Method and apparatus for acceleration limiting a gas turbine engine

• US 4,593,523 A
• Filed: 07/01/1983
• Issued: 06/10/1986
• Est. Priority Date: 12/17/1980
• Status: Expired due to Term

• Current Assignee: Allied Corp. (Honeywell International Inc.)
• Original Assignee: Allied Corp. (Honeywell International Inc.)
• Inventors: Hawes, David J.
• Primary Examiner(s): Casaregola, Louis J.
• Application Number:
  US06/510,124
• Time in Patent Office: 1,075 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 2270/042 by keeping it below damagingly high values

Abstract

A method and apparatus for acceleration limiting a gas turbine engine (10) is disclosed. A proportional 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 Ng. The demanded speed signal Nd is generated by an integrator (32) as the time integral of the difference between the demanded signal Nd and a scheduled speed signal Ngs. Additionally, the difference signal is limited between an upper limit A1 and a lower limit D1 prior to the integration by a comparator (28) and a limiter circuit (30). The acceleration limit, A1 is generated as a function of a nondimensional parameter ratio (dN/dt×N)/Wf.

Claims

1. In a fuel control system for a gas turbine engine including:

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 engine 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; and

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

an improvement comprising;

means for limiting said difference signal to a limit value; and

means for generating said limit value as a function of the fuel flow to the engine Wf, and the speed of the engine N;

said limit valve generating means including a memory device for storing a schedule of an acceleration parameter as function of engine speed, wherein said memory device stores values of the ratio (dN/dt×

N)/Wf.

2. A fuel control system as defined in claim 1 which further includes:

means for generating a correctional value to be combined with said limit value.

3. A fuel control system as defined in claim 2, wherein:

said correctional value is generated as a function of at least one of the group comprising;

ambient temperature To, variable geometry position Gp, ambient pressure Po, and bleed pressure Bp.

4. In a fuel control system for a gas turbine engine including:

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 engine 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 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; and

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

an improvement comprising;

means for limiting said difference signal to a limit value; and

means for generating said limit value as a function of the fuel flow to the engine Wf, and the speed of the engine N,

said limit value generating means including a memory device for storing a schedule of an acceleration parameter as function of engine speed, wherein said memory device stores values of the ratio (dN/dt)/Wf.

5. A fuel control system as defined in claim 4 which further includes:

means for generating a correctional value to be combined with said limit value.

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

said correctional value is generated as a function of at least one of the group comprising;

ambient temperature To, variable geometry position Gp, ambient pressure Po, and bleed pressure Bp.