Fluidic sealing for turbomachinery

Rotary kinetic fluid motors or pumps – With means for re-entry of working fluid to blade set – Re-entry working fluid joins inlet working fluid upstream of...

Reexamination Certificate

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C415S057400, C415S058700

Reexamination Certificate

active

08052375

ABSTRACT:
Disclosed is a seal for turbomachinery including a seal face locatable between a first turbomachinery component and a second turbomachinery component. At least one fluid channel extends through the seal. The at least one fluid channel is capable of injecting fluid flow between the first turbomachinery component and the second turbomachinery component at the seal face thereby disrupting a leakage flow between the first turbomachinery component and the second turbomachinery component. Further disclosed is a turbomachine utilizing the seal.

REFERENCES:
patent: 5282718 (1994-02-01), Koff et al.
patent: 5308225 (1994-05-01), Koff et al.
patent: 5431533 (1995-07-01), Hobbs
patent: 5474417 (1995-12-01), Privett et al.
patent: 5607284 (1997-03-01), Byrne et al.
patent: 2006/0110247 (2006-05-01), Nelson et al.

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