ClaudeMachining

Sniper or Shearer?

Did you bang her or not??

Sweeeeet!!

Cuuuuuuuuute!

It's not rocket science.... you have the electrical drawings....Making a harness is easy too.

Communication is the key.

Smh...

My dad was a mechanic. I was young and he gave me this advice : if you want to hate doing mechanics, buy cheap tools.

Understand what you're doing is always a better idea.

Do it with %, it's easier to do the math. let's say you mix at 32:1 and you have 15 litres of gas. 32:1 is a ratio so, 1/32= 0.03125 0.03125 x 15L = 0,469L or 469ml of oil

ANYTHING under 1 kilos is about 15$ Can to ship anywhere to USA. A crank is obviously more than 1 kilo but i guess the shipping would be about 30$

Driveline took care of my top end in less than 3 weeks. Since i wanted it ported, i waited for the new unplated batch, they ported it, send it to plating and it's almost ready to ship now.

Ok boss, i got it.

Your lack of scenitific background is showing. Trying to bully me doesnt change science. Numbers dont lies, your just a parrot.

I putted out all the numbers. I cant do better than that. I still wonder why Ti is used in airplanes, dam, they should call JT and ask him why they should use Chromo instead lol!

Then just make it the same weight as the chromo one and it will be as stiff. I posted all the data, i cant say munch more than that.

Titanium alloys : G (young modulus) : 110 to 119GPA D (density) : 4.4 to 4.5mg/m3 G/D (stiffness to weight ratio) 25-26.5 ChroMo Alloys: G: 150-245 D: 7.75 to 9 G/D : 19.35 to 27.2 I rest my case. Dont try to bully your way out JT. You know Shee and machining, fair enough, but we are talking engineering/material here, we are not in the same league.

The Ti chassis was way lighter if the tubes were the same.

Definition from the net: Specific modulus Specific modulus is a materials property consisting of the elastic modulus per mass density of a material. It is also known as the stiffness to weight ratio or specific stiffness. High specific modulus materials find wide application in aerospace applications where minimum structural weight is required. The dimensional analysis yields units of distance squared per time squared. So again, at the same weight, they will bent about the same.

You're not following hun?

Since it have a better G/D ratio, the Ti tube will be lighter. It will not have the same Dia or thinckness but IT WILL BE LIGHTER and as stiff as the chrome one. If you have 'fitting issue' ok. But if you want the lightest, Ti all the way. FFS guys, why do you think Ti is the material of choice in aeronautic??

You said in the SB : 'Take 1 inch tube same wall thickness in TI and chrom. Let me know what one flexes more' You just show me that you dont undertand at all. The Ti tube will weight a lot less. Make them the same weight and the Ti tube will flex less. That's what i mean when i say Ti p4p, will flex less than steel.

It's ok for you to correct me about what ever, but if we do it the other way around, it's braging. Ok, i'll try to remeber that.

Then shut up.