mikeyanxu
Aerospace
- Oct 1, 2013
- 5
Had run across this type of questions a few times. There are a few standard methods at work (aircraft manufacture)and no one seems to question about it. Just follow the spec and do what is always be done, right?
[ul]
[li]For example, steel fastener in aluminum airframe. Cad plate fasteners, anodize aluminum, and wet dip fastener in primer upon installation.[/li]
[li]Steel rod end into flight control rods. Cad plated rod ends with aluminum flight control rods. Wet dip rod ends threads in primer upon installation.[/li]
[/ul]
Are the above methods adequate? Maybe, people still discover corrosion when tearing down the old airframe at the above locations.
Now, down to my own home project and I can decide what to do without an FAA approval, nice. Since I am an engineer, I would like to do it right. See the picture, it is a firearm project.
The upper receiver is anodized aluminum 6061, 7071 or maybe 7075, unknown temper.
The barrel is 8620 steel, heat treated. Parkerized or blued.
The barrel nut is steel, heat treated. Parkerized or buled.
The shim is stainless. Not known if it is passivated.
The end of the threaed section of upper receiver had been lapped/ground to produce a true perpenticular surface reference the thread. So, the anodize on the face is gone. It is bare aluminum with touch up "cold blue". I think it is a kind or touch up alodine.
So, the way it will be assembled, what anti-seize (or compound) should I use to avoid galvanic corrosion between the upper receiver and the barrel nut or between the receiver and the barrel?
Thanks.
[ul]
[li]For example, steel fastener in aluminum airframe. Cad plate fasteners, anodize aluminum, and wet dip fastener in primer upon installation.[/li]
[li]Steel rod end into flight control rods. Cad plated rod ends with aluminum flight control rods. Wet dip rod ends threads in primer upon installation.[/li]
[/ul]
Are the above methods adequate? Maybe, people still discover corrosion when tearing down the old airframe at the above locations.
Now, down to my own home project and I can decide what to do without an FAA approval, nice. Since I am an engineer, I would like to do it right. See the picture, it is a firearm project.
The upper receiver is anodized aluminum 6061, 7071 or maybe 7075, unknown temper.
The barrel is 8620 steel, heat treated. Parkerized or blued.
The barrel nut is steel, heat treated. Parkerized or buled.
The shim is stainless. Not known if it is passivated.
The end of the threaed section of upper receiver had been lapped/ground to produce a true perpenticular surface reference the thread. So, the anodize on the face is gone. It is bare aluminum with touch up "cold blue". I think it is a kind or touch up alodine.
So, the way it will be assembled, what anti-seize (or compound) should I use to avoid galvanic corrosion between the upper receiver and the barrel nut or between the receiver and the barrel?
Thanks.