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AMS 5862 Stainless Steel: Composition, Properties, and Uses

Imagine a material that combines exceptional strength, impressive corrosion resistance, and remarkable versatility, all while maintaining a sleek, polished appearance. Enter AMS 5862 stainless steel, a marvel of modern metallurgy that has become a cornerstone in industries ranging from aerospace to power generation. Known for its unique chemical composition and impressive mechanical properties, this alloy offers a myriad of benefits that make it a top choice for engineers and designers alike.

In this article, we will delve into the intricate details of AMS 5862 stainless steel, exploring its precise chemical makeup and how each element contributes to its overall performance. We’ll examine the various heat treatment processes that unlock its full potential, enhancing its mechanical properties and ensuring optimal performance in demanding environments. Furthermore, we’ll discuss the alloy’s outstanding corrosion resistance, comparing it to other stainless steels to highlight its superior durability.

But that’s not all—AMS 5862’s versatility extends to its applications as well. From high-stress components in aerospace engineering to critical parts in chemical processing, we’ll uncover the diverse uses of this remarkable material. Whether you’re a manufacturer seeking to optimize production processes or a researcher comparing material properties, this comprehensive guide will provide the insights you need to fully understand and utilize AMS 5862 stainless steel. So, let’s embark on this journey to discover what makes AMS 5862 a true powerhouse in the world of stainless steels.

Introduction

Overview of AMS 5862 Stainless Steel

AMS 5862, also known as 15-5 PH stainless steel, is a specialized alloy designed for high strength, toughness, and excellent corrosion resistance. This alloy is part of the martensitic stainless steel family, known for its heat treatable high strength and good mechanical properties.

Key Characteristics

AMS 5862 is distinguished by several key characteristics that make it suitable for demanding applications:

  • High Strength: The alloy can reach very high tensile and yield strengths through heat treatment.
  • Excellent Toughness: It keeps good toughness even when highly strengthened, making it ideal for structural uses.
  • Corrosion Resistance: AMS 5862 resists corrosion well in many environments, crucial for harsh conditions.
  • Fabricability: It can be easily machined, welded, and formed using standard techniques.

Importance in Industry

Due to its exceptional properties, AMS 5862 is widely used in industries that demand reliable performance in stressful and corrosive environments. Key sectors using this alloy include aerospace, where it is used for engine parts, structural elements, and landing gear. It is also employed in defense for high-stress components, in power generation for gas turbine engines, valves, and shafts, and in nuclear reactors for its strength and corrosion resistance.

Composition and Properties

AMS 5862 includes chromium, nickel, and copper, along with smaller amounts of aluminum, molybdenum, and columbium plus tantalum. These elements give the alloy its unique balance of properties. Its mechanical properties can be customized through different heat treatments like H900, H925, H1025, H1075, and H1150, each providing varying strength and toughness levels.

Applications

AMS 5862 is versatile and robust, making it ideal for applications requiring high mechanical strength and corrosion resistance. Beyond aerospace and defense, it is used in power generation and nuclear industries where reliability and performance are essential.

By understanding the key characteristics and industrial significance of AMS 5862 stainless steel, engineers and designers can decide if it’s suitable for their specific applications.

Chemical Composition

Chemical Composition of AMS 5862

AMS 5862, also known as 15-5 PH stainless steel, has a carefully designed chemical composition that balances various properties. Here are the major elements and their respective ranges:

  • Carbon (C): Up to 0.07%. It helps achieve the desired hardness and strength through heat treatment.
  • Manganese (Mn): Up to 1.00%. It improves the alloy’s hardenability and tensile strength.
  • Phosphorus (P): Up to 0.040%. Low levels prevent embrittlement and maintain ductility.
  • Sulfur (S): Up to 0.030%. Keeping sulfur low helps maintain good impact toughness and ductility.
  • Silicon (Si): Up to 1.00%. It contributes to the alloy’s strength and oxidation resistance.
  • Chromium (Cr): 14.00% to 15.50%. It provides excellent corrosion resistance and hardness.
  • Nickel (Ni): 3.50% to 5.50%. Nickel enhances toughness, ductility, and corrosion resistance.
  • Copper (Cu): 2.50% to 4.50%. Copper aids in precipitation hardening, crucial for high strength.
  • Columbium plus Tantalum (Cb + Ta): 0.15% to 0.45%. These elements enhance strength and stability during heat treatment.
  • Molybdenum (Mo): Up to 0.50%. It increases resistance to pitting and crevice corrosion.
  • Iron (Fe): Makes up the balance of the composition, forming the alloy’s base structure.

