7050 Aluminium Alloy Powder

Översikt över 7050 aluminiumlegering pulver

7050 aluminium alloy powder is a strong, tough, heat-treatable alloy powder that has high strength properties combined with excellent fatigue resistance. It is part of the 7xxx series of aluminium alloys, with zinc being the primary alloying element.

7050 alloy powder offers a high strength-to-weight ratio and is commonly used in structural and high-stress applications in the aerospace, automotive, and defence industries. Parts made from 7050 powder metallurgy techniques can replace components traditionally made of steel, titanium or nickel alloys.

Some key properties and characteristics of 7050 aluminium alloy powder include:

7050 Aluminium Alloy Powder Properties

The high zinc and copper content in 7050 powder enables heat treatment to achieve very high yield and tensile strengths while also providing good fatigue resistance compared to other aerospace aluminium alloys.

The following sections provide more details on the composition, processing methods, properties, applications, specifications, pricing, advantages and limitations of 7050 aluminium alloy powder.

Composition of 7050 aluminium alloy powder

The 7050 aluminium alloy consists of the following typical elemental composition:

7050 Aluminium Alloy Composition

The high levels of zinc enable precipitation hardening heat treatments to achieve very high strength. Magnesium and copper add to the age hardening effects with zinc.

Zirconium is added for grain structure control. Iron, silicon, manganese, chromium and titanium are present as impurity elements with small individual limits.

7050 aluminiumlegering pulver Bearbetning

7050 aluminium alloy powder can be manufactured into fully-dense powder metallurgy components using techniques like:

• Het isostatisk pressning (HIP)
• Direct hot extrusion
• Formsprutning av metall

HIP involves encapsulating the powder in a container and applying heat and very high isostatic pressures in special vessels to consolidate the powder. This avoids prior compaction steps and achieves uniform properties and net shape or near-net shape parts.

Direct hot extrusion involves compacting powder into billets and then forcing it through a die to produce long profiles or rods. The high pressure and heat bond the particles during deformation into a fully dense product.

Metal injection molding allows shaping more complex net or near-net shape parts from powder using specialized tooling. The powder-binder mixture known as feedstock is injected into molds and then subjected to debinding and sintering.

The 7050 aluminium alloy powder itself is atomized from molten alloys into fine spherical powders around 10 – 45 microns diameter using inert gas atomization or water atomization processes. The purity, particle size distribution, morphology and surface oxide content is carefully controlled to enable full density during consolidation.

7050 aluminium alloy powder Properties

The properties of parts made from 7050 aluminium alloy powder can be tailored by varying processing parameters. Some typical properties after heat treatment are:

7050 Aluminium Alloy Powder Properties

The T6 temper involves solution heat treatment followed by artificial aging to achieve peak strength. T7 conditioning applies an overaging treatment after T6 to provide improved stress corrosion cracking resistance at slightly reduced strength levels.

7050 alloy powder has low density combined with high strength levels leading to excellent specific strength properties. The thermal and electrical conductivity is moderate for an aluminium alloy. Corrosion resistance is poorer than pure aluminium but acceptable in most environments.

Fatigue strength in particular is outstanding for aerospace aluminium alloys, while machinability and weldability is inferior to more formable alloys like 6061 due to the high zinc levels.

7050 aluminium alloy powder Applications

The combination of properties makes 7050 aluminium alloy powder suitable for:

Applications of 7050 Aluminium Alloy Powder

For aerospace use, 7050 is second in use only to 7075 aluminium alloy for strength-critical airframe components requiring durability. HIP processed parts tend to replace forgings and billet-based parts.

Automotive and defence applications take advantage of lightweighting and performance over more conventional aluminium or magnesium alloys, with improved mechanical properties over composites.

7050 aluminium alloy powder Specifications

7050 alloy powder and consolidated products meet various specifications that define the composition limits, processing methods, properties and quality requirements for aerospace and defence applications:

7050 Aluminium Alloy Powder Specifications

Specifications cover powder size distribution, shape and flow characteristics, impurity limits, typical density and mechanical properties in different heat treatment conditions, sampling procedures, testing methods, inspection criteria and documentation requirements.

7050 aluminium alloy powder Suppliers

Some leading global suppliers of 7050 aluminium alloy powders include:

7050 Aluminium Alloy Powder Suppliers

These companies offer gas- or water-atomized 7050 aluminium alloy powders customized for additive manufacturing or metal injection molding feedstock applications with specialized particle size distributions and shapes.

In addition, major metal powder producers and consolidators have extensive experience working with 7050 alloy systems optimized for hot isostatic pressing to aerospace component specifications.

7050 aluminium alloy powder Cost

7050 aluminium alloy powder prices depend significantly on:

• Purity / Impurity levels
• Particles size distribution
• Morphology and shape
• Inköpskvantitet
• Additional processing like sieving

Indicative pricing for gas-atomized spherical 7050 powder suitable for additive manufacturing is around $50 – $65 per kg. Prices are higher for tighter distributions needed for MIM feedstocks or hot isostatic pressing.

7050 aluminium alloy powder Pros and Cons

Advantages of 7050 Aluminium Alloy Powder

• Highest strength 7xxx series alloy
• Excellent fatigue performance
• Låg densitet
• Used extensively in aerospace industry
• Replaces steels and titanium alloys
• Parts can be complex, monolithic shapes

Begränsningar av 7050 Aluminium Alloy Powder

• Måttlig korrosionsbeständighet
• Weldability issues
• Lower thermal / electrical conductivity
• Cost is higher than normal extrusion alloys
• Processing has more controls and qualifications

For many critical structural parts needed in performance applications, 7050 delivers the vital combination of strength, damage tolerance and low weight. Despite some fabrication and corrosion drawbacks, the capabilities offset the slightly higher powder cost where weight savings matter.

Vanliga frågor

Frequently Asked Questions on 7050 Aluminium Alloy Powder

Q: What is 7050 aluminium alloy?

A: 7050 is a very high strength 7xxx series aluminium alloy containing major additions of zinc, magnesium and copper plus trace additions like zirconium. It is age-hardenable to achieve an exceptional combination of tensile properties and fatigue resistance.

Q: Is 7050 stronger than 7075?

A: Yes, 7050 aluminium alloy has slightly higher ultimate tensile and yield strengths than the very popular 7075 alloy in peak-aged tempers, along with superior fatigue strength. It matches the corrosion resistance of 7075.

Q: What are some uses of 7050 aluminium?

A: Key uses are aircraft structural parts like wing skins, fittings and pylons, helicopter rotor components like spindles, automotive chassis and suspension parts, applications like armour, space booms, lifting equipment, and sporting goods like golf clubheads and bicycle rims.

Q: What processing methods can make 7050 alloy parts?

A: While traditional wrought processes like extrusion and forging can make 7050 products, powder metallurgy techniques are growing rapidly including hot isostatic pressing (HIP), direct hot extrusion and metal injection molding (MIM) to exploit the alloy’s strengths.

Q: Is 7050 aluminium weldable?

A: No, welding of 7050 alloy is very difficult compared to medium or lower strength alloys due to cracking issues cause by its high zinc and copper content. Mechanical fastening or adhesive bonding are alternate joining methods recommended.

Q: What replaces 7050 aluminium alloys?

A: For the highest strength requirements where fatigue life is less critical, very high strength aerospace aluminium alloys like C465 or 7085 are being evaluated to replace certain applications of 7050 alloy. Composites and advanced metal alloys are also competing solutions.

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