Development and Evaluation of a Low Cutpoint Virtual Impactor
Designing an impactor with a submicrometer cutpoint is a technical challenge, since high jet velocities (resulting in low pressures downstream of the jet nozzle) or small orifices are required. This paper presents the development of a low cutpoint virtual impactor that operates at a small pressure d...
Gespeichert in:
Veröffentlicht in: | Aerosol science and technology 1994-01, Vol.21 (3), p.223-235 |
---|---|
Hauptverfasser: | , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 235 |
---|---|
container_issue | 3 |
container_start_page | 223 |
container_title | Aerosol science and technology |
container_volume | 21 |
creator | Sioutas, C. Koutrakis, P. Olson, B. A. |
description | Designing an impactor with a submicrometer cutpoint is a technical challenge, since high jet velocities (resulting in low pressures downstream of the jet nozzle) or small orifices are required. This paper presents the development of a low cutpoint virtual impactor that operates at a small pressure drop. A parametric study was performed to determine the conditions that affect the performance of the virtual impactor. In addition, a detailed measurement of the particle losses through the system is presented. By developing a better understanding of the particle collection and losses as a function of geometric and flow parameters, the design of low cut-point virtual impactors can be optimized. The results show that the virtual impactor has a cutpoint of 0.12 μm at a pressure drop of 0.08 atm, with low particle losses, averaging about 7% with a maximum of 14% at the 50% cutpoint. The separation characteristics of the virtual impactor are similar to those predicted by the theory. Reducing the minor flow ratio from 0.2 to 0.1 results in a larger cutpoint size, a steeper collection efficiency curve and an increase in particle losses. The 50% cutpoint increases as the collection-to-acceleration nozzle diameter ratio (D
r
/D
j
) increased from a standard value of 1.4 to 2. Increasing the jet velocity and therefore the pressure drop across the impactor's nozzle results in a decrease in the 50% cutpoint, as well as in a decrease in the particle losses within the virtual impactor. |
doi_str_mv | 10.1080/02786829408959711 |
format | Article |
fullrecord | <record><control><sourceid>proquest_pasca</sourceid><recordid>TN_cdi_pascalfrancis_primary_3369883</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>149196</sourcerecordid><originalsourceid>FETCH-LOGICAL-c399t-1fe66eb08e46cb3a52c3886834bf66abe2b61af8cbc76164b20295998f9af91c3</originalsourceid><addsrcrecordid>eNp1kDFPwzAQhS0EEqXwA9gyILaAz04dW4IBlQKVKrEAa3RxbSnIiYPtgPrvSdXCgphuuO-9u_cIOQd6BVTSa8pKKSRTBZVqpkqAAzKBGYO85FIeksl2n4-AOCYnMb5TSqFkMCG39-bTON-3pksZduts8YluwNT4LvM2w2zlv7L5kHrfjMBbE9KALlu2Perkwyk5suiiOdvPKXl9WLzMn_LV8-NyfrfKNVcq5WCNEKam0hRC1xxnTI9fCcmL2gqBtWG1ALRS17oUIIqaUTamUNIqtAo0n5LLnW8f_MdgYqraJmrjHHbGD7ECIZVkRTmCsAN18DEGY6s-NC2GTQW02hZV_Slq1FzszTFqdDZgp5v4K-RcKCn5iN3ssKazPrT45YNbVwk3zocfDf__yje043og</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>16898247</pqid></control><display><type>article</type><title>Development and Evaluation of a Low Cutpoint Virtual Impactor</title><source>EZB-FREE-00999 freely available EZB journals</source><source>Free Full-Text Journals in Chemistry</source><creator>Sioutas, C. ; Koutrakis, P. ; Olson, B. A.</creator><creatorcontrib>Sioutas, C. ; Koutrakis, P. ; Olson, B. A.</creatorcontrib><description>Designing an impactor with a submicrometer cutpoint is a technical challenge, since high jet velocities (resulting in low pressures downstream of the jet nozzle) or small orifices are required. This paper presents the development of a low cutpoint virtual impactor that operates at a small pressure drop. A parametric study was performed to determine the conditions that affect the performance of the virtual impactor. In addition, a detailed measurement of the particle losses through the system is presented. By developing a better understanding of the particle collection and losses as a function of geometric and flow parameters, the design of low cut-point virtual impactors can be optimized. The results show that the virtual impactor has a cutpoint of 0.12 μm at a pressure drop of 0.08 atm, with low particle losses, averaging about 7% with a maximum of 14% at the 50% cutpoint. The separation characteristics of the virtual impactor are similar to those predicted by the theory. Reducing the minor flow ratio from 0.2 to 0.1 results in a larger cutpoint size, a steeper collection efficiency curve and an increase in particle losses. The 50% cutpoint increases as the collection-to-acceleration nozzle diameter ratio (D
