Technical Terms of Corrosion Simplified

Stress Corrosion Cracking

ssc

Stress corrosion cracking or SCC occurs when these two factors occur simultaneously:

1. Tensile stress (either directly applied or residual stress)

2. Corrosive environment like saltwater or acid

The tricky part about stress corrosion cracking is that it may occur in mildly acidic environments which typically cause little or no effect to the material. It is only the combination of stress and corrosive media which causes it to occur – both factors must be present for SCC to take place. As most of the surface remains unattacked, except for a few fine cracks, the material may appear unharmed – metals often remain bright and shiny – causing SCC to go undetected until unexpected failures occur.

SCCImageMaterials In Focus:

SCC of nickel alloys has been found to occur in three types of environments: high-temperature halogen-ionic solutions, high-temperature waters, and high-temperature alkaline environments. 

  • C276 offers excellent stress corrosion cracking resistance many acidic, reducing and mildly oxidizing environments. 
  • Monel fasteners and flanges prevent stress corrosion cracking and pitting in most fresh and industrial waters; whereas stagnant salt water situations can sometimes result in crevice and pitting corrosion to occur.
  • AL-6XN’s high nickel and molybdenum contents make it resistant to SCC (stress corrosion cracking) in chloride. 

 


Pitting 

pittingThis is an extremely localized corrosion that leads to the creation of small holes in the material. Once pitting corrosion occurs, it can quickly spread into the material, corroding it entirely. An easy way to wrap your brain around this concept is a tooth with a cavity – where there is a small point of decay that can spread throughout your tooth. Pitting is often the most destructive form of corrosion and the most difficult to detect since the pits that cause the initial attack are often very small yet corrode deeply. Pitting Corrosion Cross sec

Pitting corrosion typically occurs when there are points of weakness in the passive layer. Pitting is affected most by acids, chlorides and high temperature. Chloride is particularly damaging to the protective passive layer of a metal so pitting can initiate at oxide breaks.

Materials In Focus: 

  • AL-6XN is an ideal choice to help prevent pitting corrosion in chloride environments.
  • Titanium has been shown to have no signs of pitting corrosion even after years of submersion in seawater.

Intergranular Corrosion 

intergranular corrosionThis is where the grain boundaries of the material’s structure are more susceptible to corrosion. So what does that mean? Each material is made up of grains, surrounded by grain boundaries, packed tightly together to form the metal or alloy.

Think of the material like a brick wall, with the grains of the material being the bricks and the grain boundaries being the mortar. Intergranular corrosion occurs in the mortar (grain Intergranular corrosion1boundaries) or along the edge of the mortar while the grains themselves (or for our example the bricks) remain largely unaffected.

Intergranular corrosion is a localized attack affecting the grain boundaries rather than the grains. Even though corrosion only occurs at the grain boundaries, it will still cause the material to disintegrate. Think of our brick wall. If you destroy the mortar the wall will fall, even if the bricks themselves are still intact.  

Intergranular corrosion is typically caused by:

  • Impurities at the grain boundaries
  • Enrichment of one of the alloying elements
  • Depletion of an alloy element in the grain-boundary area

Corrosion Fatigue

fatique crackThis type of corrosion occurs when there are cycles of stress on a material in a corrosive environment. The altering stresses are thought to cause the passive protective film to break which causes the underlying material to occur. Keep in mind that often the rapidly fluctuating stresses may be well below the tensile strength of the material. Similar to stress corrosion cracking, corrosion fatigue is caused by cyclic stresses whereas SCC is brought on by constant stress.Fatique Corrosion

Think of it like a shoe. Cycling stress occurs when you are walking (verses the constant stress of standing – SCC). This altering stress can cause cracks or breaks in this protective soles (like the passive layer).


 

Crevice Corrosion

crevicesCrevice corrosion is an intense localized corrosion, which occurs within crevices or gaps between two joining services. It can occur in the crevice or gap between two metals or a metal and non-metallic material. Outside this area the materials may be completely resistant to the crevice corrosioncorrosive environment, but when the corrosive solution becomes trapped or stagnant in this gap, chemical changes can occur in the solution causing the micro environment to be very corrosive.

 

 


Passivation

passivation

This is the creation of an outer protective layer to a material – also called the passive layer. It is formed when a chemical reaction occurs with the base material to rapidly oxidize the surface. In terms of many metals and alloys, this technique creates a metal oxide layer that protects the base material from corrosion and is especially important on materials that form this oxide layer slowly, like steel but much less important for corrosion resistant alloys like Hastelloy C276 as the oxide layer is readily formed in air. It is called a “passive” layer as it is less affected by the environment. A simple example is the tarnish of silver.


