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Structural Materials for Motorcycles

Billy Wight, President, Luxon MX

July 13, 2024

Billet Aluminum
A pile of 7075 and 6061 billet blanks ready to be machined into triple clamps.

We've got a future blog post on flex/stiffness in the works, but to better understand that, we first need to go over materials. Here we'll cover various structural materials, alloys, tempers, and why or why not they might be a good choice for triple clamps or other parts on the bike.

Note: This is an enormous subject to cover, and this blog post is not intended to replace multiple engineering courses in materials science! There will be exceptions to the rules and the generalizations presented here, but the vast majority of this directly applies to the discussion of structural motocross parts and is correct for the scope of this discussion.

Material Properties

There are A LOT of different material properties. Structural properties, thermal properties, manufacturing properties, etc. But for this discussion, we're focusing on the primary structural properties that are relevant to what you feel on the bike. The chart below lists these properties for a variety of materials. Materials that may be suitable for a triple clamp are highlighted in yellow. Other materials are presented for reference. Finally, there are comparison percentages listed for each material; those are all relative to 6061-T6 aluminum as a baseline since that is a common material used in many motorcycle parts.

material properties chart

A summary of various material properties

Density (ρ)

This is how much the material weighs for how much of it there is in volume. A square meter of water weighs 1000 kilograms, so the density is 1000 kg/m3. Steel has a density nearly eight times that at about 7800 kg/m3, and aluminum is much lighter at about 2700 kg/m3.

Modulus (E)

Young's modulus, also called tensile modulus, is a measure of how much stress a material has for a given strain (deflection). It is directly related to the stiffness of the material. A material that has twice the modulus of another material will be twice as stiff. The material modulus of the various parts is very significant to the feel of the bike since it's one of the two attributes that contributes to the overall stiffness that you feel. An interesting thing to note here is that various alloys of the same material will have nearly the same Modulus (within a few percent). But modulus varies significantly between different materials.

Yield Strength (YTS)

The yield strength is the stress level at which a material starts to permanently deform (bend). Once the part has reached this point, it has failed (it's bent, etc.) and needs to be replaced.

Ultimate Strength (UTS)

The ultimate strength is the stress level of the material at which it completely fails: cracks, splits, etc. It isn't terribly significant because you've already yielded (bent) the part before you get to this point. But it's usually nice for the material to have a good gap between the yield stress and the ultimate stress level, so the part bends instead of completely failing.

Note that strength and stiffness are not the same thing! I've seen confusion around this in some discussion forums and posts online. Stiffness is how much something deflects with a force applied to it. Strength is how much it can deflect before it fails (bends or breaks).

Alloys

Some people think of aluminum when the word alloy comes up; I've seen it used interchangeably in various writings. But alloy doesn't specifically refer to aluminum. Most structural metals are alloys, which just means that they are combinations of multiple metals. 6061 aluminum is an alloy of aluminum with a small amount of magnesium and silicon added (plus tiny amounts of other metals). Grade 5 titanium is an alloy of titanium with 6% aluminum and 4% vanadium added. Brass is an alloy of copper and zinc. Steel is an “alloy” of iron and carbon (carbon, being a non-metal technically doesn't make steel an alloy unless other metallic elements are added). The following chart breaks down the differences in some popular aluminum alloys. The 1060 “alloy” is included for reference as 1000 series aluminum is essentially pure aluminum.

alloy percentages chart

Details of various aluminum alloys

The base element will be the vast majority of the alloy and smaller amounts of other elements are added to change the material properties. It doesn't take much to significantly change the properties of an alloy. From the properties chart you can see that pure aluminum (1060) isn't very strong. But the addition of less than 5% of other elements, making it 6061 alloy, can increase its strength by more than ten-fold!

Different alloys are developed for strength reasons, resistance to high heat, manufacturability, etc. There are thousands of different alloys, all for different purposes. For example, you will use a different aluminum alloy for a machined part than you would for a cast part. The casting alloys have different elements added that help the material flow through the mold better. Those additional elements also reduce the strength of the casting alloy, so they are not included in the alloys used for machined parts.

Heat Treatment

Some alloys are heat treatable. Heat treatment is the controlled heating and cooling of a material to alter its properties. Different crystal structures can form in an alloy at different temperatures. By controlling the formation of these structures at high temperatures and cooling the material at specific rates to “lock” them in place, different properties are produced. The 2000, 6000, and 7000 series of aluminum alloys are all heat treatable and you'll usually see a T designation after the alloy. This is the temper, which refers to the specific heat treatment of the alloy. For example, 7075-T6 aluminum. The 7000 series designates a blend of mostly aluminum with zinc and other elements added. 7075 is a more specific blend of those elements; T6 is the temper referring to how the heat treatment was performed.

