The difference between tungsten carbide-like wear-resistant welding wire and tungsten carbide

Tungsten carbide-like wire, is an inexpensive alternative to tungsten carbide alloys, with the same wear resistance as tungsten carbide alloys. The density of the tungsten carbide-like welding wire is low, and the density of the tungsten carbide alloy is high, and the wear-resistant layer of the same area and size will be used for surfacing. Material costs. At present, only Beijing Guben Technology Co., Ltd. develops and produces tungsten carbide series welding wires in China. Let’s take a look at the difference between tungsten carbide-like welding wire and tungsten carbide alloy.

1. Metallographic organization

Tungsten carbide alloy is a soft matrix that wraps large, unevenly distributed tungsten carbide particles. In actual use, the soft matrix on the surface of tungsten carbide alloy will wear out quickly, and the combination of tungsten carbide particles and the matrix will loosen, which will easily lead to tungsten carbide particles falling off and affect the overall working life of the wear-resistant layer.

Tungsten carbide-like welding wire is distributed on a solid base with a large number of fine and uniformly dispersed special carbides. Since the tungsten carbide-like is dispersed in the matrix finely and evenly, the bonding performance between the carbide particles and the matrix is ​​good, and the phenomenon of loosening and falling off will not occur, and finally the ideal wear resistance effect is obtained.

2. Number of surfacing layers

Generally, tungsten carbide alloy can only be surfacing with one layer, while tungsten carbide-like welding wire can be used for multi-layer surfacing. The multi-layer surfacing can obtain a thicker wear-resistant layer, so that the tungsten carbide-like welding wire has a longer working life than the tungsten carbide alloy, and is more suitable for severe wear conditions.

3. Welding process

The oxyacetylene welding process is used for tungsten carbide alloy, the welding position is limited, the welding speed is slow, and the welding efficiency is low. Tungsten carbide-like welding wire uses a gas shielded welding process, which can be welded in various positions, semi-automatic welding, fast speed and high efficiency.

Matters needing attention in titanium alloy processing

Pressure machining of titanium alloys is more similar to steel machining than to non-ferrous metals and alloys. Many process parameters of titanium alloys in forging, volume stamping and sheet stamping are close to those in steel processing. But there are some important features that must be paid attention to when press working Chin and Chin alloys.

Although it is generally believed that the hexagonal lattices contained in titanium and titanium alloys are less ductile when deformed, various press working methods used for other structural metals are also suitable for titanium alloys. The ratio of yield point to strength limit is one of the characteristic indicators of whether the metal can withstand plastic deformation. The larger this ratio, the worse the plasticity of the metal. For industrially pure titanium in the cooled state, the ratio is 0.72-0.87, compared to 0.6-0.65 for carbon steel and 0.4-0.5 for stainless steel.
Carry out 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 temperature range of forging and stamping heating 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, the parts made of these alloys are mostly made of intermediate annealed blanks without heating and stamping. 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, annealing treatment between processes must be performed.

The wear of the insert groove in the machining of titanium alloys is the local wear of the back and front in the direction of the depth of cut, which 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 of the blade and are “welded” to the blade edge under high pressure and high temperature, forming a built-up edge. When the built-up edge peels off the cutting edge, the carbide coating of the insert is taken away.

Due to the heat resistance of titanium, cooling is crucial in the machining process. The purpose of cooling is to keep the cutting edge and tool surface from overheating. Use end coolant for excellent chip evacuation when shoulder milling and face milling of pockets, pockets or full grooves. When cutting titanium metal, the chips are easy to stick to the cutting edge, causing the next round of milling cutter to cut the chips again, often causing the edge line to chip. Each insert cavity has its own coolant hole/injection to address this issue and enhance constant edge performance. Another neat solution is threaded cooling holes. Long edge milling cutters have many inserts. Applying coolant to each hole requires a high pump capacity and pressure. On the other hand, it can block unwanted holes as needed, thereby maximizing flow to the holes that are needed.

Orders from Thailand customers are being prepared

This is our second cooperation with a Thailand customer. The customer expressed that the first cooperation was very satisfied with our product quality and service, and hoped for long-term cooperation in the future!

Orders from Thailand customers are being prepared

这是我们与泰国客户的第二次合作。客户表示第一次合作对我们的产品质量和服务非常满意,希望以后能长期合作!

 

Customers from Indonesia have been successfully delivered

Product name: ASTM B338 Grade 2 seamless titanium tube
Destination: Indonesia
Specifications: 19.05*1.00*6000mm
Quantity: 2 tons

Dear friends, if you have the same needs, please contact us. Email:[email protected] Tel: +86-29-8950 6568

Hastelloy C22 Welded Tube order is ready for shipping

Through 30 days hard work, finally, we successfully delivered 2 pieces ∅239.6x8x4000mm welded Hastelloy C22 Tubes.

Standard: ASTM B626/B619, Grade: UNS N06022/C22.

They will be shipped by sea to our French customer. Hereby I am sharing some photos with you:

Tube Wall Thickness Measurement:

Thickness measuring

Tube OD Measurement:

Tube OD measurement

PMI TEST:

PMI TEST

Tube surface:

Tube surface

If you have RFQs for Incoloy 825, 800H/HT, Monel 400, Inconel 600, Inconel 601, Inconel 625, Inconel 718, Hastelloy C22, B2, X, G30, C276, welcome to contact us for quote!