Galvanic Corrosion

galvanic picAlso called two-metal corrosion, this occurs when two different metal or alloys are placed in contact with one another and are immersed in a corrosive or simply a conductive solution like sea water. When these distinct metals touch each other in this type of environment, it causes electron flow between them, which results in galvanic corrosion – with the less noble material being severely attacked and the more noble material suffering less attack. 

galvanic corrosionWith regards to fasteners, it’s extremely important that the more noble material be the actual fastener, as galvanic corrosion could rapidly corrode the threads of a screw. The effects of galvanic corrosion could be minimized if the less noble material be significantly larger in mass. Like a screw going into a large piece of process equipment. The galvanic effects are distributed across a large mass and not concentrated on the relatively small threads. Galvanic corrosion could also be avoided by electrically isolating the fasteners with non-conductive polymers or ceramics. Galvanic Corrosion Chart Aug 2020

Industrial Fasteners

Industrial CollageThe industrial segment has a broad range of requirements and we pride ourselves on being able to solve some of industries most challenging fastener applications. Working with our customers in the chemical processing, oil & gas, pharma, mining, electronics, alternative energy etc. we help them choose the best materials and fastener form for their tough applications. 

If you have an extreme fastener requirement, contact our experts and let us know how we could help

 

Medical Device Fasteners

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Extreme Bolt & Fastener focus on medical device fastener prototyping. We can accommodate short runs, unique alloys and custom designs. Whether its modifying an existing design or a completely new concept, Extreme Bolt & Fastener can help you rapidly produce and prototypes your designs. Specializing on engineered polymers like PEEK and PTFE and specialty alloys like titanium, tantalum and cobalt chrome (MP35N), we understand the competing needs for bio-compatibility, strength, weight, modulus and can help you understand the various grades and subtleties of production that affect these parameters.

If you have a medical device requirement, contact us and let us know how we could help.

  • Specialty Alloys & Polymers
  • Short Runs
  • Quick Lead Times
  • Modified Standard Parts
  • Custom Fasteners 

PTFE

PTFE is a thermoplastic polymer which is known for its strength, toughness, lubricity, biocompatibility and chemical inertness.  It is also useful due to its ability to prevent bacteria and other infectious agents from adhering to it. PTFE is most widely used for graft material in surgical interventions and implants of soft tissue replacement due to its biocompatibility and inertness.

Learn more about PTFE fasteners.


PEEK

Originally developed by the aerospace industry in the 1970’s it offers a diversity of industries the unique combination of a high temperature, high strength polymer. More than 20 years later a highly pure and implantable grade of PEEK was developed and soon adopted as a standard in medical devices. Then in 2000’s a carbon-fiber reinforced PEEK made its debut into the medical community. Today it is widely accepted across a broad range of implants, especially spine implants as well as bone fixation screws, and dental implants. It usability continues to rise due to its:

  • Improved compatible with diagnostic imaging than metal implants - x-ray transparency of PEEK prevents image distortion, even on CT and MRI
  • Biocompatibility and bio-stability
  • Strength and stiffness, even in instances where metals were historically the standard practice
  • Favorable fatigue, creep, and wear performance
  • Chemical resistance and stability allow it to be sterilized using common sterilization methods

Learn more about PEEK fasteners.


Titanium

Titanium’s high strength-to-weight ratio and biocompatibility make it an ideal material for many medical applications. Titanium grade 23 or TI 6AL-4V ELI is an Extra Low Intersticial grade and is typically looked upon as medical grade titanium. In the medical device community titanium is often used for implants in joint replacement, as well as dental implants; many of these lasting up to 20 years.

  • Biocompatibility, as well as the ability to meaning that it serves as a structural and functional connection between living bone and the surface of a load-bearing artificial implant
  • Well-known for its high strength-to-weight ratio, Titanium is 60% denser than aluminum, but more than twice as strong
  • Low density that is quite ductile, which prevents cracking
  • Non-magnetic and non-ferromagnetic, which allows patients to be safely imaged with MRI

Learn more about titanium fasteners.


Tantalum

In industry, tantalum is most often known for its superior corrosion resistance and inertness. However tantalum is also one of the most biocompatible metals due to the fact that tantalum non-reactive in most medias including the human body.  Because tantalum does not irritate the body, more rapid bone growth can be achieved which is why tantalum finds uses in orthopedic and spinal implants.

  • Superior inertness and biocompatibility.
  • Dense, ductile and hard.
  • Ability to form a direct bond to hard tissue
  • Nonirritating and resistant to bodily fluids

Learn more about tantalum fasteners.


MP35N

Comprised of nickel, cobalt, chromium and molybdenum, MP35N is a super alloy which delivers a combination of superior high strength, toughness, ductility, and corrosion resistance. Beyond its overall package, MP35N is most often utilized by the medical community for its extreme tensile strength of 227 ksi to 294 ksi (age hardened). In addition, MP35N is also biocompatible which is critical for use in this field. These two key properties make it a choice for braces which require strength and ductility to withstand rigors of orthodontics, even in small and delicate formations. In addition, prosthetics also rely on MP35N’s superior strength for weight-bearing support.

