Pyrometer systems for gas-turbine engines

Thermal measuring and testing – Temperature measurement – In spaced noncontact relationship to specimen

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

356 43, 374121, 374133, G01J 510

Patent

active

047970065

ABSTRACT:
In a pyrometer system, a pyrometer provides output signals to a processor indicative of the temperature of rotating blades in a gas-turbine engine. The processor includes a synchronization unit and a gate controlled by the synchronization unit. After monitoring the output of the pyrometer to identify which parts of the output signal arise from radiation from the blades and which arise from the combustion chamber, the synchronization unit is set in synchronism with the blade signals and the gate is controlled to pass signals from the blade and to interrupt signals arising from the combustion chamber. The output of the processor is thereby indicative of blade temperature and is insensitive to combustion chamber radiation.

REFERENCES:
patent: 3207027 (1965-09-01), Bouchet
patent: 3623368 (1971-11-01), Decker, Jr.
patent: 4579463 (1986-04-01), Rosenewaig et al.
patent: 4582426 (1986-04-01), Douglas

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Pyrometer systems for gas-turbine engines does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Pyrometer systems for gas-turbine engines, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Pyrometer systems for gas-turbine engines will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-2105391

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.