Thermal cracks have the characteristic of spreading along the grain boundary. When the crack penetrates the surface and communicates with the outside, it has a significant hydrogenation tendency. Cold cracks occur during the cooling process after welding, mostly on the base metal or the fusion line between the base metal and the weld. The primary reason for this is that the heat-affected zone or the welding seam constitutes a quenching arrangement. Under the effect of high stress, it causes cracks in the grains. When welding easy-quenchable titanium alloys with higher carbon content or more alloying elements , The most prone to cold cracks. Too much hydrogen melted into the weld can also cause cold cracks.

Cracks are one of the most risky shortcomings. In addition to reducing the load-bearing section, severe stress accumulation will occur. The cracks will gradually expand during use and eventually cause damage to the components. Therefore, such shortcomings are usually not allowed in the welding layout.

When the pore weld metal absorbs too much gas (such as H2) or the gas (such as CO) generated by the metallurgical reaction in the molten pool at high temperature, it is too late to be discharged when the molten pool is cooled and condensed, and it is formed inside or on the outside of the weld. Holes are pores. The existence of pores reduces the useful working section of the weld and reduces the mechanical strength of the joint. If there are penetrating or continuous pores, it will severely affect the tightness of the weldment. During or after welding, cracks in the metal part of the welded joint area are called cracks. Cracks can occur in the weld, and can also occur in the heat-affected zone on both sides of the weld. Sometimes it occurs on the outside of the metal, and sometimes inside the metal.
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Application of titanium and titanium alloys in aviation

The tensile modulus of industrial pure titanium is 105-109 Gpa, and the tensile modulus of most titanium alloys in the annealed state is 110-120 Gpa. The age-hardened titanium alloy has a slightly higher tensile elastic modulus than in the annealed state, and the compressive elastic modulus is equal to or greater than the tensile elastic modulus. Although the strength of titanium and titanium alloys is much higher than that of aluminum and aluminum alloys, they are only 55% of the stiffness. The specific elastic modulus of titanium alloy is equal to that of aluminum alloy, second only to beryllium, molybdenum and some high-temperature alloys. The torsion or shear modulus of industrial pure titanium is 46 Gpa, and the shear modulus of titanium alloy is 43-51 Gpa.
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Characteristics of TA1, TC4, TC11 titanium rods and titanium alloy rods and heat treatment process

TC4 titanium alloy is also called Ti-6Al-4V, this type of alloy contains 6% Al and 4% V. TC4 is widely used in titanium alloys. Al is an element that improves the stability of the phase, and V is an element that improves the stability of the β phase. After adding aluminum to pure titanium, aluminum has sufficient solubility in a-Ti. Aluminum is widely distributed in nature, easy to prepare, and relatively cheap. Aluminum is much lighter than titanium. Adding aluminum to titanium reduces the density and increases the specific strength. More importantly, while the alloy maintains sufficient plasticity, aluminum can be effectively solid-solution strengthened. Aluminum can effectively strengthen the phase not only at room temperature but also at high temperature, and improve the thermal strength and working temperature of the titanium alloy. TC4 with 6% aluminum can work for a long time at 400℃ and maintain high strength. However, only aluminum-containing titanium aluminum alloy (Ti-4Al) will become brittle after long-term heating at 550°C. Therefore, adding an appropriate amount of β-type stabilizing element X to the titanium aluminum alloy will hinder the formation of brittleness, and contains a certain amount of β phase, which improves the hot workability of the alloy and the plasticity of the alloy, and it can also be heat treated ( Such as solid-solution + aging to further improve the strength). The structure of TC4 deformed and annealed is a+β coexistence. The content of the β phase in TC4 is relatively small, accounting for about 10%. TC4 alloy has good overall mechanical properties after being kept at 750~800℃ for 1-2h and then air-cooled (recrystallization annealing). The structure of the alloy at this time is an equiaxed a+β phase.

TC4 titanium alloy can usually be solid-solution + aging strengthening heat treatment, such as heating at 913~940℃ for 1h, water quenching +523~550℃ for 3~4h, after air cooling, the strength can be increased by 20%~25%, but the plasticity is slightly declined. However, the current domestic TC4 is mainly used in the annealed state, and it is rarely used in the strengthened heat treatment state. The high-temperature strength of TC4 is greatly improved due to the addition of aluminum.
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Analysis of application requirements of titanium and titanium alloy materials in civil, aerospace and manufacturing industries

Target application:

The phenomenon that energetic particles (such as argon ions) bombard the solid surface, causing various particles on the surface, such as atoms, molecules or clusters, to escape from the surface of the object is called "sputtering." In magnetron sputtering coating, the positive ions generated by argon ionization are usually used to bombard the solid (target), and the sputtered neutral atoms are deposited on the substrate (workpiece) to form a film. The magnetron sputtering coating has a " Two characteristics: low temperature and fast speed.

Principle of magnetron sputtering:

Add an orthogonal magnetic field and electric field between the sputtered target (cathode) and the anode, and fill the required inert gas (usually Ar gas) in the high vacuum chamber. The permanent magnet forms 250-350 on the surface of the target material The Gaussian magnetic field forms an orthogonal electromagnetic field with the high-voltage electric field.

Under the action of an electric field, Ar gas ionizes into positive ions and electrons, and a certain negative high voltage is applied to the target. The electrons emitted from the target are affected by the magnetic field and the ionization probability of the working gas increases. A high-density plasma is formed near the cathode, and Ar ions are accelerated to the target surface under the action of the Lorentz force, and bombard the target surface at a high speed, so that the atoms sputtered out of the target follow the principle of momentum conversion. The high kinetic energy departs from the target surface and flies toward the substrate to deposit a film.

Magnetron sputtering is generally divided into two types: DC sputtering and radio frequency sputtering. Among them, the principle of DC sputtering equipment is simple, and its rate is also fast when sputtering metal. The application range of radio frequency sputtering is more extensive. In addition to sputtering conductive materials, non-conductive materials can also be sputtered. At the same time, reactive sputtering can be used to prepare compound materials such as oxides, nitrides, and carbides. If the frequency of radio frequency increases, it becomes microwave plasma sputtering. Nowadays, electron cyclotron resonance (ECR) type microwave plasma sputtering is commonly used.
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