发明名称 |
High speed hot air leak sensor |
摘要 |
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.
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申请公布号 |
US4655607(A) |
申请公布日期 |
1987.04.07 |
申请号 |
US19850793496 |
申请日期 |
1985.10.30 |
申请人 |
SANTA BARBARA RESEARCH CENTER |
发明人 |
KERN, MARK T.;CINZORI, ROBERT J.;FULLER, WILLIAM D. |
分类号 |
B64D45/00;G01M3/00;G01M3/38;(IPC1-7):G01K1/16;G01N25/72 |
主分类号 |
B64D45/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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