FIELD: engines and pumps.
SUBSTANCE: invention can be used in systems for measuring temperature of gas turbine engines (GTE). First proportional link of this meter is connected with its input to differentiator output while its output is connected to second input of second multiplier unit. Meter also comprises series-connected second proportional link with input connected to output of second multiplier unit and third adder with second input connected to output of integrator and with output connected to second input of second adder.
EFFECT: increase of noise immunity of gas temperature meter of gas turbine engine.
1 cl, 5 dwg
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|---|---|---|---|
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|
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