Key Characteristics

The specific combination of these elements gives AMS 5862 several key characteristics, including high strength, excellent toughness, and corrosion resistance. Precipitation hardening, facilitated by copper, columbium, and tantalum, enhances the alloy’s strength and stability. Additionally, the alloy’s composition allows for easy machining, welding, and forming with standard techniques.

Importance of Composition

The precise chemical composition of AMS 5862 ensures it performs well in demanding applications, making it ideal for industries like aerospace, defense, and power generation. Understanding the composition helps engineers and designers select the right material for their specific needs, ensuring reliability and efficiency in their applications.

Mechanical Properties

Mechanical Properties Overview

AMS 5862 stainless steel, also known as 15-5 PH, offers a variety of mechanical properties that can be customized through different heat treatments, making it suitable for high-strength and tough applications. These properties make it highly versatile for demanding applications requiring high strength and toughness, and they vary significantly based on the heat treatment condition.

Mechanical Properties by Condition

The mechanical properties of AMS 5862 stainless steel change with each heat treatment, offering different levels of strength, hardness, and ductility.

Condition A

  • Hardness: Rockwell C hardness 363 HB max
  • Description: Solution annealed with no specific tensile or yield strength, serving as the baseline for further heat treatments.

H900

  • Ultimate Tensile Strength (UTS): 190 ksi
  • 0.2% Yield Strength: 170 ksi
  • Elongation: 10%
  • Reduction of Area: 35%
  • Rockwell C Hardness: 388-444
  • Summary: Offers the highest strength and hardness, suitable for applications requiring maximum mechanical performance.

H925

  • Ultimate Tensile Strength (UTS): 170 ksi
  • 0.2% Yield Strength: 155 ksi
  • Elongation: 10%
  • Reduction of Area: 38%
  • Rockwell C Hardness: 375-429
  • Summary: Provides a balance of high strength and moderate ductility.

H1025

  • Ultimate Tensile Strength (UTS): 155 ksi
  • 0.2% Yield Strength: 145 ksi
  • Elongation: 12%
  • Reduction of Area: 45%
  • Rockwell C Hardness: 331-401
  • Summary: Offers good strength with increased ductility compared to H900 and H925.

H1075

  • Ultimate Tensile Strength (UTS): 145 ksi
  • 0.2% Yield Strength: 125 ksi
  • Elongation: 13%
  • Reduction of Area: 45%
  • Rockwell C Hardness: 311-375
  • Summary: Suitable for applications requiring a balance of strength and higher ductility.

H1100

  • Ultimate Tensile Strength (UTS): 140 ksi
  • 0.2% Yield Strength: 115 ksi
  • Elongation: 14%
  • Reduction of Area: 45%
  • Rockwell C Hardness: 302-363
  • Summary: Offers moderate strength with good ductility.

H1150

  • Ultimate Tensile Strength (UTS): 135 ksi
  • 0.2% Yield Strength: 105 ksi
  • Elongation: 16%
  • Reduction of Area: 50%
  • Rockwell C Hardness: 277-352
  • Summary: Provides the highest ductility with good strength, enhancing toughness and formability.

Mechanical Properties for Sheets and Plates

AMS 5862 sheets and plates have slightly different mechanical properties than bars, especially in elongation and hardness.

Condition A

  • Hardness: Rockwell C hardness 38 max
  • Description: Solution annealed, serving as the baseline for further heat treatments.

H900

  • Ultimate Tensile Strength (UTS): 190 ksi
  • 0.2% Yield Strength: 170 ksi
  • Elongation: 5%
  • Rockwell C Hardness: 40-47
  • Summary: Provides the highest strength and hardness for sheets and plates.

H925

  • Ultimate Tensile Strength (UTS): 170 ksi
  • 0.2% Yield Strength: 155 ksi
  • Elongation: 5%
  • Rockwell C Hardness: 38-45
  • Summary: Offers high strength with moderate hardness.

