Invention Application
- Patent Title: APPARATUS FOR MEASURING TEMPERATURE OF AERO-ENGINE TURBINE BLADES
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Application No.: US15949037Application Date: 2018-04-09
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Publication No.: US20180348059A1Publication Date: 2018-12-06
- Inventor: Chao WANG , Zezhan ZHANG , Fei WANG , Chengui ZHANG , Jun HU , Yang YANG , Jing JIANG , Hongchuan JIANG , Yueming WANG , Yuhua CHENG , Jiexiong DING , Li DU , Houjun WANG
- Applicant: UNIVERSITY OF ELECTRONIC SCIENCE AND TECHNOLOGY OF CHINA
- Priority: CN201710413059.7 20170605
- Main IPC: G01J5/08
- IPC: G01J5/08 ; G01J5/06 ; G01N21/27

Abstract:
An apparatus for measuring temperature of turbine blades, including: a radiation collection device, a data processing module; a master control unit (MCU); a calibration module; and a motion servo. The radiation collection device includes a scan reflector, a collimator lens, a first dichroic mirror, a first focus lens, a visible and near-infrared (VNIR) detector, a second dichroic mirror, a second focus lens, a short-wave infrared (SWIR) detector, a third focus lens, and a medium-wave infrared (MWIR) detector. The calibration module includes a calibration reflection mirror and a blackbody furnace. The scan reflector, the collimator lens, the first dichroic mirror, the second dichroic mirror, the third focus lens, and the MWIR detector are disposed successively along a first optical axis; the first dichroic mirror, the first focus lens, and the VNIR detector are disposed successively along a second optical axis that is perpendicular to the first optical axis.
Public/Granted literature
- US10746604B2 Apparatus for measuring temperature of aero-engine turbine blades Public/Granted day:2020-08-18
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