Monitoring Helicopter Swash Plates Assemblies by Integration of Ferrography and Atomic Emission Spectrometry
Helicopters Swash Plates Assembly allows helicopter steering movement and is defined as a safety system. This system experiences wear and high loads during flight. Following a failure of an assembly that caused a helicopter forced landing, a novel method was developed to monitor the system for early...
Gespeichert in:
| Veröffentlicht in: | Journal of failure analysis and prevention 2022-08, Vol.22 (4), p.1442-1456 |
|---|---|
| Hauptverfasser: | , , , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 1456 |
|---|---|
| container_issue | 4 |
| container_start_page | 1442 |
| container_title | Journal of failure analysis and prevention |
| container_volume | 22 |
| creator | Kruchinin, R. Baron, G. Fishman, D. Shemesh, G. Levi, O. |
| description | Helicopters Swash Plates Assembly allows helicopter steering movement and is defined as a safety system. This system experiences wear and high loads during flight. Following a failure of an assembly that caused a helicopter forced landing, a novel method was developed to monitor the system for early warning based on integration of the Ferrography and Atomic Emission Spectrometry methods. The critical values of metal concentration and particle size in a sample were determined for Ferrography and Atomic Emission Spectrometry methods, respectively. The valuable results allowed developing a decision-making flowchart. The integration of the methods yielded complementary detectability and extended detection range. Over a period of 7.5 years, 37 different assemblies were monitored, yielding a wide data base of 1618 samples. Recently, four assemblies were removed from helicopters following the method alerts and found as True Positive cases, in addition one control assembly was dismantled and found True Negative. Nowadays, this method is implemented on helicopters in service. |
| doi_str_mv | 10.1007/s11668-022-01409-6 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2719458786</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2719458786</sourcerecordid><originalsourceid>FETCH-LOGICAL-c270t-8e0f14c9dcc3c97bfb39237d925d30d62b94eb12138c320c9dcb04952399c0653</originalsourceid><addsrcrecordid>eNp9kF1LwzAUhoMoOKd_wKuA19F8tWkux9jcYKIwvQ5tmm4ZbVOTDOm_t7WCd16d98DzngMPAPcEPxKMxVMgJE0zhClFmHAsUXoBZkTQDCWp4JdDTrhAAlN5DW5COGHMEsLpDNQvrrXRedse4MbUVrsuGg_3X3k4wrc6jybARQimKWo7xKKH2zaag8-jdS10FVwb792wd8ce5m0JF9E1VsNVY0MYkX1ndPSuMdH3t-Cqyutg7n7nHHysV-_LDdq9Pm-Xix3SVOCIMoMrwrUstWZaiqIqmKRMlJImJcNlSgvJTUEoYZlmFI9ggblMKJNS4zRhc_Aw3e28-zybENXJnX07vFRUEMmTTGTpQNGJ0t6F4E2lOm-b3PeKYDVaVZNVNVhVP1bVWGJTKXSjM-P_Tv_T-gbjZHuT</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2719458786</pqid></control><display><type>article</type><title>Monitoring Helicopter Swash Plates Assemblies by Integration of Ferrography and Atomic Emission Spectrometry</title><source>SpringerLink Journals</source><creator>Kruchinin, R. ; Baron, G. ; Fishman, D. ; Shemesh, G. ; Levi, O.</creator><creatorcontrib>Kruchinin, R. ; Baron, G. ; Fishman, D. ; Shemesh, G. ; Levi, O.</creatorcontrib><description>Helicopters Swash Plates Assembly allows helicopter steering movement and is defined as a safety system. This system experiences wear and high loads during flight. Following a failure of an assembly that caused a helicopter forced landing, a novel method was developed to monitor the system for early warning based on integration of the Ferrography and Atomic Emission Spectrometry methods. The critical values of metal concentration and particle size in a sample were determined for Ferrography and Atomic Emission Spectrometry methods, respectively. The valuable results allowed developing a decision-making flowchart. The integration of the methods yielded complementary detectability and extended detection range. Over a period of 7.5 years, 37 different assemblies were monitored, yielding a wide data base of 1618 samples. Recently, four assemblies were removed from helicopters following the method alerts and found as True Positive cases, in addition one control assembly was dismantled and found True Negative. Nowadays, this method is implemented on helicopters in service.