Troubleshooting Platinum & Iridium Loops: Reasons and Solutions

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Discussion Overview

The discussion revolves around the failure of loops made from an 85% platinum and 15% iridium alloy after several sterilization cycles. Participants explore potential reasons for the breakdown, including material properties and environmental factors, while also seeking additional information about the loops' dimensions, heat treatment, and intended use.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested

Main Points Raised

  • One participant notes the loops break down after 3 or 4 sterilization cycles and seeks advice on the reasons and solutions.
  • Another participant requests more information about the loops, including dimensions, heat treatment details, and the mode of failure, suggesting that the quality of the alloy and trace impurities may be relevant.
  • It is proposed that the fracture could be due to embrittlement from high-temperature oxidation of the grain boundaries.
  • Some participants discuss the conditions in rocket motors, suggesting that the environment may be oxidation deficient, which could affect the alloy's performance.
  • There is a mention of oxygen attack on grain boundaries being a known issue for refractory metals and alloys, with a specific reference to hydrazine fuel engines and their reducing atmospheres.
  • Concerns are raised about the oxidation resistance of the Pt-Ir alloy at high temperatures, despite its general reputation for corrosion resistance.
  • A participant expresses uncertainty about the oxidation issue due to the alloy's properties, indicating a need for more information on impurities and their effects.

Areas of Agreement / Disagreement

Participants express multiple competing views regarding the causes of the failure, particularly around the role of oxidation and embrittlement. The discussion remains unresolved, with no consensus reached on the exact reasons for the breakdown of the loops.

Contextual Notes

Participants highlight the importance of additional information regarding the loops' composition, dimensions, and intended use, which may influence the analysis of the failure. The discussion also reflects uncertainty about the effects of impurities and the specific environmental conditions affecting the alloy's performance.

wajdi
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HI
I have loops made of 85% platinum and 15% iridium. It brokes down after 3 or 4 steralization cycles (by getting red on Bunsen Burner) please advice reason and solution
thanks
 
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To diagnose a reason, if lucky, we would need more information. Can you specify the dimensions of the loops, the details of the heat treatment and the mode of failure? Also, the quality of the alloy is important - can you tell us the complete composition, including trace impurity levels?

As for providing a solution, we need to know what you are using the hoops for and why you are sterilizing them?

I've heard of Pt-Ir screens being used in rocket engine chambers where temperatures get to be close to 1000C. There's also one or two reports of embrittlement at high temperatures due to Group III impurities. I may have something bookmarked on my work computer.
 
The fracture could be due to embrittlement due to high temperature oxidation of the grain boundaries.

In rocket motors, the environment is likely oxidation deficient. In LOX/LH2 motors, the working fluid is usually slightly enriched in H2 to enhance specific impulse, Isp.
 
Astronuc said:
The fracture could be due to embrittlement due to high temperature oxidation of the grain boundaries.
"It has to be grain boundary embrittlement" (for brittle failure) - that was my first thought too.

In rocket motors, the environment is likely oxidation deficient. In LOX/LH2 motors, the working fluid is usually slightly enriched in H2 to enhance specific impulse, Isp.
I think the stuff I'd read was with hydrazine fuel engines - again a highly reducing atmosphere, that serves as an oxidation inhibitor. So again, I think you're right that it's probably oxidation related embrittlement. The reason I was a little wary to suggest oxidation is because of the nature of the alloy. Pt-15%Ir is probably the most corrosion resistant alloy there is. That's the reason the SI uses it as a Pt-Ir block as the standard measure of the kilogram (and until some years ago, used it as the standard measure of the meter as well).

(long time, no see, Astro - you been traveling?)
 
Last edited:
Gokul43201 said:
"It has to be grain boundary embrittlement" (for brittle failure) - that was my first thought too.
Oxygen attack on the grain boundaries is a notorious problem for refractory metals and alloys.

Gokul43201 said:
I think the stuff I'd read was with hydrazine fuel engines - again a highly reducing atmosphere, that serves as an oxidation inhibitor. So again, I think you're right that it's probably oxidation related embrittlement. The reason I was a little wary to suggest oxidation is because of the nature of the alloy. Pt-15%Ir is probably the most corrosion resistant alloy there is. That's the reason the SI uses it as a Pt-Ir block as the standard measure of the kilogram (and until some years ago, used it as the standard measure of the meter as well).
At room or low temperature, that is very true. At high temperature, oxidation of grain boundaries is a problem. Good point about the impurities. I hope you post whatever you have bookmarked on your computer.

Gokul43201 said:
(long time, no see, Astro - you been traveling?)
Yep.
 
Astronuc said:
I hope you post whatever you have bookmarked on your computer.
Can't find it Astro. Guess I didn't bookmark it after all. :frown:
 

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