r
/D
j
) increased from a standard value of 1.4 to 2. Increasing the jet velocity and therefore the pressure drop across the impactor's nozzle results in a decrease in the 50% cutpoint, as well as in a decrease in the particle losses within the virtual impactor.</description><identifier>ISSN: 0278-6826</identifier><identifier>EISSN: 1521-7388</identifier><identifier>DOI: 10.1080/02786829408959711</identifier><identifier>CODEN: ASTYDQ</identifier><language>eng</language><publisher>London: Taylor & Francis Group</publisher><subject>Aerosols ; Analysis methods ; Applied sciences ; Atmospheric pollution ; Design ; Exact sciences and technology ; Pollution ; Q1</subject><ispartof>Aerosol science and technology, 1994-01, Vol.21 (3), p.223-235</ispartof><rights>Copyright Taylor & Francis Group, LLC 1994</rights><rights>1995 INIST-CNRS</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c399t-1fe66eb08e46cb3a52c3886834bf66abe2b61af8cbc76164b20295998f9af91c3</citedby><cites>FETCH-LOGICAL-c399t-1fe66eb08e46cb3a52c3886834bf66abe2b61af8cbc76164b20295998f9af91c3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>315,781,785,27929,27930</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=3369883$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Sioutas, C.</creatorcontrib><creatorcontrib>Koutrakis, P.</creatorcontrib><creatorcontrib>Olson, B. A.</creatorcontrib><title>Development and Evaluation of a Low Cutpoint Virtual Impactor</title><title>Aerosol science and technology</title><description>Designing an impactor with a submicrometer cutpoint is a technical challenge, since high jet velocities (resulting in low pressures downstream of the jet nozzle) or small orifices are required. This paper presents the development of a low cutpoint virtual impactor that operates at a small pressure drop. A parametric study was performed to determine the conditions that affect the performance of the virtual impactor. In addition, a detailed measurement of the particle losses through the system is presented. By developing a better understanding of the particle collection and losses as a function of geometric and flow parameters, the design of low cut-point virtual impactors can be optimized. The results show that the virtual impactor has a cutpoint of 0.12 μm at a pressure drop of 0.08 atm, with low particle losses, averaging about 7% with a maximum of 14% at the 50% cutpoint. The separation characteristics of the virtual impactor are similar to those predicted by the theory. Reducing the minor flow ratio from 0.2 to 0.1 results in a larger cutpoint size, a steeper collection efficiency curve and an increase in particle losses. The 50% cutpoint increases as the collection-to-acceleration nozzle diameter ratio (D
r
/D
j
) increased from a standard value of 1.4 to 2. Increasing the jet velocity and therefore the pressure drop across the impactor's nozzle results in a decrease in the 50% cutpoint, as well as in a decrease in the particle losses within the virtual impactor.</description><subject>Aerosols</subject><subject>Analysis methods</subject><subject>Applied sciences</subject><subject>Atmospheric pollution</subject><subject>Design</subject><subject>Exact sciences and technology</subject><subject>Pollution</subject><subject>Q1</subject><issn>0278-6826</issn><issn>1521-7388</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1994</creationdate><recordtype>article</recordtype><recordid>eNp1kDFPwzAQhS0EEqXwA9gyILaAz04dW4IBlQKVKrEAa3RxbSnIiYPtgPrvSdXCgphuuO-9u_cIOQd6BVTSa8pKKSRTBZVqpkqAAzKBGYO85FIeksl2n4-AOCYnMb5TSqFkMCG39-bTON-3pksZduts8YluwNT4LvM2w2zlv7L5kHrfjMBbE9KALlu2Perkwyk5suiiOdvPKXl9WLzMn_LV8-NyfrfKNVcq5WCNEKam0hRC1xxnTI9fCcmL2gqBtWG1ALRS17oUIIqaUTamUNIqtAo0n5LLnW8f_MdgYqraJmrjHHbGD7ECIZVkRTmCsAN18DEGY6s-NC2GTQW02hZV_Slq1FzszTFqdDZgp5v4K-RcKCn5iN3ssKazPrT45YNbVwk3zocfDf__yje043og</recordid><startdate>19940101</startdate><enddate>19940101</enddate><creator>Sioutas, C.