Triple spectral area pyrometer
AssigneeUnited Technologies Corporation
InventorsErnesto Suarez-Gonzalez, Raymond L. Oqlukian
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AssigneeUnited Technologies Corporation
InventorsErnesto Suarez-Gonzalez, Raymond L. Oqlukian
Estimating the term…
An optical pyrometer for use with jet engines is characterized by the use of three spectral areas or bands in a temperature computation. A target temperature is optically distinguished from background radiation by dividing a received optical beam into three spectral components which are comprised of emitted and reflected radiation. A controller computes the measured power in each band as a function of the emitted power by the target and a ratio of reflected power in adjacent bands to yield signals of reflection corrected radiation. These are used with the reflected power ratios to determine values of temperature in adjacent bands. The difference between these computed temperatures is iteratively adjusted until the difference therebetween is approximately equal to a preselected value.
A pyrometer for measuring the temperature of a remote target having a known value of emissivity, comprising:
In a pyrometer that measures the temperature of a remote target having a known value of emissivity, said pyrometer having a means for receiving a target optical beam having a spectral width and a beam power including an emitted component and a reflected component, a detection module that divides said target optical beam into three optical sub-beams each having a subportion of the optical beam spectral width, said detector means for providing respective electrical signal equivalents of said divided optical sub-beams, a controller comprising:
A detection module for use with an optical pyrometer that provides, along an optical guide, an optical beam having a spectral width, said detection module comprising:
Dependencies are inferred from the claim text.