# Carbon vs Aluminum Fuse

**URL:** <https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656>\
**Category:** Uncategorized\
**Created:** [November 14, 2024, 7:21pm UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656 "2024-11-14T19:21:42Z")\
**Posts on this page:** 17\
**Page:** 2

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**Author:** ![JohnVu](https://avatars.discourse-cdn.com/v4/letter/j/71c47a/32.png) [@JohnVu](https://forum.progressionproject.com/u/JohnVu)\
**Post date:** [November 20, 2024, 12:34am UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/21 "2024-11-20T00:34:49Z")

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Gong Titanium fuselage is 207 Euros!

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**Author:** ![Tomate](https://avatars.discourse-cdn.com/v4/letter/t/e47c2d/32.png) [@Tomate](https://forum.progressionproject.com/u/Tomate)\
**Post date:** [November 20, 2024, 6:03am UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/22 "2024-11-20T06:03:56Z")

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My titan fuselage from gong is way heavier than the aluminium counterpart

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**Author:** ![seawing](https://avatars.discourse-cdn.com/v4/letter/s/48db29/32.png) [@seawing](https://forum.progressionproject.com/u/seawing)\
**Post date:** [November 20, 2024, 6:13pm UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/23 "2024-11-20T18:13:59Z")

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Yeah a Ti fuse _could_ be lighter than an aluminum fuse if it used less material to produce a part of similar strength. The Gong Ti fuse is the same shape as the aluminum one, so it’s much heavier.

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**Author:** ![Kili2386](https://avatars.discourse-cdn.com/v4/letter/k/a9a28c/32.png) [@Kili2386](https://forum.progressionproject.com/u/Kili2386)\
**Post date:** [November 22, 2024, 1:02am UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/24 "2024-11-22T01:02:40Z")

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Sounds exactly like the Allure (French brand) fuse, Titanium between the front wing and the mast, and a carbon tube bonded for the tail. Description on their website justifies using carbon on the back of the fuse to save weight vs titanium. The wing to fuse connection is a flat mount with 4 screw, not to far from what Axis or AFS use.

 ![1000038225](https://canada1.discourse-cdn.com/flex030/uploads/progressionproject/original/2X/f/f95317a9c09cdb166363e69a29d22d8ca90870e8.jpeg)  
 ![1000038226](https://canada1.discourse-cdn.com/flex030/uploads/progressionproject/original/2X/d/d16d9c10f570185acbc6c986df7109a8fd02de31.png)

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**Author:** ![jondrums](https://avatars.discourse-cdn.com/v4/letter/j/7ea924/32.png) [@jondrums](https://forum.progressionproject.com/u/jondrums)\
**Post date:** [November 22, 2024, 6:46pm UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/25 "2024-11-22T18:46:59Z")

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YES! the allure fuse looks like the optimum to me. Wish I could get one for axis mast/wing or AFS mast/wing joint config. I think we may see this architecture more widespread

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**Author:** ![jondrums](https://avatars.discourse-cdn.com/v4/letter/j/7ea924/32.png) [@jondrums](https://forum.progressionproject.com/u/jondrums)\
**Post date:** [November 22, 2024, 6:50pm UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/26 "2024-11-22T18:50:51Z")

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Nobody mentioned yet about Titanium - perfect corrosion properties for salt water, and also compatible with carbon fiber direct joints. Aluminum is absolutely terrible on both properties, corrosion but also significant galvanic problems when joining with carbon. Magnesium and Steel are pretty much not an option. Stainless steel with appropriate corrosion properties sacrifices the structural properties.

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**Author:** ![TooMuchEpoxy](https://avatars.discourse-cdn.com/v4/letter/t/c5a1d2/32.png) [@TooMuchEpoxy](https://forum.progressionproject.com/u/TooMuchEpoxy)\
**Post date:** [November 22, 2024, 7:45pm UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/27 "2024-11-22T19:45:06Z")

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I duno man, I’m willing to die on a lot of hills to improve the industry and I find aluminum to be GREAT! Makes for a stiffer fuse than carbon at a lower cost and the corrosion is a non factor if you just throw on some clear bathroom silicon. A titanium fuse would cost more than my whole rig and realistically wouldn’t make anything stiffer - connections design and manufacturing tolerances are still the Achilles heel for stiffness

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**Author:** ![miamiwngr](https://avatars.discourse-cdn.com/v4/letter/m/f14d63/32.png) [@miamiwngr](https://forum.progressionproject.com/u/miamiwngr)\
**Post date:** [November 23, 2024, 5:29pm UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/28 "2024-11-23T17:29:24Z")

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![1000046303](https://canada1.discourse-cdn.com/flex030/uploads/progressionproject/original/2X/5/545bbd1db8e5099565fadfdd73214ca82e4624d5.jpeg)

Stainless/carbon combo vs alu full alu. Total weight of the full planes are very similar. Waiting for some wind so i can try the new KT

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**Author:** ![AnacortesRigging](https://yyz2.discourse-cdn.com/flex030/user_avatar/forum.progressionproject.com/anacortesrigging/32/4936_2.png) [@AnacortesRigging](https://forum.progressionproject.com/u/AnacortesRigging)\
**Post date:** [November 24, 2024, 8:01pm UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/29 "2024-11-24T20:01:43Z")

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New SailGP T-foils are machined titanium, not carbon composite. They hit 102kph top speed.

