Gas turbine driven high speed centrifugal compressor unit

Details Gas turbine driven high speed centrifugal compressor unit Gas turbine driven high speed centrifugal compressor unit

1975-04-25

1976-03-09

Raduazo, Henry F.

Rotary kinetic fluid motors or pumps

Working fluid passage or distributing means associated with...

Plural rigidly related blade sets

415219A, 415219C, F04D 2944

Patent

active

039429083

ABSTRACT:
A high speed centrifugal compressor is closely directly coupled to the power turbine of a two-shaft gas turbine having a gas generator section separate from its power turbine. The compressor stage assembly elements are conveniently interfitted together in the vertically split compressor casing by means of compression bolts minimizing fastening means. The gas turbine-compressor finds particularly useful application in areas where high power, compact, relatively maintenance-free units are required, as, for example, on offshore platforms in the natural gas industry.

REFERENCES:
patent: 1837873 (1931-12-01), MacMeeken
patent: 2474077 (1949-06-01), Trumpler
patent: 3044684 (1962-07-01), Fullemann
patent: 3051090 (1962-08-01), Zumbusch
patent: 3105632 (1963-10-01), Tanzberger
patent: 3188967 (1965-06-01), Glessner
patent: 3733145 (1973-05-01), Kaplansky et al.
patent: 3801217 (1974-04-01), Ryall et al.
patent: 3825368 (1974-07-01), Benjamin

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