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

Arrangement for supplying cooling air to a turbine casing of an aircraft gas turbine

Patent 5482431 Issued on January 9, 1996. Estimated Expiration Date: Icon_subject August 4, 2014. 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

2584899

3527053

3527054

Cooling apparatus for split shaft gas turbine
Patent #: 4034558
Issued on: 07/12/1977
Inventor: Korta ,   et al.

Multi-stage turbine with interstage spacer-manifold for coolant flow
Patent #: 4079587
Issued on: 03/21/1978
Inventor: Nordstrom ,   et al.

Coolant flow metering device
Patent #: 4109864
Issued on: 08/29/1978
Inventor: Clayton

Cooling apparatus for a bearing in a gas turbine
Patent #: 4156342
Issued on: 05/29/1979
Inventor: Korta ,   et al.

Turbine intermediate case
Patent #: 4369016
Issued on: 01/18/1983
Inventor: Dennison

Air cooler for providing buffer air to a bearing compartment
Patent #: 4542623
Issued on: 09/24/1985
Inventor: Hovan ,   et al.

Air cooler for providing buffer air to a bearing compartment
Patent #: 4645415
Issued on: 02/24/1987
Inventor: Hovan ,   et al.

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Inventor

Assignee

Application

No. 284476 filed on 08/04/1994

US Classes:

415/111, For shaft sealing, packing, lubricating or bearing means60/39.83, Cooling of auxiliary components415/116WITH DIVERSELY ORIENTED INLET OR ADDITIONAL INLET FOR DIVERSE FLUID (E.G., HEATING, COOLING OR MIXED WORKING FLUID, ETC.)

Examiners

Primary: Look, Edward K.
Assistant: Larson, James A.

Attorney, Agent or Firm

Foreign Patent References

  • 2113429 DE. 09/20/1972
  • 2089439 GB. 06/20/1982

International Class

F01D 025/12

Foreign Application Priority Data

1992-02-04 DE

Abstract

The wall space and the mounting space for turbine bearings in the casing of an aircraft gas turbine are each supplied with cooling air via a separate pipe, a first cooling-air pipe opening into the wall space and a second cooling-air pipe extending through the wall space and opening in the mounting space. To ensure that the respective space continues to be supplied with cooling air even if one of the two pipes breaks, the cooling-air pipe extending through the wall space and opening into the mounting space has air overflow openings in the region of the wall space.

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