G - Physics – 01 – N
Patent
G - Physics
01
N
340/140.1, 340/1
G01N 21/84 (2006.01) B64D 45/00 (2006.01) G01M 3/38 (2006.01)
Patent
CA 1242506
HIGH SPEED HOT AIR LEAK SENSOR Abstract of the Disclosure A hot air leak sensor for sensing jet engine bleed air leaks in an aircraft. Infrared detectors are combined with thermal re-radiating elements which are installed in air passages adjacent to the bleed air ducts and downstream of the region where a bleed air leak may occur. The elements are approximately 50% transmissive and 50% absorptive to infrared radiation with wavelengths within the range of approximately 4 to 20 micrometers. Incident radiation within the field of view of the detector is both transmitted and absorbed for re-radiation to the detector. If no incident radiation within the sensor field of view is available, the re-radiating element still responds to the increased airstream temperature resulting from the bleed air leak and supplies radiation to the detector to provide detection of the leak.
470445
Cinzori Robert J.
Fuller William D.
Kern Mark T.
Santa Barbara Research Center
Sim & Mcburney
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