Work (Strain) Hardening

Alloys that are not heat treatable can be work hardened. The processing of the material (rolling out extrusions, etc.) hardens and strengthens the material. The 3000 and 5000 series of aluminum alloys are not heat treatable, but they are work hardening. Work hardening is designated with a H number after the alloy, like 5052-H24.

Both heat treatment and work hardening alter the properties of the material. Most notably, the properties of strength, hardness, and ductility are changed. But neither heat treatment nor work hardening change the modulus (stiffness) of the material. This is a common misconception.

Material Property Ratios and Dependencies

The ratio between properties is a useful way to compare materials, particularly stiffness-to-weight and strength-to-weight. Most relevant structural metals have a very similar stiffness-to-weight ratio. You can see from the material properties chart presented earlier (all ratios are relative to the popular 6061-T6 material for ease of comparison).

Of the yellow highlighted materials (those suitable for structural components), the stiffness-to-weight ratio is the same within 3% and most are under 1%. Isn't that interesting? If you take a steel bar and pull on it, it will have a particular tensile stiffness. If you were to find an aluminum bar of the same weight and same length as the steel bar (it will have a larger cross-section) and pull on it, it will also have the same tensile stiffness as the steel bar. And the same applies for a titanium bar or magnesium bar. This is illustrated in the image below. All four bars are the same length, weigh the same, and have the same stiffness in tension (designated by the arrows). The only difference between them (aside from the material) is the cross-sectional area.

Bars of different material, but same weight and tensile stiffness
The four bars are all different materials, but all weight the same and have the same tensile stiffness.

It's worth noting that the bending stiffness of all four bars is different. Because the cross-sectional area of the magnesium bar is the biggest, it will have the highest bending stiffness. And the steel bar, despite its high modulus, will have the lowest bending stiffness. This demonstrates the importance of geometry to the resulting stiffness of a part. Because of this, the lowest density material will always be the winner here as it will have the largest cross-section. I'll get into a lot more detail on this in our next blog post on stiffness.

So, stiffness-to-weight is pretty much the same for all structural metals. But the strength-to-weight ratio is a different story… You can see from the previous chart that the strength-to-weight ratio varies significantly between materials and their different alloys. Since the stiffness-to-weight ratio is pretty consistent, the strength-to-weight ratio is a large factor in material selection.

Linear Properties

One nice thing about metals is that their stiffness and strength properties are linear within their useful range. If, for example, if you apply a force to the front end of the bike, then the triple clamps, fork tubes, frame, etc., will all flex some amount and be at a certain level of stress. Remove that force, and they go back to their original position and no stress. If you repeat that, but double the force, the flex also doubles and so does the stress. Triple it and everything triples as well.

This linear relationship remains true until you've either flexed things so much that the geometry has significantly changed or until the stress level in the material has exceeded the yield strength of the material, and it fails. Of course, there are some exceptions to this rule for unique geometries, but for most relevant metal parts on the bike, we can assume everything is linear under normal conditions.

This is referred to as Hooke's Law, which states: “the strain of the material is proportional to the applied stress within the elastic limit of that material”.

Material curve, Hooke's Law

A typical stress-strain curve for metals

The image above depicts a typical stress-strain curve of a metal. The linear region (green) is the “useful range” I mentioned. This applies to all the metal parts on your bike and handlebars are a great example:

• Every bump you hit causes the bars to flex some, but they stay in the linear range and they return to their normal shape after the bump. The bars are just a spring in this sense, deflecting as you hit a bump, then returning straight after the bump.

• But if you crash, there can be enough force to bend the bars permanently by exceeding the material yield strength. This is the orange region of the curve, with stresses higher than the yield strength of the material. At this point, the bars have failed and need to be replaced.

• And if you crash really hard you can break the bars completely into two pieces. This is a stress higher than the ultimate strength of the material (red region of the curve).

Neither bending nor breaking is a good outcome! So clearly, we want to stay in the linear region where the bars continue to do their job as a spring but don't fail.

Directional Properties

Many materials have direction dependent properties. This is especially true in materials like carbon fiber where the direction of the fibers has a massive impact on the stiffness and strength properties in that direction of the material. We refer to this as having anisotropic material properties.

