Thrust control system for a gas turbine engine

Claim 2

In a thrust-setting system for a gas turbine engine, the invention comprising: first means associated with a first thrust-indicating parameter for providing a first indication related to the thrust output of said engine; second means associated with a second thrust-indicating parameter for providing a second indication related to the thrust output of said engine; third means for varying the thrust output of said engine to correspond to a demanded level in a first mode wherein said variation is in response to said first and second thrust-indicating parameters, said third means adapted to vary said thrust output to correspond to a demanded level in a second mode wherein said variation is in response to said first thrust-indicating parameter and not in response to said second thrust-indicating parameter.

Claim 3

The invention as set forth in claim 1 wherein said third means is operable in said second mode when said second means is in an abnormal operating condition.

Claim 4

In a thrust-setting system for a gas turbine engine, the invention comprising: first means for determining a first error indicative of the deviation of a first thrust-indicating parameter of said engine from a first reference value; second means for determining a second error indicative of the deviation of a second thrust-indicating paramerter of said engine from a second reference value; third means for comparing said first and second errors for determining the difference between said first and second errors and for adjusting the thrust output of said engine to correspond to a demanded level in accordance with both of said first and second thrust-indicating parameters when said difference is within a predetermined range of reference magnitudes.

Claim 5

In a thrust-setting system for a gas turbine engine, the invention comprising: first means for determining a first error indicative of the deviation of a first thrust-indicating parameter of said engine from a first reference value; second means for determining a second error indicative of the deviation of a second thrust-indicating paramerter of said engine from a second reference value; third means for comparing said first and second errors for determining the difference between said first and second errors and for adjusting the thrust output of said engine to correspond to a demanded level in accordance with both of said first and second thrust-indicating parameters when said difference is within a predetermined range of reference magnitudes.

Claim 6

The invention as set forth in claim 3 wherein said thrust output of said engine is varied in a second mode in accordance with only one of said first and second thrust-indication parameters when said difference is not within said range of reference magnitudes.

Claim 7

The invention as set forth in claim 4 wherein said predetermined range of magnitudes is selected to provide for variation of said thrust output in said second mode when said first means is in an abnormal operating condition.

Claim 8

In a thrust-setting system for a gas turbine engine, the invention comprising: first means for generating a first error signal indicative of the deviation of a first thrust-indicating parameter of said engine from a first reference value; second means for generating a second error signal indicative of the deviation of a second thrust-indicating parameter of said engine from a second reference value; third means responsive to said first and second error signals for providing an output signal in a first mode wherein said first and second means are in normal operating condition and wherein said output signal is indicative of both of said first and second error signals, said third means further providing an output signal in a second mode when said first means is in an abnormal operating condition and wherein said output signal is not indicative of said first error signal; fourth means responsive to said output signal for delivering metered fuel to said engine in order to adjust the thrust output of said engine to correspond to a demanded level.

Claim 9

In a thrust-setting system for a gas turbine engine, the invention comprising: first means for generating a first error signal indicative of the deviation of a first thrust-indicating parameter of said engine from a first reference value; second means for generating a second error signal indicative of the deviation of a second thrust-indicating parameter of said engine from a second reference value; third means responsive to said first and second error signals for providing an output signal in a first mode wherein said first and second means are in normal operating condition and wherein said output signal is indicative of both of said first and second error signals, said third means further providing an output signal in a second mode when said first means is in an abnormal operating condition and wherein said output signal is not indicative of said first error signal; fourth means responsive to said output signal for delivering metered fuel to said engine in order to adjust the thrust output of said engine to correspond to a demanded level.

Claim 10

The invention as set forth in claim 6 wherein said third means is responsive to the difference between the magnitude of said first error signal and the magnitude of said second error signal.

Claim 11

The invention as set forth in claim 7 wherein said third means includes difference signal generating means for generating a signal indicative of the difference between the magnitude of said first error signal and the magnitude of said second error signal.

Claim 12

The invention as set forth in claim 8 wherein said output signal is varied in accordance with said difference signal.

Claim 13

The invention as set forth in claim 9 wherein said third means is adapted to provide said output signal as indicative of both of said first and second error signals when said difference signal is within a predetermined range of reference signal magnitudes and further adapted to provide said output signal as indicative of said first error signal when said difference signal is not within said predetermined range of reference signal magnitudes.

Claim 14

The invention as set forth in claim 7 wherein said third means includes difference signal generating means for generating a signal indicative of the difference between the magnitude of said first error signal and the magnitude of said second error signal and further includes signal limiting means for limiting the magnitude of said difference signal to within a predetermined range of signal magnitudes.

Claim 15

The invention as set forth in claim 11 wherein said signal limiting means limits the magnitude of said difference signal when said first means is in an abnormal operating condition.

Claim 16

The invention as set forth in claim 12 wherein said output signal is responsive to said limited difference signal when said third means provides said output signal in said second mode.