Research on particle impact noise detection standards
Particle impact noise detection (PIND) is a reliable screening technique specified by MIL-STD-883E. But MIL-STD-883E gives some test conditions which are not always appropriate. The test conditions of PIND are derived here based on dynamics. The upper limit frequency expression is obtained by a tran...
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Veröffentlicht in: | IEEE transactions on aerospace and electronic systems 2008-04, Vol.44 (2), p.808-814 |
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creator | Zhang, Hui Wang, Shu-Juan Zhai, Guo-Fu |
description | Particle impact noise detection (PIND) is a reliable screening technique specified by MIL-STD-883E. But MIL-STD-883E gives some test conditions which are not always appropriate. The test conditions of PIND are derived here based on dynamics. The upper limit frequency expression is obtained by a transforming equation. How vibration acceleration, vibration frequency, recovery coefficient, particle mass, and cavity height influence the particle's output energy is discussed. Moreover, the applicable range of test conditions of MIL-STD-883E are indicated and the best vibration frequency is derived by analyzing the relationship between the output power of vibrator and the particle's output energy. Some experiments are given. |
doi_str_mv | 10.1109/TAES.2008.4560223 |
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But MIL-STD-883E gives some test conditions which are not always appropriate. The test conditions of PIND are derived here based on dynamics. The upper limit frequency expression is obtained by a transforming equation. How vibration acceleration, vibration frequency, recovery coefficient, particle mass, and cavity height influence the particle's output energy is discussed. Moreover, the applicable range of test conditions of MIL-STD-883E are indicated and the best vibration frequency is derived by analyzing the relationship between the output power of vibrator and the particle's output energy. Some experiments are given.</description><identifier>ISSN: 0018-9251</identifier><identifier>EISSN: 1557-9603</identifier><identifier>DOI: 10.1109/TAES.2008.4560223</identifier><identifier>CODEN: IEARAX</identifier><language>eng</language><publisher>New York: IEEE</publisher><subject>Acceleration ; Aerodynamics ; Aircraft components ; Contamination ; Electronic components ; Electronic equipment testing ; Electronic systems ; Frequency ; Life estimation ; Manufacturing ; Mathematical analysis ; Noise ; Particle impact ; Particle mass ; Vehicle dynamics ; Vibration ; Vibrations</subject><ispartof>IEEE transactions on aerospace and electronic systems, 2008-04, Vol.44 (2), p.808-814</ispartof><rights>Copyright The Institute of Electrical and Electronics Engineers, Inc. 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But MIL-STD-883E gives some test conditions which are not always appropriate. The test conditions of PIND are derived here based on dynamics. The upper limit frequency expression is obtained by a transforming equation. How vibration acceleration, vibration frequency, recovery coefficient, particle mass, and cavity height influence the particle's output energy is discussed. Moreover, the applicable range of test conditions of MIL-STD-883E are indicated and the best vibration frequency is derived by analyzing the relationship between the output power of vibrator and the particle's output energy. Some experiments are given.</description><subject>Acceleration</subject><subject>Aerodynamics</subject><subject>Aircraft components</subject><subject>Contamination</subject><subject>Electronic components</subject><subject>Electronic equipment testing</subject><subject>Electronic systems</subject><subject>Frequency</subject><subject>Life estimation</subject><subject>Manufacturing</subject><subject>Mathematical analysis</subject><subject>Noise</subject><subject>Particle impact</subject><subject>Particle mass</subject><subject>Vehicle dynamics</subject><subject>Vibration</subject><subject>Vibrations</subject><issn>0018-9251</issn><issn>1557-9603</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2008</creationdate><recordtype>article</recordtype><sourceid>RIE</sourceid><recordid>eNqFkU1Lw0AQhhdRsH78APESPOgpdfZ791hK_YCCoPW8bDYTTGmTupse_PcmtnrwoKdheJ93YHgIuaAwphTs7WIyexkzADMWUgFj_ICMqJQ6twr4IRkBUJNbJukxOUlp2a_CCD4i8hkT-hjesrbJNj52dVhhVq83PnRZ09YJsxI7DF3d56nzTeljmc7IUeVXCc_385S83s0W04d8_nT_OJ3M88CN7nLEoIMoKNOMygpMQYXWpmBK2xK0FwW3WIAMvDJMCg-2VJURtgos-KoCxk_Jze7uJrbvW0ydW9cp4GrlG2y3yVngSnBq7b-kMaCEYV_k9Z8kF0IxAwN49QtcttvY9P86ozjVmknVQ3QHhdimFLFym1ivffxwFNxgxg1m3GDG7c30nctdp0bEH_47_QReeIfm</recordid><startdate>20080401</startdate><enddate>20080401</enddate><creator>Zhang, Hui</creator><creator>Wang, Shu-Juan</creator><creator>Zhai, Guo-Fu</creator><general>IEEE</general><general>The Institute of Electrical and Electronics Engineers, Inc. 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But MIL-STD-883E gives some test conditions which are not always appropriate. The test conditions of PIND are derived here based on dynamics. The upper limit frequency expression is obtained by a transforming equation. How vibration acceleration, vibration frequency, recovery coefficient, particle mass, and cavity height influence the particle's output energy is discussed. Moreover, the applicable range of test conditions of MIL-STD-883E are indicated and the best vibration frequency is derived by analyzing the relationship between the output power of vibrator and the particle's output energy. Some experiments are given.</abstract><cop>New York</cop><pub>IEEE</pub><doi>10.1109/TAES.2008.4560223</doi><tpages>7</tpages></addata></record> |
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subjects | Acceleration Aerodynamics Aircraft components Contamination Electronic components Electronic equipment testing Electronic systems Frequency Life estimation Manufacturing Mathematical analysis Noise Particle impact Particle mass Vehicle dynamics Vibration Vibrations |
title | Research on particle impact noise detection standards |
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