kclim
Materials
- Jul 2, 2002
- 168
To do with the fabrication of a valve seat ring
The material in question is C62700 (admiralty bronze)
Approximate composition
Cu 80%, Al 10%, Fe 5%, Ni 5%, Zn 0.2%
All other elements below 0.1%
The product was in round bar form (extruded) with 39 mm diameter
The bar was then rolled into a ring, approximately 46 (~1200 mm) inches in diameter, with the ends being welded together.
The following describes the (post weld) heat treatment the whole ring was subject to
- Held at 650 C for 1 hour
- Quenched in water – 600 to 300 C (presumably quench to prevent gamma 2 phase formation)
- Slow cool (air) from 300 C to room temp
At this point cracks were found in the ring upon closer inspection.
Unfortunately, we could not determine when the cracks had arisen as no inspection had been performed up to that point.
The cracks were oriented circumferentially (around the larger ring, not the cross section) and went through the welded region but did not appear to be associated with the welding.
Tried performing some metallography – took a section which profiled the crack depth (which was more than 10 mm deep). The sample was etched in a 5% FeCl3/HCl/ethanol solution. See linked images:
General Microstructure
Showing cracking
Close up of cracking
From what I have researched & observed,
Microstructure appears to be consistent with aluminium bronze – alpha phase with interspersed kappa phase.
Cracks appear to be predominantly integranular (intercellular? between the islands of pure alpha phase).
What I am trying to determine is:
How long have the cracks been present?
Is it possible to tell, just from the microstructures? Were they present before the quench?
What is the damage mechanism?
I’m leaning towards either a quench associated damage mechanism (hydrogen embrittlement?) or a rolling defect-associated mechanism.
Any leads/comments would be greatly appreciated.
The material in question is C62700 (admiralty bronze)
Approximate composition
Cu 80%, Al 10%, Fe 5%, Ni 5%, Zn 0.2%
All other elements below 0.1%
The product was in round bar form (extruded) with 39 mm diameter
The bar was then rolled into a ring, approximately 46 (~1200 mm) inches in diameter, with the ends being welded together.
The following describes the (post weld) heat treatment the whole ring was subject to
- Held at 650 C for 1 hour
- Quenched in water – 600 to 300 C (presumably quench to prevent gamma 2 phase formation)
- Slow cool (air) from 300 C to room temp
At this point cracks were found in the ring upon closer inspection.
Unfortunately, we could not determine when the cracks had arisen as no inspection had been performed up to that point.
The cracks were oriented circumferentially (around the larger ring, not the cross section) and went through the welded region but did not appear to be associated with the welding.
Tried performing some metallography – took a section which profiled the crack depth (which was more than 10 mm deep). The sample was etched in a 5% FeCl3/HCl/ethanol solution. See linked images:
General Microstructure
Showing cracking
Close up of cracking
From what I have researched & observed,
Microstructure appears to be consistent with aluminium bronze – alpha phase with interspersed kappa phase.
Cracks appear to be predominantly integranular (intercellular? between the islands of pure alpha phase).
What I am trying to determine is:
How long have the cracks been present?
Is it possible to tell, just from the microstructures? Were they present before the quench?
What is the damage mechanism?
I’m leaning towards either a quench associated damage mechanism (hydrogen embrittlement?) or a rolling defect-associated mechanism.
Any leads/comments would be greatly appreciated.