Zero running clearance centrifugal compressor

Rotary kinetic fluid motors or pumps – Runner or blade selectively adjustable relative to casing – Axially adjusted

Reexamination Certificate

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C415S173200, C060S803000

Reexamination Certificate

active

07824151

ABSTRACT:
A turbine engine includes an engine housing enclosing: a centrifugal compressor having a rotor; at least one centrifugal compressor bore mounted to the rotor; at least one blade mounted to each of the at least one centrifugal bore and disposed proximate to at least one static wall; a turbine disposed in connection with the centrifugal compressor; a thrust bearing disposed in connection with the rotor; and means for moving said rotor with reference to the at least one static wall attached to the thrust bearing.

REFERENCES:
patent: 2977758 (1961-04-01), Haworth et al.
patent: 3045894 (1962-07-01), Ross
patent: 5263816 (1993-11-01), Weimer et al.
patent: 6058791 (2000-05-01), Brunet
patent: 6273671 (2001-08-01), Ress, Jr.
patent: 6692222 (2004-02-01), Prinz et al.
patent: 2006/0122798 (2006-06-01), Teolis et al.
patent: 2007/0043497 (2007-02-01), Leogrande et al.

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