Learn more about MP35N fasteners.

Aerospace Fasteners - NAS Screws

Aerospace Unsplash Free Rocketlaunch

Extreme Bolt & Fastener’s aerospace focus is in specialty alloys, short runs, custom parts and modified version of standard NAS fasteners with quick lead times.  Our niche is on corrosion resistant, lightweight and high temperature alloys like A-286Inconel 718TitaniumMP35NWaspaloy.

If you have an aerospace fastener requirement, contact us and let us know how we could help.

  • Specialty Alloys
  • Short Runs
  • Quick Lead Times
  • Modified Standards / Modified NAS Screws
  • Custom Fasteners

A286

This is an iron-based superalloy which features an austenitic structure with high amounts of nickel and chromium. A286 (or Incoloy) is ideal for high strength and corrosion resistance up to 704°C and for lower stress applications at high temperatures. Learn more about A-286 fasteners.

Benefits:

  • Low temperature capabilities including ductility, non-magnetic, high strength to -196°C
  • Good strength and oxidation resistance at temperatures up to 1300°F
  • Low stress application above 1300°F
  • High oxidation resistant in continuous service up to 1500°F (816°C) and intermittent service to 1800°F (982°C).
  • Excellent corrosion resistance to high temperature atmospheres such as those encountered in jet engine applications

Fastener Uses:

  • Gas turbine disks and blades
  • Turbine wheels, frames, casings, afterburner parts

Inconel 718

Operating aircraft engines at higher temperatures improves energy efficiency and hence fuel efficiency. To do so, aerospace engineers rely on super alloys like Inconel 718 for the hot sections of turbo reactors. Inconel 718 is an age (precipitation) hardened alloy that retains its high yield strength and usability to 1800°F. Did you know that 50% of the Inconel 718 produced is used solely for the manufacturing of aircraft engines in their essential parts including blades, sheets and discs?  Learn more about Inconel Fasteners

Benefits:

  • Usable to 1800°F
  • Good creep and rupture strength with a high resistance to fatigue
  • Low susceptibility to post-weld cracking
  • Strong resistance to corrosion up to 1000°C
  • Resistant to pitting

Fastener Uses:

  • High pressure section of the compressor
  • Rocket engine components
  • Hot sections of turboreactors

Titanium

Both military and commercial aircraft utilize titanium for its superior strength-weight ratio, helping them to be lighter and more fuel efficient without sacrificing safety and longevity. In addition engine and airframe parts which need to withstand temperature swings from subzero to 600°F utilize titanium’s high temperature strength performance. Learn more about titanium.

Benefits

  • High strength to weight ratio - Titanium grade 5 is about 4x stronger than steel but 45 percent lighter
  • Resistance to corrosion
  • High temperature performance to 600°F for Grade 5
  • Nonmagnetic and does not conduct heat or electricity well

Used as Fasteners in:

  • Exterior air frames
  • Jet engine parts including the housing, fan blades, pumps, and screens
  • Discs, blades, shafts and casings for the front fan to the rear end of the engine
  • Landing gear
  • Internal components of wings and propellers

MP35N

The superman of materials, this material defines strength. It is a nickel-cobalt based alloy that boasts ultra-high strength, toughness, and ductility. Learn more about MP35N.

Benefits:

  • Maintain strength in maximum operating temperature of 800°F
  • Tensile strength of 227-294 ksi at room temperature
  • MP35N resists corrosion in hydrogen sulphide, salt water and other chloride solutions.
  • Resistant to crevice and stress corrosion cracking in extreme environments.
  • Ideal for when application requires the combination of hight strength, high modulus values and good corrosion resistance.

Fastener Uses:

  • Leading edge strips
  • Airframes
  • Space shuttle structure

Waspaloy

When temperatures are hot, this super alloy can take the heat and maintain its strength. Waspalloy is a nickel based alloy which delivers strength and reliability at extreme temperatures as high as 1600°F/870°C.  Waspaloy derives its high-temperature strength from a solid solution of molybdenum, cobalt and chromium, and its age-hardening elements aluminum and titanium. When hot, Waspaloy a stable and adherent oxide layer protecting its surface. It is often used for hottest sections of jet engines and other gas turbines where other super alloys such as Inconel 718 might fail due to extreme heat.  Learn more about Waspaloy fasteners.

Benefits:

  • Temperature limits of 1200°F (650°C) for critical rotating applications and up to 1600°F (870°C) for stationary parts
  • Relatively impervious to  under conditions of frequent thermal cycling, as well as continuous exposure to temperatures up to 1900°F
  • Low thermal conductivity
  • Excellent creep rupture strength

Fastener Uses:

  • Parts where burning jet fuel can cause parts to become immensely hot for extended periods of time
  • Gas turbine blades, seals, rings, shafts and turbine disks
  • Missile systems

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