Bi-material Sealing Interface for Space-Based Life Support Systems

Project number: 
21065
Sponsor: 
Honeywell Aerospace
Academic year: 
2020-2021
Project Goal: Design a serviceable high-temperature metal-to-ceramic seal for Honeywell's life support system aboard the International Space Station.

Long-distance space travel is possible with a closed-loop oxygen regeneration system that restores CO2 into breathable air. While this can be achieved using methane pyrolysis, conventional sealing designs cannot handle the required elevated temperatures of approximately 500 degrees Celsius. A better seal would improve this process.

The team designed a mechanical seal for the ceramic cylinder in the methane pyrolysis reactor. It uses Inconel and silicon nitride materials, capable of handling temperatures well above the requirement. Parametric modeling software facilitated the design, which was then verified with finite element analysis tools.

To minimize leakage due to thermal expansion, the metal interface uses a specific locking geometry and an Inconel 718 gasket. This provides an interface that is easy to service, resistant to changes in temperature and ensures a long and reliable service life

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