</creator><creator>Koutrakis, P.</creator><creator>Olson, B. A.</creator><general>Taylor & Francis Group</general><general>Taylor & Francis</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>19940101</creationdate><title>Development and Evaluation of a Low Cutpoint Virtual Impactor</title><author>Sioutas, C. ; Koutrakis, P. ; Olson, B. A.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c399t-1fe66eb08e46cb3a52c3886834bf66abe2b61af8cbc76164b20295998f9af91c3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1994</creationdate><topic>Aerosols</topic><topic>Analysis methods</topic><topic>Applied sciences</topic><topic>Atmospheric pollution</topic><topic>Design</topic><topic>Exact sciences and technology</topic><topic>Pollution</topic><topic>Q1</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Sioutas, C.</creatorcontrib><creatorcontrib>Koutrakis, P.</creatorcontrib><creatorcontrib>Olson, B. A.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><jtitle>Aerosol science and technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Sioutas, C.</au><au>Koutrakis, P.</au><au>Olson, B. A.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Development and Evaluation of a Low Cutpoint Virtual Impactor</atitle><jtitle>Aerosol science and technology</jtitle><date>1994-01-01</date><risdate>1994</risdate><volume>21</volume><issue>3</issue><spage>223</spage><epage>235</epage><pages>223-235</pages><issn>0278-6826</issn><eissn>1521-7388</eissn><coden>ASTYDQ</coden><abstract>Designing an impactor with a submicrometer cutpoint is a technical challenge, since high jet velocities (resulting in low pressures downstream of the jet nozzle) or small orifices are required. This paper presents the development of a low cutpoint virtual impactor that operates at a small pressure drop. A parametric study was performed to determine the conditions that affect the performance of the virtual impactor. In addition, a detailed measurement of the particle losses through the system is presented. By developing a better understanding of the particle collection and losses as a function of geometric and flow parameters, the design of low cut-point virtual impactors can be optimized. The results show that the virtual impactor has a cutpoint of 0.12 μm at a pressure drop of 0.08 atm, with low particle losses, averaging about 7% with a maximum of 14% at the 50% cutpoint. The separation characteristics of the virtual impactor are similar to those predicted by the theory. Reducing the minor flow ratio from 0.2 to 0.1 results in a larger cutpoint size, a steeper collection efficiency curve and an increase in particle losses. The 50% cutpoint increases as the collection-to-acceleration nozzle diameter ratio (D
r
/D
j
) increased from a standard value of 1.4 to 2. Increasing the jet velocity and therefore the pressure drop across the impactor's nozzle results in a decrease in the 50% cutpoint, as well as in a decrease in the particle losses within the virtual impactor.</abstract><cop>London</cop><pub>Taylor & Francis Group</pub><doi>10.1080/02786829408959711</doi><tpages>13</tpages><oa>free_for_read</oa></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0278-6826 |
ispartof | Aerosol science and technology, 1994-01, Vol.21 (3), p.223-235 |
issn | 0278-6826 1521-7388 |
language | eng |
recordid | cdi_pascalfrancis_primary_3369883 |
source | EZB-FREE-00999 freely available EZB journals; Free Full-Text Journals in Chemistry |
subjects | Aerosols Analysis methods Applied sciences Atmospheric pollution Design Exact sciences and technology Pollution Q1 |
title | Development and Evaluation of a Low Cutpoint Virtual Impactor |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-11T22%3A45%3A52IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_pasca&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Development%20and%20Evaluation%20of%20a%20Low%20Cutpoint%20Virtual%20Impactor&rft.jtitle=Aerosol%20science%20and%20technology&rft.au=Sioutas,%20C.&rft.date=1994-01-01&rft.volume=21&rft.issue=3&rft.spage=223&rft.epage=235&rft.pages=223-235&rft.issn=0278-6826&rft.eissn=1521-7388&rft.coden=ASTYDQ&rft_id=info:doi/10.1080/02786829408959711&rft_dat=%3Cproquest_pasca%3E149196%3C/proquest_pasca%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=16898247&rft_id=info:pmid/&rfr_iscdi=true |