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

Bearing case support arrangement

Patent 5810558 Issued on September 22, 1998. Estimated Expiration Date: Icon_subject August 7, 2016. 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

2879092

Support arrangements for turbomachines
Patent #: 3937433
Issued on: 02/10/1976
Inventor: Portaleoni

Insulated coupling
Patent #: 4407602
Issued on: 10/04/1983
Inventor: Terry, Jr.

Improvements in or relating to gas turbine engines
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Issued on: 01/05/1988
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Inventor: Meron

Support arrangement for a space based cryogenic vessel
Patent #: 5012948
Issued on: 05/07/1991
Inventor: Van Den Bergh

Disk drive unit
Patent #: 5035396
Issued on: 07/30/1991
Inventor: Krum, et al.

Rotary reactor and lifter assembly
Patent #: 5040973
Issued on: 08/20/1991
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Mounting assembly
Patent #: 5090198
Issued on: 02/25/1992
Inventor: Nightingale, et al.

Impingement manifold
Patent #: 5100291
Issued on: 03/31/1992
Inventor: Glover

More ...

Inventor

Assignee

Application

No. 693439 filed on 08/07/1996

US Classes:

415/213.1, Casing with mounting means403/335INTERCONNECTED FLANGES OR SHOULDERS

Examiners

Primary: Kwon, John T.

Attorney, Agent or Firm

Foreign Patent References

  • 426886 CH. 06/11/1967
  • 777598 GB. 06/11/2012
  • 913375 GB. 12/11/1962
  • 2284148 GB. 05/11/1995

International Class

F01D 025/26

Abstract

The present invention relates to turbomachines and to a support for the bearing casing used in such machines. One end of a turbomachine housing is rigidly supported by a support member while the second end is supported by the inboard end of a bearing case. The inboard end of the bearing case is supported by an inboard support which permits horizontal movement of the bearing case in a direction parallel to the turbomachine shaft. The outboard support has a flange on which the bearing case rests and a base connected to and positioned below the flange. The flange contains flange bores through which rods attached on their first end to and protruding downwardly from the bearing case pass. The rods are optionally prevented from moving upwardly through the flange bore by a retainer, such as a nut or nut and washer combination, which is attached to the rod's second end. The retainer is mounted on the rod so that a gap is created between the upper surface of the retainer and the bottom surface of the flange. The support can further include a spacer mounted on the rod inside the flange bore and fitted between the retainer and the bearing case. The spacer has a length greater than the thickness of the flange and, thus, defines the size of the gap. The gap permits limited upward vertical movement of the bearing case. In this manner, the outboard support element maintains the alignment of the bearing case with the turbine shaft during operation of the turbomachine at elevated temperatures when differential heating of the supports causes them to undergo unequal vertical expansion.

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