H1025

  • Ultimate Tensile Strength (UTS): 155 ksi
  • 0.2% Yield Strength: 145 ksi
  • Elongation: 5%
  • Rockwell C Hardness: 35-42
  • Summary: Balances strength and ductility.

H1075

  • Ultimate Tensile Strength (UTS): 145 ksi
  • 0.2% Yield Strength: 125 ksi
  • Elongation: 5%
  • Rockwell C Hardness: 33-39
  • Summary: Provides good strength with higher ductility.

H1100

  • Ultimate Tensile Strength (UTS): 140 ksi
  • 0.2% Yield Strength: 115 ksi
  • Elongation: 5%
  • Rockwell C Hardness: 32-38
  • Summary: Offers moderate strength and good ductility.

H1150

  • Ultimate Tensile Strength (UTS): 135 ksi
  • 0.2% Yield Strength: 105 ksi
  • Elongation: 8%
  • Rockwell C Hardness: 28-37
  • Summary: Provides the highest ductility with good strength for sheets and plates.

Key Takeaways

  • Strength and Hardness: AMS 5862 exhibits high tensile and yield strengths, particularly in the H900 condition, making it suitable for applications requiring high mechanical performance.
  • Ductility: The alloy maintains good elongation and reduction of area, especially in the H1150 condition, enhancing its toughness and formability.
  • Heat Treatment Impact: Different heat treatments allow for a wide range of mechanical properties, enabling customization for specific applications.

Conclusion

Understanding these mechanical properties helps in selecting the appropriate condition of AMS 5862 stainless steel for various high-performance applications. Its versatility and ability to be tailored through heat treatments make it an excellent choice for demanding environments requiring both strength and toughness.

Heat Treatment Process

Solution Annealing

Solution annealing is an essential first step in the heat treatment of AMS 5862 stainless steel. During this process, the alloy is heated to 1010-1150°C (1850-2100°F) for 1-4 hours to dissolve precipitates and homogenize its microstructure. This prepares the material for subsequent heat treatments by creating a uniform and stable structure.

Precipitation Hardening

Precipitation hardening enhances the mechanical properties of AMS 5862 stainless steel by heating the material to specific temperatures to form strengthening phases. Various heat treatment conditions yield different mechanical properties.

H900 Heat Treatment

  • Temperature: 900°F (482°C)
  • Process: Heat the material to 900°F and then cool rapidly.
  • Results: This treatment achieves high tensile strength (around 190 ksi or 1310 MPa), yield strength (about 170 ksi or 1172 MPa), and a Rockwell C hardness of 40-47.

H925, H1025, H1075, H1100, and H1150 Heat Treatments

  • Temperature: Respective temperatures of 925°F (498°C), 1025°F (553°C), 1075°F (579°C), 1100°F (593°C), and 1150°F (621°C).
  • Process: Heat the material to the respective temperature and then cool rapidly.
  • Results: These treatments result in progressively lower tensile and yield strengths but increased ductility and toughness, with H1150 providing the highest ductility and formability.

General Heat Treatment Steps

After solution annealing, the alloy undergoes aging at around 480°C (896°F) for 4-16 hours to promote the precipitation of the strengthening phase, enhancing its strength, hardness, and toughness. Rapid cooling is essential to achieve the desired properties.

Effects of Heat Treatment

Heat treatment significantly influences the mechanical properties of AMS 5862 stainless steel. The H900 condition provides the highest tensile strength, while other conditions offer varying strengths with different levels of ductility and toughness. Hardness ranges from 38-47 HRC, depending on the treatment. AMS 5862 retains moderate corrosion resistance across different conditions, making it suitable for various industrial applications.

Corrosion Resistance

Chemical Composition and Corrosion Resistance

The corrosion resistance of AMS 5862 stainless steel is primarily influenced by its chemical composition. Key elements such as chromium, nickel, and copper contribute to its ability to withstand corrosive environments. The specific percentages of these elements are as follows:

  • Chromium (14.0-15.50%): Provides a protective oxide layer, enhancing resistance to oxidation and corrosion.
  • Nickel (3.50-4.50%): Increases toughness and helps maintain corrosion resistance.
  • Copper (2.50-4.50%): Aids in precipitation hardening and enhances corrosion resistance, particularly in acidic environments.
  • Columbium (0.45%): Stabilizes the alloy and prevents intergranular corrosion.

