Stall control apparatus for axial flow compressors

Claim 2

A stall control system for compressors, comprising: (a) first means for generating a varying reference pressure signal in response to operating conditions within a compressor, (b) a plurality of pressure responsive elements located within the housing of a compressor for developing signals indicative of the nonsteady pressure variations therein, (c) separate means associated with each one of said elements for separately filtering and rectifying each of said signals, (d) second means for independently comparing each one of said filtered and rectified signals with said reference pressure signal and developing an intermediate control signal if any one of said filtered and rectified signals exceeds said reference pressure signal, (e) third means for developing a composite signal indicative of the combined amount by which each of said signals exceeds said reference pressure signal, (f) fourth means responsive to said intermediate control signal for integrating said composite signal to generate a control signal for influencing the actuation of a controlled variable within a compressor, and (g) means for varying the decay rate of said control signal.

Claim 3

The system according to claim 1, wherein; (h) said second means comprises comparators and a logic circuit, and (i) said fourth means comprises a gate and an integrator.

Claim 4

The system according to claim 1, wherein; (h) said means for varying the decay rate of said control signal comprises an adjustable time delay controlling short and long time constant circuits.

Claim 5

In a turboengine system having a compressor, a controlled variable within the compressor, an actuator for said controlled variable, an engine control system having as one of its outputs means for controlling said actuator during normal operation, the improvement of stall control means located between said engine system output and said actuator for controlling movement thereof in response to unsteady pressure variations within said compressor, comprising; (a) a variable reference pressure signal responsive to operating conditions within said compressor, (b) a plurality of pressure responsive elements located within the housing of said compressor for developing signals indicative of the nonsteady pressure variations therein, (c) separate filters and rectifiers associated with each of said elements developing separate processed signals, (d) comparators for each of said processed signals for delivering a plurality of signals the amplitude of each of which is a function of the difference between said reference pressure signal and each of said processed signals, (e) gate comparators for independently comparing each one of said processed signals with said reference pressure signal, (f) logic circuits responsive to the output of said gate comparator for developing an intermediate control signal if any one of said processed signals exceeds said reference pressure signal, (g) a gate responsive to said intermediate control signal for passing said plurality of signals from said comparator, and (h) an integrator for integrating the output of said gate and delivering a control signal for said actuator.

Claim 6

In a turboengine system having a compressor, a controlled variable within the compressor, an actuator for said controlled variable, an engine control system having as one of its outputs means for controlling said actuator during normal operation, the improvement of stall control means located between said engine system output and said actuator for controlling movement thereof in response to unsteady pressure variations within said compressor, comprising; (a) a variable reference pressure signal responsive to operating conditions within said compressor, (b) a plurality of pressure responsive elements located within the housing of said compressor for developing signals indicative of the nonsteady pressure variations therein, (c) separate filters and rectifiers associated with each of said elements developing separate processed signals, (d) comparators for each of said processed signals for delivering a plurality of signals the amplitude of each of which is a function of the difference between said reference pressure signal and each of said processed signals, (e) gate comparators for independently comparing each one of said processed signals with said reference pressure signal, (f) logic circuits responsive to the output of said gate comparator for developing an intermediate control signal if any one of said processed signals exceeds said reference pressure signal, (g) a gate responsive to said intermediate control signal for passing said plurality of signals from said comparator, and (h) an integrator for integrating the output of said gate and delivering a control signal for said actuator.

Claim 7

The system according to claim 4, further comprising; (i) a time delay circuit coacting with said integrator for controlling the decay rate of said control signal.

Claim 8

The system according to claim 5, wherein said time delay circuit includes; (j) a long time constant circuit, and (k) a short time constant circuit operative to increase the decay rate of said control signal after said intermediate control signal goes to zero for a predetermined time.

Claim 9

The system according to claim 6, wherein; (l) said controlled variable comprises bleed doors.

Claim 10

In a turboengine system having a compressor, a controlled variable within the compressor, an actuator for said controlled variable, an engine control system having as one of its outputs means for controlling said actuator during normal operation, the improvement of stall control means located between said engine system output and said actuator for controlling movement thereof in response to unsteady pressure variations sensed at multiple locations within said compressor and compared with a reference pressure signal which varies as a function of operating conditions within said compressor, said stall control means comprising; (a) a variable reference pressure signal responsive to operating conditions within said compressor, (b) a plurality of pressure responsive transducers located within said compressor for generating signals indicative of the nonsteady pressure variations therein, (c) parallel processing channels for independently filtering and rectifying said signals, and (d) means for independently comparing each of said filtered and rectified signals with said pressure reference signal for generating an intermediate control signal.

Claim 11

In a turboengine system having a compressor, a controlled variable within the compressor, an actuator for said controlled variable, an engine control system having as one of its outputs means for controlling said actuator during normal operation, the improvement of stall control means located between said engine system output and said actuator for controlling movement thereof in response to unsteady pressure variations sensed at multiple locations within said compressor and compared with a reference pressure signal which varies as a function of operating conditions within said compressor, said stall control means comprising; (a) a variable reference pressure signal responsive to operating conditions within said compressor, (b) a plurality of pressure responsive transducers located within said compressor for generating signals indicative of the nonsteady pressure variations therein, (c) parallel processing channels for independently filtering and rectifying said signals, and (d) means for independently comparing each of said filtered and rectified signals with said pressure reference signal for generating an intermediate control signal.

Claim 12

The system according to claim 8, further comprising; (e) means for independently comparing each of said filtered and rectified signals with said pressure reference signal for generating a composite analog signal; and (f) means responsive to said intermediate control signal for passing said composite signal.

Claim 13

The system according to claim 9, further comprising; (g) an integrator responsive to the output of said last mentioned means for delivering a control signal for said actuator.

Claim 14

The system according to claim 10, further comprising; (h) means for increasing the decay rate of said control signal after a predetermined delay.

Claim 15

The system according to claim 11, wherein; (i) said controlled variable comprises bleed doors.