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.
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 代理人
主权项
地址