General Corrosion Resistance

AMS 5862 stainless steel shows moderate to high corrosion resistance, making it suitable for various industrial uses. Tests have shown that it performs well in both highly oxidizing and reducing environments. It is especially resistant to atmospheric corrosion, which is important for outdoor applications.

Comparative Corrosion Resistance

Compared to other stainless steels, AMS 5862 offers better corrosion resistance than Types 410 and 431, and is similar to Type 17-4 PH stainless steel. This makes it a versatile choice for environments requiring both strength and corrosion resistance.

Effect of Heat Treatment on Corrosion Resistance

The corrosion resistance of AMS 5862 depends on its heat treatment condition:

  • H900 Condition: Provides the best overall corrosion resistance. The aging process at 900°F results in a hardened structure that effectively resists both general and localized corrosion.
  • Higher Aging Temperatures (H1075, H1150): As the aging temperature increases, corrosion resistance slightly decreases. These conditions offer better ductility and toughness but come with a small reduction in corrosion resistance.

Mechanical Properties and Corrosion

The mechanical properties achieved through different heat treatments also affect the alloy’s corrosion resistance. For example:

  • Ultimate Tensile Strength (UTS) and Yield Strength: High strength levels, like those in the H900 condition, generally correlate with better corrosion resistance due to a refined microstructure.
  • Elongation and Hardness: The alloy maintains good elongation and hardness across various heat treatments, which helps preserve its structural integrity and resistance to corrosion.

Practical Applications and Corrosion Performance

AMS 5862 stainless steel is used in various applications where corrosion resistance is crucial:

  • Aerospace: Components such as engine parts, structural elements, and landing gear benefit from the alloy’s corrosion resistance and high strength.
  • Power Generation: Parts like gas turbine engine components, valves, and shafts require materials that can withstand corrosive environments while maintaining high mechanical performance.
  • Industrial Applications: The alloy is favored in the chemical, petrochemical, and food service industries due to its robust corrosion resistance and mechanical properties.

Understanding the corrosion resistance of AMS 5862 stainless steel is essential for choosing the right material for applications that demand both high strength and durability in corrosive environments.

Applications and Uses

Aerospace Industry

AMS 5862 stainless steel is a key material in the aerospace industry due to its outstanding mechanical properties and resistance to corrosion. The alloy is ideal for manufacturing critical components that require high strength and toughness, such as:

  • Engine Parts and Aircraft Structural Components: Components like turbine blades, compressor discs, shafts, fuselage frames, and wing spars benefit from AMS 5862’s high strength, toughness, and durability.
  • Landing Gear: AMS 5862 is ideal for landing gear parts because it can handle significant stress and impact.

Defense and Military

In the defense sector, AMS 5862 is highly valued for its strength and toughness, making it suitable for demanding applications:

  • Structural Components and Weapon Systems: AMS 5862 is used in military vehicles, equipment, and advanced weapon systems due to its high strength and corrosion resistance.

Power Generation

The power generation industry uses AMS 5862 for critical components that need to perform in high-stress environments:

  • Gas Turbine Engine Parts: AMS 5862 is essential for turbine blades, vanes, and other engine components exposed to high temperatures and corrosive environments.
  • Valves and Shafts: The alloy is used for valves and shafts that must maintain performance in harsh conditions.

Nuclear Industry

In the nuclear industry, AMS 5862 is used for reactor components like control rods, fasteners, and structural supports, due to its strength and toughness under radiation and corrosive conditions.

Manufacturing and Engineering

AMS 5862 is chosen for high-stress environments in general manufacturing and engineering due to its versatility and performance:

  • High-Stress Parts: Components such as gears, fasteners, and fittings benefit from the alloy’s high tensile strength and resistance to pitting and crevice corrosion.
  • Harsh Environments: AMS 5862 is ideal for parts that must perform reliably in corrosive or high-temperature conditions, ensuring longevity and durability.

Specific Components

The specific applications of AMS 5862 stainless steel are diverse, owing to its excellent mechanical properties and ease of fabrication:

  • Shafts and Gears: AMS 5862’s strength and toughness make it perfect for producing precisely machined shafts and gears.
  • Fittings, Fasteners, and Valve Parts: AMS 5862 is commonly used for fittings, fasteners, and valve components that need to withstand significant stress and corrosion.

