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| Categories | Nickel Alloy Fasteners |
|---|---|
| Brand Name: | HT |
| Model Number: | Incoloy25-6Mo Inconel 926 DIN 1.4529 UNS N08926 Alloy 926 Nickel Alloy Fasteners |
| Certification: | ISO9001 |
| Place of Origin: | China |
| MOQ: | 1 pcs |
| Price: | USD 1000/piece |
| Payment Terms: | L/C,T/T, Western Union |
| Supply Ability: | 1000 pcs per month |
| Delivery Time: | 30-35 working days |
| Packaging Details: | wooden case, wooden pallet |
| Product Type: | bolt nut washer |
| Name: | Incoloy25-6Mo Inconel 926 DIN 1.4529 UNS N08926 Alloy 926 Nickel Alloy Fasteners |
| Size: | M6-M100 |
| Finish: | Cold galvanizing, Hot-dip Galvanizing, PTFE, Zinc Nickel, Black coating, Plain |
| Standard: | DIN931 DIN933 DIN912 DIN934 DIN125 DIN127 |
| Material: | Nickel alloy/stainless steel/duplex stainless |
Incoloy25-6Mo Inconel 926 DIN 1.4529 UNS N08926 Alloy 926 Nickel Alloy Fasteners
Alloy 926 is a super-austenitic molybdenum stainless steel that exhibits excellent resistance to a variety of highly corrosive environments. The combination of molybdenum and nitrogen in its composition resists pitting and crevice corrosion, while copper improves sulfuric acid resistance, and nitrogen improves yield and tensile strengths.
The following datasheet will provide more details about alloy 926.
The following table shows the chemical composition of alloy 926.
| Element | Content (%) |
|---|---|
| Iron, Fe | 41.69 - 50.35 |
| Nickel, Ni | 24-26 |
| Chromium, Cr | 19-21 |
| Molybdenum, Mo | 6-7 |
| Manganese, Mn | ≤2 |
| Copper, Cu | 0.5-1.5 |
| Silicon, Si | ≤0.5 |
| Nitrogen, N | 0.15-0.25 |
| Phosphorous, P | ≤0.03 |
| Carbon, C | ≤0.02 |
| Sulfur, S | ≤0.01 |
The physical properties of alloy 926 are outlined in the following table.
| Properties | Metric | Imperial |
|---|---|---|
| Density | 8.03 g/cm³ | 0.29 lb/in³ |
The mechanical properties of alloy 926 are outlined in the following table.
| Properties | Metric | Imperial |
|---|---|---|
| Tensile strength | ≥648 MPa | ≥94000 psi |
| Yield strength | ≥296 MPa | ≥43000 psi |
| Modulus of elasticity | 192 GPa | 27800 ksi |
| Elongation at break | ≥35 % | ≥35 % |
| Rockwell B hardness | ≤86 | ≤86 |
The following are some of the major applications of alloy 926:
2. Mechanical Properties
| Properties | Conditions | ||
| T (°C) | Treatment | ||
| Density (×1000 kg/m3) | 7.8 | 25 | |
| Poisson's Ratio | 0.27-0.30 | 25 | |
| Elastic Modulus (GPa) | 190-210 | 25 | |
| Tensile Strength (Mpa) | 515 | 25 | annealed (sheet, strip) more |
| Yield Strength (Mpa) | 275 | ||
| Elongation (%) | 40 | ||
| Reduction in Area (%) | |||
Thermal Properties
| Properties | Conditions | ||
| T (°C) | Treatment | ||
| Thermal Expansion (10-6/ºC) | 17.5 | 0-100 more | |
| Thermal Conductivity (W/m-K) | 16.2 | 100 more | |
| Specific Heat (J/kg-K) | 500 | 0-100 | |
Electric Properties
| Properties | Conditions | ||
| T (°C) | Treatment | ||
| Electric Resistivity (10-9W-m) | 690 | 25 | |
High temperature alloy refers to iron, nickel, cobalt as base, can
in the 600-1200 ℃ high temperature and must stress under the action
of a kind of metal materials long-term work; And it has higher
temperature strength, good resistance to oxidation and corrosion
resistance, good fatigue performance, the fracture toughness, and
other comprehensive performance. High temperature alloy for a
single austenitic organization, in all kinds of temperature has
good stability and reliability of the organizations use, based on
these properties, and high temperature alloy alloying degree is
higher, also called "super alloys", it is widely used in aviation,
spaceflight, petroleum, chemical industry, ships is a kind of
important material. According to the matrix element to points, high
temperature alloy and divided into iron base, nickel and cobalt
base, high temperature alloy etc. Iron base high temperature alloy
using temperature normally only up to 750 ~ 780 ℃, in the higher
temperature of the heat used parts, used the nickel and refractory
metal based
Characteristics:
1;High temperature alloy with high temperature strength.
2;Good resistance to oxidation and corrosion resistance
performance.
3;Good fatigue performance, the fracture toughness, plastic.
Organizational characteristics:
High temperature alloy for a single (austenitic) matrix
organization, in all kinds of temperature has good stability and
reliability of the organization to use.
High temperature alloy quality requirements:
External quality: external contour shape, size accuracy, the
surface defect cleaning method.
Internal quality: chemical composition, structure, mechanical and
physical and chemical properties.
Mechanical properties: room temperature and high temperature
tensile properties and impact toughness, high temperature lasting
several creep properties, hardness and high weeks and weeks, creep,
fatigue performance under the mutual action of fatigue and the
mechanical properties, thermal and corrosion resistance to
oxidation.
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