U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Turbine installation, especially steam turbine installation

Patent 6988869 Issued on January 24, 2006. Estimated Expiration Date: Icon_subject September 25, 2023. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

2933893

3464654

3837164

Turboset support
Patent #: 4204804
Issued on: 05/27/1980
Inventor: Woodger

Gas turbine construction and method of controlling the labyrinth seal clearance automatically and continuously
Patent #: 4405283
Issued on: 09/20/1983
Inventor: Owsianny

Multi-cylinder steam turbine set
Patent #: 5051061
Issued on: 09/24/1991
Inventor: Meylan

Method and a device in a rotating machine
Patent #: 5330320
Issued on: 07/19/1994
Inventor: Mansson

Turbine plant having a thrust element, and thrust element Patent #: 6092986
Issued on: 07/25/2000
Inventor: Oeynhausen, et al.

Inventor

Assignee

Application

No. 10670804 filed on 09/25/2003

US Classes:

415/104, WITH SHAFT CONNECTED FLUID FORCE SUBJECTED THRUST BALANCING SURFACE415/108, CASING AND SPACED HOUSING WITH SPACE VENTED TO WORKING FLUID415/119, WITH SOUND OR VIBRATORY WAVE ABSORBING OR PREVENTING MEANS OR ARRANGEMENT415/134, INCLUDING THERMAL EXPANSION JOINT415/142, SHAFT BEARING COMBINED WITH OR RETAINED BY ARM OR VANE IN SURROUNDING WORKING FLUID SPACE415/229BEARING, SEAL, OR LINER BETWEEN SHAFT OR SHAFT SLEEVE AND STATIC PART

Examiners

Primary: Look, Edward K.

Foreign Patent References

  • 1 216 322 DE 05/01/1966
  • 35 22 916 DE 01/01/1987
  • 196 29 933 DE 09/01/1997
  • 0 601 825 EP 06/01/1994
  • 1 145 612 GB 03/01/1969

International Class

F01D 25/28

Abstract

The invention relates to a turbine installation, especially a steam turbine installation. The inventive turbine installation comprises at least two partial turbines, each of the partial turbines having a rotor disk that extends along the main axis. Said rotor disks are rigidly interlinked to a shafting. At least one of the partial turbines has an inner housing that concentrically encloses the rotor disk and that is mounted so as to be axially displaceable in a bearing area. To allow for an axial displacement a push element transmits the axial force and is linked with the inner housing. In order to allow the inner housing to be axially displaced as easily as possible, the bearing area has a bearing device with a static friction and/or sliding friction that is so low that the axial misplacement that spontaneously occurs when the static friction is overcome during displacement of the inner housing is smaller 2 mm.

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