In the regeneration of a catalyst located interior of an insulation-clad vessel having an axis of symmetry, by elevating the temperature of said catalyst only after production of hydrocarbon products such as petrochemicals, gasolines, light-fuel oils and the like, has been terminated, the method of monitoring the efficiency of such regeneration process comprising the steps of:
- i. prior to operation of said vessel and either production or regeneration processing modes, affixing a plurality of metallic stud members to the metallic sidewall of said vessel, said plurality of metallic stud members extending through said insulation of the vessel, and being associated with a set of imaginary laterally offset spatial positions interior of said vessel for identifying full top-to-bottom interior temperature readings within each catalyst bed when said vessel undergoes regeneration,
- ii. during regeneration of said catalyst, monitoring from an aircraft having known geographical coordinates with respect to said vessel at the earth's surface, infrared energy--in real time--being emitted from said plurality of metallic stud members defining a viewable space of said stud members in a frequency range greater than 300 .times. 10.sup.9 but less than 10.sup.15 Hertz,
- iii. converting said detected infrared energy to electrical signals,
- iv. enhancing those portions of said electrical signals based on whether the detected energy represented thereby radiated from all sources including that from said stud members remains stationary during two adjacent scanning cycles as said aircraft overflies said vessel,
- v. dynamically indicating temperatures of said catalyst interior of said vessel for the purpose of optimizing said regeneration process by displaying said enhanced signals as a function of geometric and time variables associated with said stud members as viewed from said aircraft, and
- vi. cyclically repeating the scanning sequence as said aircraft overflies said vessel on a flight pattern of sufficient height so that, between said scanning cycles, said stud members appear to be stationary with respect to said aircraft.