Heat Treatment and Fabrication

AMS 5862 can be easily machined, welded, and formed, and its mechanical properties can be customized through heat treatments, making it a highly versatile material:

  • Machining: AMS 5862 can be precisely manufactured into complex components.
  • Welding and Forming: AMS 5862 can be effectively welded and formed into intricate shapes, enhancing its application versatility.

The wide range of applications and uses of AMS 5862 stainless steel across various industries underscores its importance as a high-performance alloy capable of meeting stringent requirements for strength, toughness, and corrosion resistance.

Fabrication and Machining

Formability

AMS 5862 stainless steel, also known as 15-5 PH, is highly adaptable for various forming processes. Its ability to undergo both cold and hot forming makes it suitable for applications requiring complex shapes and structures.

Cold Forming

Cold forming is an effective method for shaping AMS 5862 without applying heat, making it ideal for producing components that require precise dimensions and high strength. The alloy can be cold formed into various shapes, including sheets, strips, and complex geometries, while maintaining its mechanical properties and surface finish. Cold working can increase hardness and strength, so intermediate annealing might be needed to relieve stress and prevent cracking.

Hot Forming

Hot forming heats the material to make it more pliable, allowing easier shaping. This process usually heats the alloy to between 1700°F and 1900°F (927°C to 1038°C). Although less common due to the precipitation hardening characteristics of AMS 5862, hot forming can be performed when necessary. It is useful for applications requiring large deformations, achieving complex shapes while minimizing the risk of cracking.

Machining

Machining AMS 5862 stainless steel requires careful attention to tooling, cutting parameters, and cooling techniques due to its high strength and hardness. Proper machining practices ensure a good surface finish and extend tool life.

Tooling and Cutting Parameters

The high strength and hardness of AMS 5862 necessitate the use of robust tooling and optimized cutting parameters, with carbide tools being preferred for their ability to withstand high cutting forces and temperatures. The recommended cutting speeds and feed rates depend on the specific heat treatment condition of the alloy. For instance, the H900 condition, being harder, requires lower cutting speeds and higher feed rates compared to softer conditions like H1150.

Cooling and Lubrication

Adequate cooling and lubrication are crucial to prevent overheating and excessive tool wear. Using high-performance coolants helps dissipate heat, reduce friction, and improve the overall surface finish. It’s important to ensure a consistent flow of coolant to the cutting zone, especially during high-speed operations.

Surface Finish

A high-quality surface finish is essential for applications needing low friction and high precision. AMS 5862 can achieve excellent surface finishes with proper machining techniques. Fine-grained carbide tools and precision grinding are effective methods for attaining the desired surface roughness. Controlling the depth of cut and maintaining sharp tooling edges contribute to a superior finish.

Heat Treatment

Heat treatment is key to optimizing the mechanical properties of AMS 5862 stainless steel. The process involves solution annealing followed by precipitation hardening to achieve the desired strength, hardness, and toughness.

Solution Annealing

Solution annealing is typically performed at temperatures ranging from 1010°C to 1150°C (1850°F to 2100°F) for 1 to 4 hours. This process dissolves precipitates and homogenizes the microstructure, preparing the material for subsequent aging treatments. Proper solution annealing ensures a uniform and stable structure, essential for consistent mechanical properties.

Precipitation Hardening

After solution annealing, AMS 5862 is precipitation hardened to achieve high strength and hardness. The alloy is aged at various temperatures, depending on the desired mechanical properties. Common aging treatments include:

  • H900: Aging at 900°F (482°C) for 4 hours, resulting in maximum strength and hardness.
  • H925, H1025, H1075, H1100, H1150: Aging at respective temperatures for varying durations, balancing strength, ductility, and toughness.

Each heat treatment condition offers different mechanical properties, allowing customization based on specific application requirements.

Welding

Welding AMS 5862 stainless steel is possible with standard techniques, but precautions are needed to maintain its mechanical properties and corrosion resistance.

Welding Techniques

Common welding methods for AMS 5862 include GTAW/TIG, GMAW/MIG, and SMAW. These techniques provide good control over the heat input and allow for precise welding of the alloy.

Precautions

Pre-weld and post-weld heat treatments are crucial to prevent brittle phases and ensure optimal properties. Pre-weld heating helps minimize thermal stresses, while post-weld heat treatment, such as solution annealing followed by aging, restores the desired mechanical properties and corrosion resistance.