In the case of most metals, though, we have isotropic material properties. This means that the material properties are essentially the same in all directions. Of course there are some exceptions to this, but that's outside the scope of this post (and mostly irrelevant for the subject of materials on the bike).

Material Selection

Ashby material selection plot

An Ashby plot showing the relationship between various materials strength and density properties

There's a lot that goes into material selection when you're designing a part. Everything I've touched on in this post is significant, plus a lot of other details I haven't. We won't get too deep into all the requirements, but here's a quick breakdown of materials and their application for an aftermarket machined triple clamp (also largely applies to many other parts - bar mounts, linkages, engine mounts, etc.):

Foams, Plastics, and Rubbers

This may be obvious, but the low stiffness and strength properties of these materials eliminates them as contenders for a triple clamp. There is use for them in some areas, of course, like the synthetic rubber bushings we use as vibration isolators in our 4-post bar mounts.

Carbon Fiber

This structural composite is an amazing material. Lightweight and super strong, but it's expensive, requires rather complicated manufacturing processes and is susceptible to significant strength reduction after it has been damaged. For example, roost hitting a triple clamp can cause stress risers where a carbon clamp could fail. And it tends to fail catastrophically when it does let go! Triple clamps are rather bulky and see loads in many directions. They would be a very complicated part to design and effectively manufacture from carbon fiber. For these various reasons it's not a good choice.

Magnesium

Magnesium, specifically AZ31B-H24, seems like a great material. It's really lightweight and has a good strength-to-weight ratio. But it's not a heat treatable alloy, it's work hardened. With the thickness of the billet we need for triple clamps, the work hardened (higher strength) portion of the material is only on the outside of the billet. The material in the middle is not work hardened and can have up to 30% less strength. Magnesium is also horribly corrosive with few coatings available to stop/slow the corrosion. On top of that, availability is relatively scarce, and it's really expensive. All that pretty well rules it out.

Titanium

Titanium is a metal that a lot of motorsports people love, and rightfully so for the right parts. A grade 5 titanium bolt is stronger than a class 8.8 steel bolt, but 40% lighter. Titanium also has excellent corrosion resistance. But for triple clamps, it's not a great choice. It's really expensive, and it's rather difficult to machine. Additionally, the thin walls required to achieve a reasonable weight don't give much bending stiffness or strength. The high cost and difficulty of manufacturing eliminate titanium as a material choice.

Steel

Steel is out for some of the same reasons as titanium. Though it's far less costly, and most alloys have good strength, the high density requires really thin walls to keep the weight down. These walls have low bending and buckling strengths and increase the difficulty of machining. Further, steel is corrosive and requires coatings to keep it from rusting.

Stainless Steel

Similar to steel, except with enhanced corrosion resistance. Some alloys of stainless steel are the optimal choice for high stress parts exposed to really high heat, but that's not a match for triple clamps.

Aluminum

I saved the best choice for last… Aluminum is readily available, lightweight yet strong, has adequate corrosion resistance, and machines fairly easily. For structural applications, the heat-treatable alloys are great choices, but which one is the best? It depends on which trade-offs you are willing to make in the design. And it often comes down to cost vs. performance.

6061-T6

This is the most common structural aluminum alloy (6082-T6 is a close equivalent prevalent in European countries). It's used all over the place as it's fairly strong, yet inexpensive. This alloy is suitable for triple clamps, but it doesn't offer the performance available with premium alloys. We use 6061-T6 in our Gen3 standard triple clamps to offer a performance clamp at a reasonable price point.

7075-T6

One of the top choices for triple clamps. It's 82% stronger than 6061, 4% stiffer, and only 4% heavier. This alloy has one of the highest strength-to-weight ratios of the aluminum alloys. So, you can design a triple clamp that's significantly stronger than one from 6061 but at the same weight and stiffness. Or you can design a lighter weight clamp that's still stronger. The drawback of this material is that it's rather pricey, at more than three times the cost of 6061. We use 7075-T6 on our Gen3 Pro triple clamps, where cost comes secondary to performance.

2024-T4

This 2000 series alloy is not a terrible choice, but it is a strange choice. The main reason to choose 2024 is that it retains its strength better at high temperatures than other aluminum alloys. But triple clamps aren't exposed to high temperatures, so there's no benefit there. It's slightly stronger than 6061-T6, but not nearly as strong as 7075-T6. It is more ductile than 7075 (there's a bigger window between bending and breaking), but that increase in ductility doesn't justify the much lower strength than 7075-T6. 2024 is also expensive, at about the same cost as 7075-T6. So, if you see someone making triple clamps from 2024, you should question why.

