Stall detector and surge prevention feature for a gas turbine engine

• US 4,507,915 A
• Filed: 01/25/1984
• Issued: 04/02/1985
• Est. Priority Date: 04/30/1981
• Status: Expired due to Fees

• Current Assignee: Allied Corp. (Honeywell International Inc.)
• Original Assignee: Allied Corp. (Honeywell International Inc.)
• Inventors: Evans, Rowland M.
• Primary Examiner(s): Casaregola, Louis J.
• Application Number:
  US06/573,542
• Time in Patent Office: 433 Days
• Field of Search: 60/39.281
• US Class Current: 60/39.281
• CPC Class Codes: F02C 9/28 Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed F02C9/30 - F02C9/38, F02C9/44 take precedence
• CPC Class Codes: F05D 2270/04 to control acceleration (u)
• CPC Class Codes: F05D 2270/101 Compressor surge or stall

Abstract

A proportional fuel fuel control (11) regulates the fuel flow (Wf) from a hydromechanical unit (36) based upon an error signal (E) representing the difference between a demanded speed signal (Nd) and an actual speed signal (Nh). The demanded speed signal (Nd) is generated by an integrator (32) as the time integral of the least of a plurality of acceleration terms (Aa, Ab, Ac, Ad) selected by a select low gate (38). The demanded acceleration term (Aa) is generated by junction (26) as the difference between the demanded signal (Nd) and a scheduled speed signal (Ngs). Stress acceleration terms (Ac, Ad) are generated by junctions (48, 50) and scheduling means (42, 44) which form stress limiter circuits. A stall acceleration term (Ab, is generated by a junction (46) and a scheduling means (40) which form a stall prevention feature.

Claims

1. A fuel control system for a gas turbine engine comprising:

means for generating an actual speed signal proportional to the actual turbine speed of the gas turbine engine;

means for generating a scheduled speed signal proportional to a desired output power;

means for generating a demanded speed signal proportional to the time integral of a difference signal;

means for generating said difference signal proportional to the difference between said scheduled speed signal and said demanded speed signal;

means for generating an error signal proportional to the difference between said demanded speed signal and said actual speed signal;

means for controlling the fuel flow to the gas turbine engine as a function of said error signal;

means responsive to the actual speed signal and the demanded speed signal for generating a stall factor as a function of the difference between actual speed signal and the demanded speed signal and indicative of the degree of stall the engine is experiencing; and

means, responsive to the stall factor, to further control fuel flow to the gas turbine engine.

2. The fuel control system as defined in claim 1 wherein:

said stall factor is generated as a function of the difference between the demanded speed signal and the actual speed signal.

3. A fuel control system as defined in claim 2 which further includes:

means for modifying the rate of change of the demanded speed signal as a function of the stall factor.

4. A fuel control system as defined in claim 3 wherein said means for modifying the rate of change of the demanded speed signal includes:

means for generating a multiplicative factor as a function of the stall factor; and

means for multiplying said multiplicative factor by an acceleration limit to modify the said limit before it is input to the comparator to limit the rate of change of said demanded speed.

5. A fuel control system as defined in claim 4 wherein:

said multiplicative factor is a function of the degree of stall the engine is experiencing such that no modification of the acceleration limit is scheduled if the stall factor indicates that the engine is substantially on an acceleration schedule.

6. A fuel control system as defined in claim 5 wherein:

said multiplicative factor is a function of the degree of stall the engine is experiencing such that a fractional modification is scheduled if the stall factor indicates the engine is off the acceleration schedule.

7. A fuel control system as defined in claim 6, whrein:

said multiplicative factor is a function of the degree of stall the engine is experiencing such that a zero acceleration is scheduled if the stall factor indicates the engine is in danger of experiencing a mild surge condition.

8. A fuel control system as defined in claim 7, wherein:

said multiplicative factor is a function of the degree of stall the engine is experiencing such that a deceleration is scheduled if the stall factor indicates the engine is in danger of experiencing a total surge condition.

9. A fuel control system as defined in claim 3, wherein:

said means for modifying the rate of change of the demanded speed signal includes modifying said signal as a function of at least one other engine operating parameter.

10. A fuel control system as defined in claim 9, wherein:

said other engine operating paramenter is actual engine speed corrected for temperature.

11. A fuel control system as defined in claim 10, wherein:

said modification is proportional to the change in fuel/air ratio as a function of corrected engine speed.

12. A fuel control system as defined in claim 11, wherein:

said modification is proportional to the change in the acceleration limit as a function of corrected engine speed.