By understanding the specific requirements for fabrication and machining, engineers and manufacturers can effectively utilize AMS 5862 stainless steel in various demanding applications, ensuring optimal performance and longevity.

Frequently Asked Questions

Below are answers to some frequently asked questions:

What is the chemical composition of AMS 5862 stainless steel?

AMS 5862 stainless steel, also known as 15-5PH stainless steel, has the following chemical composition: Carbon (C) 0.07% maximum, Silicon (Si) 1.0% maximum, Manganese (Mn) 1.0% maximum, Phosphorus (P) 0.03% maximum, Sulfur (S) 0.015% maximum, Chromium (Cr) 14.0-15.50%, Nickel (Ni) 3.50-5.50%, Copper (Cu) 2.50-4.50%, Columbium (Cb) 0.45% maximum, Molybdenum (Mo) 0.50% maximum, and Iron (Fe) balance.

What are the mechanical properties of AMS 5862 in different conditions (e.g., H900, H925)?

The mechanical properties of AMS 5862 stainless steel, specifically 15-5PH, vary based on its heat treatment condition. In the H900 condition, it exhibits an ultimate tensile strength of 190 ksi, a yield strength of 170 ksi, 10% elongation in 2 inches, a reduction of area of 35%, and a Rockwell C hardness of 388-444. In the H925 condition, the ultimate tensile strength is 170 ksi, yield strength is 155 ksi, elongation is 10%, reduction of area is 38%, and Rockwell C hardness ranges from 375-429. These properties highlight the alloy’s adaptability to different mechanical requirements, making it suitable for high-performance applications.

How does the heat treatment process affect the properties of AMS 5862?

The heat treatment process significantly impacts the properties of AMS 5862 stainless steel. This alloy can be heat-treated to various conditions, such as Condition A (solution annealed) and Conditions H 900 to H 1150, to tailor its mechanical properties. For instance, in Condition H 900, the material achieves high tensile and yield strengths, while higher heat treatment temperatures like H 1150 reduce these strengths but increase ductility and toughness. Additionally, specific treatments like Condition H 1150-M (double overaged) enhance the material’s toughness and resistance to stress corrosion cracking. Overall, heat treatment allows for the optimization of AMS 5862’s mechanical properties, corrosion resistance, and microstructure to meet diverse application requirements.

What are the common applications of AMS 5862 stainless steel?

AMS 5862 stainless steel, also known as 15-5PH, is commonly used in applications that require a combination of high strength, toughness, and moderate corrosion resistance. Key applications include aerospace components such as engine parts, structural elements, and landing gear; power generation parts like gas turbine engine components, valves, and shafts; nuclear reactor components; military structural components; and other high-performance parts such as turbine blades. These uses leverage the alloy’s excellent mechanical properties and corrosion resistance.

How does AMS 5862 compare to other stainless steel alloys in terms of corrosion resistance?

AMS 5862 stainless steel, also known as 15-5PH, offers moderate corrosion resistance that is similar to 17-4 PH stainless steel. It surpasses the corrosion resistance of Types 410 and 431 stainless steels. This alloy is particularly effective in both oxidizing and reducing environments and maintains its corrosion resistance best in the fully hardened condition, although it decreases slightly with increased aging temperatures. The alloy’s balanced composition, including elements like chromium, nickel, copper, and columbium, contributes to its corrosion resistance. This makes AMS 5862 suitable for applications requiring a combination of high strength, toughness, and moderate corrosion resistance, such as in aerospace and nuclear industries.

Can AMS 5862 be easily machined, welded, and formed?

AMS 5862, also known as 15-5 PH stainless steel, can be machined, welded, and formed, but these processes require specific considerations. Machining is best performed in the solution-annealed condition (Condition A) and improves significantly after heat treatment. Welding is feasible using common fusion and resistance techniques, with optimal results achieved by selecting appropriate heat-treated conditions and possibly using a weld filler like AWS E/ER 630. Forming operations are generally limited to mild operations in Condition A, with heat treatment before cold working or hot forming methods recommended to maintain mechanical properties. Overall, while AMS 5862 is versatile, careful handling and specific techniques are necessary to optimize its properties during fabrication.

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