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

Compressor stall and surge control using airflow asymmetry measurement

Patent 5915917 Issued on June 29, 1999. Estimated Expiration Date: Icon_subject November 2, 2015. 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

Engine surge prevention system
Patent #: 4550564
Issued on: 11/05/1985
Inventor: Callahan ,   et al.

Chuck for tool Patent #: 5340127
Issued on: 08/23/1994
Inventor: Martin

Inventors

Application

No. 676387 filed on 11/02/1995

US Classes:

415/1, METHOD OF OPERATION60/795, Bleed415/17, Plural diverse condition responsive (e.g., temperature and pressure, speed and level, etc.)415/27Of relief valve in branched pump discharge line

Examiners

Primary: Look, Edward K.
Assistant: Woo, Richard

Attorney, Agent or Firm

Foreign Patent References

  • 401211696 JP 08/13/1989

International Class

F01D 017/08

Abstract

A technique for controlling compressor stall and surge is disclosed. In a gas turbine engine, static pressure asymmetry is sensed at a plurality of locations along the circumference of the compressor inlet. Time rate of change of the mass flow in the compressor is also estimated using pressure measurements in the compressor. A signal processor uses these signals to modulate a compressor bleed valve responsive to the level of flow property asymmetry, the time rate of change of the annulus average flow to enhance operability of the compressor.

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