THRUST BEARING SYSTEM WITH INVERTED NON-CONTACTING DYNAMIC SEALS FOR GAS TURBINE ENGINE

A gas turbine engine includes a first non-contacting dynamic rotor seal interfaced with a spool, the first non-contacting dynamic seal operates to seal adjacent to an outer diameter and a second non-contacting dynamic rotor seal with respect to the spool, the second non-contacting dynamic seal opera...

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Bibliographische Detailangaben
1. Verfasser: CAPRARIO JOSEPH T
Format: Patent
Sprache:eng
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Zusammenfassung:A gas turbine engine includes a first non-contacting dynamic rotor seal interfaced with a spool, the first non-contacting dynamic seal operates to seal adjacent to an outer diameter and a second non-contacting dynamic rotor seal with respect to the spool, the second non-contacting dynamic seal operates to seal adjacent to an inner diameter.