Radiation pyrometer system

Thermal measuring and testing – Temperature measurement – Combined with diverse art device

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374128, 356 43, G01J 500

Patent

active

045563284

ABSTRACT:
A pyrometer system for a gas-turbine engine, or the like, has a high-resolution radiation pyrometer that supplies signals to a detector unit. The detector unit includes an inverter that inverts the pyrometer output and supplies these signals via a diode to one electrode of a capacitor. The other electrode of the capacitor is grounded, a resistor being connected across the capacitor so that it is slowly discharged. The charge on the capacitor approximately follows the high-value/low-temperature signals, which are reinverted by a processing unit to give an averaged temperature indication. The diode is short-circuited for periods, approximately equal to the blade rotational frequency. During these periods the charge on the capacitor drops to the instantaneous value of the pyrometer output, producing a low-voltage/high-temperature spike. The detector unit includes a store to which these spikes are supplied after reinversion. The store has a long time period so as to produce a signal which approximately follows the tips of the high-temperature spikes.

REFERENCES:
patent: 3574282 (1971-04-01), Curwen
patent: 3623368 (1971-11-01), Decker, Jr.
patent: 3668427 (1972-06-01), Curwen
Electronics, vol. 51, No. 1, Jan. 5, 1978, "Infrared Sensor Outclasses Thermocouples in Checking Metal Fatigue in Jet Engines", pp. 54-55.

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