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公开(公告)号：US10995402B2
公开(公告)日：2021-05-04
申请号：US16884602
申请日：2020-05-27
Applicant: Raytheon Technologies Corporation
Inventor： Shayan Ahmadian , Hoyt Y. Chang
Abstract: A coating system including a reflective cool down chamber with at least one arcuate wall; and an infrared lamp directed at the arcuate wall.
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公开(公告)号：US20210301676A1
公开(公告)日：2021-09-30
申请号：US17024975
申请日：2020-09-18
Applicant: Raytheon Technologies Corporation
Inventor： Shayan Ahmadian , Charles W. Haldeman , Mark F. Zelesky , Christopher T. Bergman , Sebastian Martinez
Abstract: A method of measuring a gas turbine engine component of a gas turbine engine according to an example of the present disclosure includes, among other things, providing at least one gas turbine engine component including a coating on a substrate, detecting infrared radiation emitted from at least one localized region of the coating at a first wavelength in a first electromagnetic radiation frequency range, detecting infrared radiation emitted from the substrate corresponding to the at least one localized region at a second, different wavelength in a second electromagnetic radiation frequency range that differs from the first electromagnetic radiation frequency range, and determining a heat flux relating to the at least one localized region based upon a comparison of the first wavelength and the second wavelength.
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公开(公告)号：US20200318231A1
公开(公告)日：2020-10-08
申请号：US16884602
申请日：2020-05-27
Applicant: Raytheon Technologies Corporation
Inventor： Shayan Ahmadian , Hoyt Y. Chang
Abstract: A coating system including a reflective cool down chamber with at least one arcuate wall; and an infrared lamp directed at the arcuate wall.
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公开(公告)号：US11346239B2
公开(公告)日：2022-05-31
申请号：US17024975
申请日：2020-09-18
Applicant: Raytheon Technologies Corporation
Inventor： Shayan Ahmadian , Charles W. Haldeman , Mark F. Zelesky , Christopher T. Bergman , Sebastian Martinez
Abstract: A method of measuring a gas turbine engine component of a gas turbine engine according to an example of the present disclosure includes, among other things, providing at least one gas turbine engine component including a coating on a substrate, detecting infrared radiation emitted from at least one localized region of the coating at a first wavelength in a first electromagnetic radiation frequency range, detecting infrared radiation emitted from the substrate corresponding to the at least one localized region at a second, different wavelength in a second electromagnetic radiation frequency range that differs from the first electromagnetic radiation frequency range, and determining a heat flux relating to the at least one localized region based upon a comparison of the first wavelength and the second wavelength.
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