Discussion Overview
The discussion revolves around sealing options for a turbojet shaft operating under extremely high temperatures and pressures. Participants explore various sealing technologies suitable for high-performance applications in turbomachinery, particularly in the context of a combustor seal with unique design constraints.
Discussion Character
- Technical explanation
- Debate/contested
- Experimental/applied
Main Points Raised
- One participant suggests that aside from brush and labby seals, other sealing options for high temperatures and pressures need to be considered.
- Another participant argues that carbon seals, either radial or face types, are likely the best options, but notes potential issues with seal delta P.
- A participant expresses concern about high leakage rates with labby seals and questions the suitability of carbon face seals for the temperature range involved.
- There is a suggestion to potentially relocate the seal away from the hot area by modifying the shaft design.
- Participants discuss the possibility of using cooling schemes to manage temperatures around the seal.
- One participant highlights the challenge of finding suppliers that meet the high-temperature requirements for seals in high-performance applications.
- A question is raised about the feasibility of routing high-pressure bleed air through a cooler before directing it back to the seal area.
Areas of Agreement / Disagreement
Participants express differing views on the effectiveness of various sealing options, with no consensus reached on the best approach. Concerns about leakage rates and temperature limits remain unresolved.
Contextual Notes
Participants mention specific challenges related to the unique shape of the shaft and the high surface velocities involved, which may limit the effectiveness of certain sealing technologies. The discussion also reflects a lack of clarity regarding the definitions of high temperature in the context of seal suppliers.
Who May Find This Useful
Engineers and professionals involved in turbomachinery design, particularly those focused on sealing technologies in high-temperature and high-pressure environments.