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**Author:** ![JohnVu](https://avatars.discourse-cdn.com/v4/letter/j/71c47a/32.png) [@JohnVu](https://forum.progressionproject.com/u/JohnVu)\
**Post date:** [November 25, 2024, 12:36am UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/30 "2024-11-25T00:36:38Z")

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Gong Titanium fuse is 450 Euros.  
It’s beefy, beautiful tolerance and fit.  
I have 2 of the V2 (~500g) and 1 of the the V3 (~600g).  
The bolts goes straight into Titanium, no helicoil.  
No corrosion to worry about (esp since I put them on and leave them on Cedrus Evolution aluminum adaptor).

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**Author:** ![Greg\_F](https://yyz2.discourse-cdn.com/flex030/user_avatar/forum.progressionproject.com/greg_f/32/2842_2.png) [@Greg\_F](https://forum.progressionproject.com/u/Greg_F)\
**Post date:** [December 12, 2024, 8:36pm UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/31 "2024-12-12T20:36:44Z")

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> [@Kili2386](#):
>
> Allure (French brand) fuse, Titanium between the front wing and the mast, and a carbon tube bonded for the tail. Description on their website justifies using carbon on the back of the fuse to save weight vs titanium. T

Hey John, will be interesting to hear how the aluminum adapter holds up over time. Although the titanium will not corrode, it is very noble so will setup a circuit with aluminum. Corrosion happens faster if the surface area of the aluminum is small compared to the Titanium which is true in your case. The anodization will provide insulation in theory to stop the connection, so hopefully that is enough, I’d really try to avoid scratching the surface of the aluminum foot.

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**Author:** ![jondrums](https://avatars.discourse-cdn.com/v4/letter/j/7ea924/32.png) [@jondrums](https://forum.progressionproject.com/u/jondrums)\
**Post date:** [December 13, 2024, 6:38pm UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/32 "2024-12-13T18:38:28Z")

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> [@Greg\_F](#):
>
> Hey John, will be interesting to hear how the aluminum adapter holds up over time

There would not be any aluminum at all. just titanium and carbon - that’s key.

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**Author:** ![Greg\_F](https://yyz2.discourse-cdn.com/flex030/user_avatar/forum.progressionproject.com/greg_f/32/2842_2.png) [@Greg\_F](https://forum.progressionproject.com/u/Greg_F)\
**Post date:** [December 13, 2024, 7:18pm UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/33 "2024-12-13T19:18:59Z")

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> [@JohnVu](#):
>
> s straight into Titan

You’re absolutely right John, I quoted the wrong post somehow.

Maybe it was another thread or the post was deleted - would have sworn I’d read someone talking about using a mast with an aluminum foot in a titanium fuselage.

That or I’ve just been breathing too much epoxy fumes!

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<div class="post-metadata">

**Author:** ![JohnVu](https://avatars.discourse-cdn.com/v4/letter/j/71c47a/32.png) [@JohnVu](https://forum.progressionproject.com/u/JohnVu)\
**Post date:** [December 13, 2024, 11:14pm UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/34 "2024-12-13T23:14:56Z")

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It’s not the fume lol.

Cedrus adapters are anodized aluminum.  
Yes I pay attention at not scratching the surface.

The Gong fuse I have are Titanium.

I put a small layer of dielectric grease in between the two.

The bolts are titanium going into stainless steel helicoils.

I didn’t think it would be enough reaction realistically to worry about Titanium-Aluminium reaction. But I’m no chemical engineer

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**Author:** ![Greg\_F](https://yyz2.discourse-cdn.com/flex030/user_avatar/forum.progressionproject.com/greg_f/32/2842_2.png) [@Greg\_F](https://forum.progressionproject.com/u/Greg_F)\
**Post date:** [December 13, 2024, 11:34pm UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/35 "2024-12-13T23:34:25Z")

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haha, yeah I see your original post now - I was just looking at the quote - so it’s at least a little bit the fumes affecting my brain!

yeah, between keeping up with the greasing and keeping the anodization in place I imagine you’ll get decent part life. There may still be a an electrical connection through the helicoils but hopefully factory applied coatings prevent that.

Please update us in 6-12 months on how the aluminium is looking!

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<div class="post-metadata">

**Author:** ![JohnVu](https://avatars.discourse-cdn.com/v4/letter/j/71c47a/32.png) [@JohnVu](https://forum.progressionproject.com/u/JohnVu)\
**Post date:** [December 13, 2024, 11:59pm UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/36 "2024-12-13T23:59:27Z")

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It’s been a year now (got the preproduction Evolution mast with their first Gong V2 connector) and there’s wear and grease everywhere so I don’t know the oxidation status. 🤣  
Never got stuck, and I leave them connected for weeks at a time.  
Fit is still snug and perfect.

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**Author:** ![Greg\_F](https://yyz2.discourse-cdn.com/flex030/user_avatar/forum.progressionproject.com/greg_f/32/2842_2.png) [@Greg\_F](https://forum.progressionproject.com/u/Greg_F)\
**Post date:** [December 16, 2024, 5:44pm UTC](https://forum.progressionproject.com/t/carbon-vs-aluminum-fuse/7656/37 "2024-12-16T17:44:22Z")

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Nice, good to know for anyone considering similar!

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