Device for controlling the rotational speed of turbo-jet engines

• US 4,171,613 A
• Filed: 10/12/1977
• Issued: 10/23/1979
• Est. Priority Date: 01/24/1977
• Status: Expired due to Term

• Current Assignee: Bodenseewerk Gerätetechnik Gmbh
• Original Assignee: Bodenseewerk Gerätetechnik Gmbh
• Inventors: Wust, Peter, Schmidt-Roedenbeck, Heiner
• Primary Examiner(s): Garrett, Robert E.
• Application Number:
  US05/841,594
• Time in Patent Office: 741 Days
• Field of Search: 60/39.28 R
• 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: F02C 9/32 characterised by throttling of fuel F02C9/38 takes precedence
• CPC Class Codes: F05D 2200/13 Product
• CPC Class Codes: G05B 11/01 electric

Abstract

The commanded rotational speed is compared with the actual rotational speed to produce a deviation signal. This deviation signal is multiplied by a coefficient which is determined by state variables (speed and intake pressure) of the engine and a proportional component plus an integral component of the multiplication product is employed as a control signal. This control signal is checked to make sure that it is outside critical engine states associated with the actual performance of the engine. On this control signal is superposed a signal representing the steady-state fuel flow associated with the commanded rotary speed (or under some circumstances the actual rotary speed) to determine the fuel flow rate to the engine.

Claims

1. An apparatus for controlling the rotational speed of an aircraft turbo-jet engine, which engine has a compressor, said apparatus comprising:

a commanded value generator providing a commanded rotational speed signal representing a commanded rotational speed of said compressor;

compressor speed means for providing an actual rotational speed signal representing the actual rotational speed of said compressor;

difference means connected to the commanded value generator and to the compressor speed means to receive said signals therefrom and to form a control deviation signal from the difference of said signals;

controller means connected to said difference means to receive said control deviation signal, said controller means providing a controller output signal from said control deviation signal;

function generator means for storing the relation between fuel flow rates and rotational speeds of said compressor in accordance with the steady-state characteristics of the turbo-jet engine and for providing a fuel flow output signal as a function of a rotational speed input signal to the function generator means;

combining means connected to the controller means and to the function generator means for combining said controller output signal from said controller means and said fuel flow output signal from said function generator means as an engine fuel flow rate signal;

a fuel control unit for metering the fuel supplied to the engine in accordance with an input signal applied thereto; and

connecting means connecting said combining means and said fuel control unit for applying said engine fuel flow rate signal to said fuel control unit as said input signal to said fuel control unit, said connecting means including limiting means for limiting said engine fuel flow rate signals such that sufficient distance from the surge line is ensured;

said apparatus being characterized by;

means connecting said commanded value generator and said function generator means for applying said commanded rotational speed signal to said function generator means as said rotational speed input signal.

2. An apparatus as set forth in claim 1, and wherein said engine supplies signals representing critical engine parameters, including comparison means connected to said engine to receive said supplied signals for comparing said critical parameters to associated threshold values and for providing difference signals, means connected to said comparison means for providing limit control signals from said difference signals, and minimum selector means connected to the last mentioned means and to said controller means to receive said limit control signals and said controller output signal to produce a limiter output signal representing the respective smallest signal applied, said minimum selector means being connected between the function generator means and the combining means to supply only said limiter output signal to said combining means, further characterized by:

means connecting said compressor speed means and said function generator means for applying said actual rotational speed signal as an input signal to said function generator means;

said function generator means providing another output signal representing the steady-state fuel flow associated with the actual rotational speed;

logic means connected to said means for providing limit control signals and to controller means and responding to any of said limit control signals becoming smaller than said controller output signal;

said connecting means being connected to said logic means and including means for providing an alternative engine fuel flow rate signal, applying said alternative engine fuel flow rate signal to said fuel control unit through said limiting means upon said logic means so responding.

3. An apparatus as set forth in claim 2, wherein said controller means comprises:

coefficient means which so receives said control deviation signal and provides a first component of said controller output signal proportional to said control deviation signal;

integrating means connected to said coefficient means for providing a second component of said controller output signal proportional to the time integral of said control deviation signal;

summer means connected to said coefficient means and said integrating means for combining said first and second components to provide said controller output signal; and

means, connected between said coefficient means and said integrating means and connected to receive said control deviation signal, for disabling said integrating means when said control deviation signal exceeds a given threshold.

4. An apparatus as set forth in claim 3, wherein the last mentioned means comprises logic means connected to said means for providing control limit signals and to said summer means for disabling said integrating means in the event that any of said limit control signals becomes smaller than said controller output signal and in the event that said control deviation signal exceeds said threshold.

5. An apparatus as set forth in claim 1, wherein said controller means comprises:

coefficient means which so receives said control deviation signal and provides a first component of said controller output signal proportional to said control deviation signal;

integrating means connected to said coefficient means for providing a second component of said controller output signal proportional to the time integral of said control deviation signal;

summer means connected to said coefficient means and said integrating means for combining said first and second components to provide said controller output signal; and

means, connected between said coefficient means and said integrating means and connected to receive said control deviation signal, for disabling said integrating means when said control deviation signal exceeds a given threshold.