Patents Assigned to Norwalk-Turbo, Inc.
  • Patent number: 4057371
    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. Through the direct close coupling and centerline mounting of the gas turbine exhaust casing for free and uniform heat expansion, alignment between stationary and rotating parts of the power turbine and compressor is maintained free from mechanical problems. The compressor stage assembly elements are conveniently interfitted together in the vertically split compressor casing by means of compression bolts minimizing fastening means. Bearings and oil seals are fed by an integrated lubrication and sealing oil system utilizing a compact oil distribution manifold assembly incorporating a quick filter change structure. The turbine fuel distribution system includes means permitting ready replacement and maintenance of individual fuel nozzles without disassembly of the entire fuel nozzle system.
    Type: Grant
    Filed: May 3, 1974
    Date of Patent: November 8, 1977
    Assignee: Norwalk-Turbo Inc.
    Inventor: Karol Pilarczyk
  • Patent number: 4028888
    Abstract: A fuel distribution system for a gas turbine-compressor includes means permitting ready replacement and maintenance of individual fuel nozzles without disassembly of the entire fuel nozzle system. 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.
    Type: Grant
    Filed: April 25, 1975
    Date of Patent: June 14, 1977
    Assignee: Norwalk-Turbo Inc.
    Inventor: Karol Pilarczyk
  • Patent number: 3976165
    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. Through the direct close coupling and center-line mounting of the gas turbine exhaust casing for free and uniform heat expansion, alignment between stationary and rotating parts of the power turbine and compressor is maintained free from mechanical problems. Bearings and oil seals are fed by an integrated lubrication and a sealing oil system utilizing a compact oil distribution manifold assembly incorporating a quick filter change structure. 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.
    Type: Grant
    Filed: April 25, 1975
    Date of Patent: August 24, 1976
    Assignee: Norwalk-Turbo, Inc.
    Inventor: Karol Pilarczyk
  • Patent number: 3942908
    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.
    Type: Grant
    Filed: April 25, 1975
    Date of Patent: March 9, 1976
    Assignee: Norwalk-Turbo, Inc.
    Inventor: Karol Pilarczyk