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

Diffuser with controlled diffused air discharge

Patent 5632141 Issued on May 27, 1997. Estimated Expiration Date: Icon_subject September 9, 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

2520697

3394543

3777489

Combustor diffuser
Patent #: 4796429
Issued on: 01/10/1989
Inventor: Verdouw

Combustor inner passage with forward bleed openings Patent #: 5187931
Issued on: 02/23/1993
Inventor: Taylor

Inventors

Application

No. 303795 filed on 09/09/1994

US Classes:

60/782, Having bleed air to cool or heat motor or component thereof (e.g., active clearance control, etc.)60/751, Having diffuser for air inlet60/785Air bleed

Examiners

Primary: Thorpe, Timothy S.

Attorney, Agent or Firm

Foreign Patent References

  • 738006 GB 10/13/2012

International Class

F02C 006/08

Abstract

A gas turbine engine diffuser case construction is described that increases the amount of available discharge air for service applications compared to the prior art while reducing downstream component distortion and degradation. The diffuser case has passageways for diffused air that connect a diffused air region to a manifold. At least one orifice is located at the end of each of the passageways in the diffused air region. The size of the orifices controls the amount of air that is discharged from the diffused air region to the manifold. Diffused compressor air collects in the manifold and is then extracted from the manifold as needed for engine or service applications. The size and location of the orifices in the diffuser radially and circumferentially control the rate of discharge of the diffused air from the diffuser before the air enters the combustor region. The ability to influence the flow of air at particular locations around the combustor helps the designer to improve cooling uniformity.

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