Proprietary Alloys

I've seen some companies claim they're using a custom material in their parts. Well, there's simply not enough money in this industry to justify the cost of developing and purchasing a custom alloy. And there's no significant performance reason to do it in the first place. This is their marketing department trying to make you think they are more advanced than they really are, or worse, they're trying to hide the fact they're using a cheaper alloy than what they should be using.

A Common Misconception

In most of our blog posts I like to refute one of the (many) myths in the motocross world. And this one is everywhere: “titanium hardware makes the bike more rigid than steel hardware”. This comes up A LOT from mechanics, riders, testers, “engineers”, etc. Here's an example:

Now, I'm not trying to single anyone out here in particular; this is an industry-wide issue. You won't have to try hard to find other examples from many people saying the same thing. This myth has been perpetuated for so long and by so many, that riders are “feeling” a difference because they expect to (not because it's actually there).

But the reality is quite the opposite. And now that you have more understanding of material properties, it's pretty simple to see why: Steel hardware has a modulus of about 200 GPa and titanium hardware has one of about 114 GPa. The exact numbers and units don't really matter here, it's the simple fact that the modulus of steel is bigger than the modulus of titanium. Remember that the modulus is directly related to the stiffness? From this alone you can do the math, [(200-114)/200], to see that titanium will be 43% LESS rigid than steel, not more rigid as many claim.

Earlier I mentioned that geometry has an effect on stiffness; what if the geometry of the titanium fastener is different from the steel one it's replacing? Well, from this blog, you'll know that the titanium bolt would have to be bigger than the steel bolt to have a chance at being stiffer. But for most fasteners, there's simply no room to change the geometry: the bolt can't get bigger and still fit in the hole. For the majority of hardware on the bike, titanium bolts are just geometric copies of the steel bolt they are replacing. Those will always be less rigid.

A Practical Example:

Even when there's opportunity to change the bolt geometry, it's likely not enough to overcome the reduction in modulus of titanium vs steel. Let's look at the bolts pictured below. A while back a company claimed in their Instagram post that the stock steel KTM mount bolt "gives the front end flex and a vague feeling" because it's relieved in the middle. But their titanium bolt provides a "more responsive feel and more traction" because it's stiffer. But is it really?

Relieved steel bolt vs constant titanium bolt
Some bolts do have room to change the geometry, but is it enough to make a difference?

Well, making the titanium bolt with a constant cross-section vs. a relieved geometry is going to increase the stiffness. But that change still doesn't offset the modulus reduction enough to make it stiffer than the stock steel bolt. You can easily calculate the stiffness difference in tension between the two knowing the differences in size. It's just the cross-sectional area multiplied by the material modulus:

Bolt Tension Stiffness Calculations

So, the titanium bolt that was claimed to be stiffer than the steel bolt is actually 13% less stiff! Now that's just tension, but what about bending? Bending is a little harder to calculate due to the variance in cross-section across the length of the bolt, but we can simulate it with some basic FEA (finite element analysis):

Bolt bending stiffness analysis
FEA bending simulation of both bolts

The FEA results revel that the titanium bolt is actually about 15% more compliant in bending than the stock steel bolt. Once again, that's not stiffer!

Except in unique (and highly unlikely) circumstances, switching from steel hardware to titanium will always make the bike less rigid due to the drop in material modulus. And, if you've read my blog post on bolt torque, you'll see the material change of the fastener doesn't much matter one way or the other. For most bolted joints, the material the bolt is made from is irrelevant to the feel of the bike because all it's doing is tying two other parts together. The bolt itself doesn't have much of anything to do with the flex of the whole system, it's just the parts it's holding together that matter. So in most cases, switching from steel to titanium hardware will have no noticeable effect on feel one way or the other.

Hopefully this gives you some more understanding of the materials used in our sport. Up next, we'll dive into stiffness (flex, compliance, rigidity) in more detail. That blog post is coming soon!

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Comments (5)

WHAT KIND OF BIT SHOULD I USE TO DRILL AND TAP AN OUTPUT SHAFT ON A POLORIS RZR

I don't know...the VitalMX crowd seems to know more. Joking, joking.

Lots of very interesting and useful info in this post! Well done.

Great post as always. 7075 alo has better shear strength

Good read, and also explained very well

Great post thanks for sharing!

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