Invention Application
US20140064326A1 NOISE ROBUST TIME OF FLIGHT ESTIMATION FOR ACOUSTIC PYROMETRY
有权
噪声估计的噪声稳定时间用于声学PYROMETRY
- Patent Title: NOISE ROBUST TIME OF FLIGHT ESTIMATION FOR ACOUSTIC PYROMETRY
- Patent Title (中): 噪声估计的噪声稳定时间用于声学PYROMETRY
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Application No.: US13961292Application Date: 2013-08-07
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Publication No.: US20140064326A1Publication Date: 2014-03-06
- Inventor: Heiko Claussen , Justinian Rosca , Michelle xiaohong Yan , Upul P. DeSilva , Nancy H. Ulerich
- Applicant: Heiko Claussen , Justinian Rosca , Michelle xiaohong Yan , Upul P. DeSilva , Nancy H. Ulerich
- Applicant Address: US FL Orlando US NJ Iselin
- Assignee: SIEMENS ENERGY, INC.,SIEMENS CORPORATION
- Current Assignee: SIEMENS ENERGY, INC.,SIEMENS CORPORATION
- Current Assignee Address: US FL Orlando US NJ Iselin
- Main IPC: G01K11/24
- IPC: G01K11/24

Abstract:
An acoustic signal traversing a hot gas is sampled at a source and a receiver and is represented in overlapping windows that maximize useable signal content. Samples in each window are processed to represented in different sparsified bins in the frequency domain. Determining a signal delay between the source and the receiver from a summation of maximum smoothed coherence transform cross-correlation values of different data windows wherein a sparseness of a mean smoothed coherence transform cross-correlation of windows is maximized. Determining a set of delay times wherein outliers are deleted to estimate a time of flight from which a temperature of the hot gas is calculated.
Public/Granted literature
- US09702768B2 Noise robust time of flight estimation for acoustic pyrometry Public/Granted day:2017-07-11
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