Experimental Investigation of Inductive Sensor Characteristic for Blade Tip Clearance Measurement at High Temperature
Turbine tip clearance of aero-engine is important to engine performance. Proper tip clearance can reduce the gas leakage over turbine blade tips and improve the engine efficiency of turbo machinery and reduce the fuel consumption. Therefore, accurate tip clearance measurement is essential. The induc...
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Published in | Sensors (Basel, Switzerland) Vol. 19; no. 17; p. 3694 |
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Main Authors | , , , |
Format | Journal Article |
Language | English |
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25.08.2019
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Abstract | Turbine tip clearance of aero-engine is important to engine performance. Proper tip clearance can reduce the gas leakage over turbine blade tips and improve the engine efficiency of turbo machinery and reduce the fuel consumption. Therefore, accurate tip clearance measurement is essential. The inductive measurement method is one of the non-contact distance measurement methods, which has the characteristics of high sensitivity, fast response speed, and strong anti-interference ability. Based on the principle of inductive sensor measuring tip clearance, the ambient temperature change may cause the material electromagnetic performance change for the conductivity and permeability varies with temperature. In order to verify the temperature effect on the sensor performance, the repeated calibration experiments were carried out to obtain the sensor repeatability error of 5.4%. Then, the sensor was calibrated in the range of 0mm-4mm clearance at temperature from 600 °C to 1000 °C and obtained the measurement error of 4.6%. Results indicate when the temperature ranged from 600 °C to 1000 °C, clearance measurement error is smaller than the sensor repeatability error so the temperature effect on the sensor characteristics can be ignored. This conclusion makes the sensor promising for monitoring the blade tip clearances at various temperature environment. |
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AbstractList | Turbine tip clearance of aero-engine is important to engine performance. Proper tip clearance can reduce the gas leakage over turbine blade tips and improve the engine efficiency of turbo machinery and reduce the fuel consumption. Therefore, accurate tip clearance measurement is essential. The inductive measurement method is one of the non-contact distance measurement methods, which has the characteristics of high sensitivity, fast response speed, and strong anti-interference ability. Based on the principle of inductive sensor measuring tip clearance, the ambient temperature change may cause the material electromagnetic performance change for the conductivity and permeability varies with temperature. In order to verify the temperature effect on the sensor performance, the repeated calibration experiments were carried out to obtain the sensor repeatability error of 5.4%. Then, the sensor was calibrated in the range of 0 mm–4 mm clearance at temperature from 600 °C to 1000 °C and obtained the measurement error of 4.6%. Results indicate when the temperature ranged from 600 °C to 1000 °C, clearance measurement error is smaller than the sensor repeatability error so the temperature effect on the sensor characteristics can be ignored. This conclusion makes the sensor promising for monitoring the blade tip clearances at various temperature environment. Turbine tip clearance of aero-engine is important to engine performance. Proper tip clearance can reduce the gas leakage over turbine blade tips and improve the engine efficiency of turbo machinery and reduce the fuel consumption. Therefore, accurate tip clearance measurement is essential. The inductive measurement method is one of the non-contact distance measurement methods, which has the characteristics of high sensitivity, fast response speed, and strong anti-interference ability. Based on the principle of inductive sensor measuring tip clearance, the ambient temperature change may cause the material electromagnetic performance change for the conductivity and permeability varies with temperature. In order to verify the temperature effect on the sensor performance, the repeated calibration experiments were carried out to obtain the sensor repeatability error of 5.4%. Then, the sensor was calibrated in the range of 0mm-4mm clearance at temperature from 600 °C to 1000 °C and obtained the measurement error of 4.6%. Results indicate when the temperature ranged from 600 °C to 1000 °C, clearance measurement error is smaller than the sensor repeatability error so the temperature effect on the sensor characteristics can be ignored. This conclusion makes the sensor promising for monitoring the blade tip clearances at various temperature environment. Turbine tip clearance of aero-engine is important to engine performance. Proper tip clearance can reduce the gas leakage over turbine blade tips and improve the engine efficiency of turbo machinery and reduce the fuel consumption. Therefore, accurate tip clearance measurement is essential. The inductive measurement method is one of the non-contact distance measurement methods, which has the characteristics of high sensitivity, fast response speed, and strong anti-interference ability. Based on the principle of inductive sensor measuring tip clearance, the ambient temperature change may cause the material electromagnetic performance change for the conductivity and permeability varies with temperature. In order to verify the temperature effect on the sensor performance, the repeated calibration experiments were carried out to obtain the sensor repeatability error of 5.4%. Then, the sensor was calibrated in the range of 0 mm−4 mm clearance at temperature from 600 °C to 1000 °C and obtained the measurement error of 4.6%. Results indicate when the temperature ranged from 600 °C to 1000 °C, clearance measurement error is smaller than the sensor repeatability error so the temperature effect on the sensor characteristics can be ignored. This conclusion makes the sensor promising for monitoring the blade tip clearances at various temperature environment. |
Author | Zhao, Lingqiang Liu, Zhenxia Zhao, Ziyu Lyu, Yaguo |
AuthorAffiliation | School of Power and Energy, Northwestern Polytechnical University, Youyi West Road 127#, Xi’an 710054, China |
AuthorAffiliation_xml | – name: School of Power and Energy, Northwestern Polytechnical University, Youyi West Road 127#, Xi’an 710054, China |
Author_xml | – sequence: 1 givenname: Zhenxia surname: Liu fullname: Liu, Zhenxia organization: School of Power and Energy, Northwestern Polytechnical University, Youyi West Road 127#, Xi'an 710054, China – sequence: 2 givenname: Ziyu orcidid: 0000-0002-5239-3323 surname: Zhao fullname: Zhao, Ziyu organization: School of Power and Energy, Northwestern Polytechnical University, Youyi West Road 127#, Xi'an 710054, China – sequence: 3 givenname: Yaguo surname: Lyu fullname: Lyu, Yaguo email: yglu@nwpu.edu.cn organization: School of Power and Energy, Northwestern Polytechnical University, Youyi West Road 127#, Xi'an 710054, China. yglu@nwpu.edu.cn – sequence: 4 givenname: Lingqiang surname: Zhao fullname: Zhao, Lingqiang organization: School of Power and Energy, Northwestern Polytechnical University, Youyi West Road 127#, Xi'an 710054, China |
BackLink | https://www.ncbi.nlm.nih.gov/pubmed/31450693$$D View this record in MEDLINE/PubMed |
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Cites_doi | 10.1088/1361-6501/aa912e 10.3390/s130607385 10.2514/6.1982-1131 10.3390/s17102162 10.1115/GT2016-57368 10.1115/GT2017-63807 10.1088/0964-1726/23/6/065018 10.3390/s19010061 10.3390/s18082610 10.3390/s16111897 10.1016/j.sna.2013.09.016 10.1115/GT2013-94104 10.1115/96-GT-349 10.1115/GT2017-63803 10.1115/GT2018-75643 |
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SubjectTerms | Ambient temperature Blade tips Calibration Distance measurement Error analysis Gas turbine engines High temperature inductive sensor Magnetic fields Measurement methods repeatability error Sensors Temperature effects Tip clearance Turbine blades |
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Title | Experimental Investigation of Inductive Sensor Characteristic for Blade Tip Clearance Measurement at High Temperature |
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