发明名称 Method and apparatus to correct for the temperature sensitivity of pressure sensitive paint
摘要 A method and apparatus for correcting for the temperature sensitivity of pressure sensitive paint using two layers of paint: one that is sensitive to both pressure and temperature and one that is sensitive to only temperature changes. A temperature sensitive paint layer or film is placed on a model to be tested in a wind tunnel for pressure changes over the surface of the model. The first film is responsive to temperature changes and has a magnitude of luminosity depending upon the temperature of the ambient air. Placed over the temperature film is a pressure sensitive paint or film that is sensitive primarily to pressure changes, but also to temperature changes, and produces a magnitude of luminosity depending upon the change in both temperature and pressure. The pressure paint layer is transparent to the luminescence of the temperature layer and a measurement of the luminosity of the temperature layer and the pressure layer is taken. The pressure layer luminosity is corrected for the temperature layer luminosity, thereby enabling a true pressure reading to be determined by comparing the magnitude of luminescence of both the temperature layer and the pressure layer.
申请公布号 US6696690(B2) 申请公布日期 2004.02.24
申请号 US20010022590 申请日期 2001.12.17
申请人 THE BOEING COMPANY 发明人 BENNE MICHAEL E.
分类号 G01L1/24;G01M9/06;G01N21/64;(IPC1-7):G01N21/64;G01K11/12 主分类号 G01L1/24
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