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Certifications for 2618/2618A aircraft aluminium rod
Standard for 2618/2618A aircraft aluminium rod
DTD 5014 2618-T6511 bar
DTD 5014A 2618-T6511 bar
Production request for 2618/2618A aircraft aluminium rod
To produce 2618/2618A aluminum rods, the following requirements and processes may apply.
Raw material: The production process begins with the selection and preparation of high-quality raw materials, including aluminum alloy ingots that meet the chemical composition and purity requirements of the 2618/2618A alloy.
Heating and melting: The aluminum alloy ingots are heated and melted in a furnace to the appropriate temperature and viscosity for the chosen production method, such as extrusion, forging, or rolling.
Forming: The molten aluminum is then shaped into the desired rod form using the chosen forming method, which may involve extruding the aluminum through a die, forging it under high pressure, or rolling it into the desired thickness.
Heat treatment: After forming, the 2618/2618A aluminum rod may be heat-treated to achieve the desired mechanical properties and temper, such as T6 or T6511. The heat treatment involves controlled heating and cooling of the aluminum to alter its microstructure and improve its strength and ductility.
Finishing: once the rods have been formed and heat-treated, they may undergo additional finishing processes to improve their surface finish, dimensional accuracy, and other properties. This may include machining, grinding, or polishing.
Quality control: throughout the production process, the aluminum rods must undergo rigorous quality control measures to ensure they meet the required standards and specifications. This may involve non-destructive testing, dimensional inspection, and other quality assurance processes.
The specific production requirements for 2618 aluminum rods will depend on the chosen production method, intended use, and other factors. It's important to work with a reputable aluminum supplier or manufacturer who has experience producing high-quality aluminum rods and can provide guidance on the appropriate production processes for your needs.
2618/2618A aircraft aluminium rod size
Outer diameter: Φ166, Φ220, Φ380, Φ396, Φ448, Φ462, Φ566, Φ582, Φ915, Φ1060, Φ1220, Φ1320, etc.
Length: less than 7500mm
2618/2618A aircraft aluminium rod characteristics
2618/2618A aviation aluminum bar is a high performance aluminum alloy material with the following characteristics.
High strength: 2618/2618A aviation aluminum bar has very high tensile strength and yield strength, which can withstand high stress and heavy load.
Good workability: 2618/2618A aviation aluminum bar has good workability, including plasticity and malleability, and is easy to be processed into various shapes during the manufacturing process.
Good corrosion resistance: 2618/2618A aviation aluminum bar exhibits good oxidation and corrosion resistance, suitable for use in harsh environments.
Good heat treatability: 2618/2618A aviation aluminum bar can be heat treated to change its organization and mechanical properties, and its properties can be customized when needed.
Light weight: compared with other commonly used metal materials, 2618/2618A aviation aluminum bar has low density and good specific strength and specific stiffness, which is ideal for manufacturing lightweight structural parts.
Widely used: 2618/2618A aviation aluminum rods are widely used in aviation, aerospace and other fields, and can be used in the manufacture of aircraft, rockets, etc.
To sum up, 2618 aviation aluminum bar has high strength, good machinability, corrosion resistance, heat treatment and light weight, etc. It is a high performance aluminum alloy material for various important industrial and aerospace applications.
2618/2618A aircraft aluminium rod chemical composition
|2618 aluminium rod chemical composition|
2618/2618A aircraft aluminium rod mechanical properties
|Tensile Strength||372 MPa|
|Tensile Strength, Ultimate||441 Mpa|
|Shear Strength||262 Mpa|
|Fatigue Strength (completely reversed stress; RR Moore machine/specimen)||124 Mpa|
|Elastic Modulus (AA; Typical; Average of tension and compression)||74.5 Gpa|
|Elongation at Break||10% at -28.0 °C|
|14% at 149 °C|
|50% at 260 °C|
2618/2618A aircraft aluminium rod application
2618 aerospace aluminum bar is a high performance aluminum alloy material that has a wide range of applications in the aviation field due to its high strength, good machinability, and light weight. The following are some examples of 2618 aviation aluminum bar in aviation applications.
Aircraft structural parts: 2618 aviation aluminum rods can be used to manufacture various aircraft structural parts, such as aircraft fuselage, wings, tail, etc.. These structural parts need to have good strength and stiffness, but at the same time to be lightweight, in order to reduce the overall weight of the aircraft, improve fuel efficiency and flight performance. 2618 aviation aluminum bar can meet these requirements.
Engine parts: 2618 aerospace aluminum rods can also be used to manufacture various parts of aircraft engines, such as cylinder blocks, pistons, valves, etc.. Aero engines need to have stability and corrosion resistance under high temperature and pressure, and 2618 aviation aluminum bar can improve these properties through appropriate heat treatment and surface treatment.
Aerospace: 2618 aviation aluminum bar can also be used to manufacture various structural parts and components of aerospace vehicles, such as rocket blocks, satellite parts, etc.. These devices need to have high strength and vibration resistance, and the high strength and good processing performance of 2618 aviation aluminum bar can meet these requirements.
In short, 2618 aviation aluminum bar has a wide range of uses in aviation applications, and can be used to manufacture a variety of structural parts, engine parts and aerospace parts, making an important contribution to the development of the aviation industry.