Ti6Al4V ELI, UNS R56407, Grade 23

Ti-6Al-4V-ELI, UNS R56407, Grade 23 (ELI=Extra Low Interstitials)

INTRODUCTION
Ti-6Al-4V-ELI, Grade 23 alloy (Extra Low Interstitials, UNS R56407) is a higher purity grade of Ti-6Al-4V alloy. This grade has lower oxygen, carbon, and iron content. It is used in biomedical applications such as surgical instruments, orthopedic implants, and is the preferred grade for marine and cryogenic applications, and some important aerospace components.
This titanium grade is produced by vacuum arc primary melting followed by a second vacuum arc remelting operation.
SPECIFICATIONS
• AMS 4930 – Bar, Wire, Billet, and Rings (annealed)
• AMS 4931 – Bar, Billet, and Rings
• AMS 4996 – Billet
• ASTM F 136 – Surgical Implants
PHYSICAL PROPERTIES
Melting Range: 2,800-3,000°F (1,538 – 1,649°C)
Density: 0.160 lbs/cu. in.; 4.47 gm/cc
Beta Transus Temperature: 1,790°F (± 25°); 976.7°C (± 3.9°)
HEAT TREATMENT
Ti-6Al-4V-ELI, Grade 23 alloy is normally used in the annealed condition.
1. Anneal: 1,300 -1,350°F; (704.4 – 732.2°C), 1 to 8 hours, air cool
2. Stress Relieving: 900 -1,200°F; (482.2 – 648.9°C), 1 to 4 hours, air cool
HARDNESS
Typical hardness in the annealed condition is Rockwell C 30-34.
FORMABILITY
The formability of Ti-6Al-4V-ELI, Grade 23 alloy is better than standard grade Ti-6Al-4V alloy, although it is still difficult to form at room temperature in the annealed condition. Severe forming operations such as bending or stretching can be performed on annealed material at temperatures up to 1,200°F; (648.9°C) without affecting mechanical properties. Hot sizing or shaping
can be done by creep forming in the 1,000 -1,200°F; (537.8 – 648.9°C) temperature range.
FORGEABILITY
Ti-6Al-4V-ELI, Grade 23 alloy is finish-forged from 1,750°F; (954.4°C) with a finishing temperature of 1,450°F; (787.8°C). Minimum reductions of 35% are recommended to obtain optimum properties.
MACHINABILITY
Ti-6Al-4V-ELI, Grade 23 alloy can be machined using practices for austenitic stainless steels using slow speeds, heavy feeds, ridgid tooling, and large amounts of non-chlorinated cutting fluid.
WELDABILITY
Ti-6Al-4V-ELI, Grade 23 alloy is easily welded in the annealed condition. Precautions must be taken to prevent oxygen, nitrogen, and hydrogen contamination. Fusion welding can be done in inert
gas-filled chambers or using inert gas welding of the molten metal and the adjacent heated zones using a trailing shield. Spot, seam, and flash welding can be performed without resorting to protective atmospheres.
Properties of Ti-6Al-4V-ELI, Grade 23 alloy welds such as ductility, impact strength, and fracture toughness are significantly better than welds of standard grade Ti-6Al-4V alloy.
SPECIAL PRECAUTIONS
Ti-6Al-4V-ELI, Grade 23 alloy can be subject to hydrogen contamination during improper pickling and by oxygen, nitrogen, and carbon pickup during forging, heat treating, brazing, etc. This contamination results in a deterioration in ductility which could adversely affect notch sensitivity and forming characteristics.

Order of Alloy 718 Round Bar

The coronavirus and its mutated virus are still spreading all over the world, the global situation is getting worse…We all are facing multiple pressures and risks…

But during this very hard time, our one of our happy Russian customer has placed us 1,750Kgs Alloy 718/UNS N07718/Inconel 718 round bar order.

Through our hard work and effort, finally, they have been finished and ready for shipping, here is a photo for your reference:

If you have Pipe, Tube, Plate, Sheet, and Bar RFQs for Inconel 600/601/617/625/718, Monel 400, Nickel 200/201, Hastelloy C22/C276/2000/B22, welcome to contact us for quotes!

Order of ASTM B111 Aluminum Bronze Tubes

Through a couple of weeks of effort, we are ready to deliver the ASTM B111 UNS C61300 Aluminum Bronze Tubes to our Italian Customer.

They will be used for heat exchangers, the dimension is: OD 10MM x WT 0.89MM x Length 1,500MM.

We also can produce UNS C11000, UNS C44300, UNS C68700, UNS C70600, UNS C71500.

If you have such RFQs, welcome to contact us via [email protected] or WhatsApp:+86 177 7897 6690

Order of ASME SB265 Gr.2 Titanium Plate

Finally, we successfully delivered the precious metal sheet to our Saudi Arabia customer. They will be used for manufacturing the Pressure Vessels for the Petrochemical plant.

Standard: ASME SB265, ASME SECTION II Part B

Grade: 2

Dimensions:

3x1000x1000mm

10x2000x2500mm

12x1600x3000mm

20x1000x1200mm