</description><identifier>ISSN: 1547-7029</identifier><identifier>EISSN: 1728-5674</identifier><identifier>EISSN: 1864-1245</identifier><identifier>DOI: 10.1007/s11668-022-01409-6</identifier><language>eng</language><publisher>New York: Springer US</publisher><subject>Assemblies ; Assembly ; Characterization and Evaluation of Materials ; Chemistry and Materials Science ; Classical Mechanics ; Corrosion and Coatings ; Decision making ; Early warning systems ; Emission ; Ferrography ; Flow charts ; Helicopters ; Materials Science ; Quality Control ; Reliability ; Safety and Risk ; Scientific imaging ; Solid Mechanics ; Spectrometry ; Spectroscopy ; Steering ; Swash plate mechanisms ; Technical Article---Peer-Reviewed ; Tribology</subject><ispartof>Journal of failure analysis and prevention, 2022-08, Vol.22 (4), p.1442-1456</ispartof><rights>ASM International 2022</rights><rights>ASM International 2022.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c270t-8e0f14c9dcc3c97bfb39237d925d30d62b94eb12138c320c9dcb04952399c0653</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids></links><search><creatorcontrib>Kruchinin, R.</creatorcontrib><creatorcontrib>Baron, G.</creatorcontrib><creatorcontrib>Fishman, D.</creatorcontrib><creatorcontrib>Shemesh, G.</creatorcontrib><creatorcontrib>Levi, O.</creatorcontrib><title>Monitoring Helicopter Swash Plates Assemblies by Integration of Ferrography and Atomic Emission Spectrometry</title><title>Journal of failure analysis and prevention</title><addtitle>J Fail. Anal. and Preven</addtitle><description>Helicopters Swash Plates Assembly allows helicopter steering movement and is defined as a safety system. This system experiences wear and high loads during flight. Following a failure of an assembly that caused a helicopter forced landing, a novel method was developed to monitor the system for early warning based on integration of the Ferrography and Atomic Emission Spectrometry methods. The critical values of metal concentration and particle size in a sample were determined for Ferrography and Atomic Emission Spectrometry methods, respectively. The valuable results allowed developing a decision-making flowchart. The integration of the methods yielded complementary detectability and extended detection range. Over a period of 7.5 years, 37 different assemblies were monitored, yielding a wide data base of 1618 samples. Recently, four assemblies were removed from helicopters following the method alerts and found as True Positive cases, in addition one control assembly was dismantled and found True Negative. Nowadays, this method is implemented on helicopters in service.</description><subject>Assemblies</subject><subject>Assembly</subject><subject>Characterization and Evaluation of Materials</subject><subject>Chemistry and Materials Science</subject><subject>Classical Mechanics</subject><subject>Corrosion and Coatings</subject><subject>Decision making</subject><subject>Early warning systems</subject><subject>Emission</subject><subject>Ferrography</subject><subject>Flow charts</subject><subject>Helicopters</subject><subject>Materials Science</subject><subject>Quality Control</subject><subject>Reliability</subject><subject>Safety and Risk</subject><subject>Scientific imaging</subject><subject>Solid Mechanics</subject><subject>Spectrometry</subject><subject>Spectroscopy</subject><subject>Steering</subject><subject>Swash plate mechanisms</subject><subject>Technical Article---Peer-Reviewed</subject><subject>Tribology</subject><issn>1547-7029</issn><issn>1728-5674</issn><issn>1864-1245</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNp9kF1LwzAUhoMoOKd_wKuA19F8tWkux9jcYKIwvQ5tmm4ZbVOTDOm_t7WCd16d98DzngMPAPcEPxKMxVMgJE0zhClFmHAsUXoBZkTQDCWp4JdDTrhAAlN5DW5COGHMEsLpDNQvrrXRedse4MbUVrsuGg_3X3k4wrc6jybARQimKWo7xKKH2zaag8-jdS10FVwb792wd8ce5m0JF9E1VsNVY0MYkX1ndPSuMdH3t-Cqyutg7n7nHHysV-_LDdq9Pm-Xix3SVOCIMoMrwrUstWZaiqIqmKRMlJImJcNlSgvJTUEoYZlmFI9ggblMKJNS4zRhc_Aw3e28-zybENXJnX07vFRUEMmTTGTpQNGJ0t6F4E2lOm-b3PeKYDVaVZNVNVhVP1bVWGJTKXSjM-P_Tv_T-gbjZHuT</recordid><startdate>20220801</startdate><enddate>20220801</enddate><creator>Kruchinin, R.</creator><creator>Baron, G.</creator><creator>Fishman, D.</creator><creator>Shemesh, G.</creator><creator>Levi, O.</creator><general>Springer US</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>7TA</scope><scope>7TB</scope><scope>8BQ</scope><scope>8FD</scope><scope>FR3</scope><scope>JG9</scope><scope>KR7</scope></search><sort><creationdate>20220801</creationdate><title>Monitoring Helicopter Swash Plates Assemblies by Integration of Ferrography and Atomic Emission Spectrometry</title><author>Kruchinin, R. ; Baron, G. ; Fishman, D. ; Shemesh, G. ; Levi, O.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c270t-8e0f14c9dcc3c97bfb39237d925d30d62b94eb12138c320c9dcb04952399c0653</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Assemblies</topic><topic>Assembly</topic><topic>Characterization and Evaluation of Materials</topic><topic>Chemistry and Materials Science</topic><topic>Classical Mechanics</topic><topic>Corrosion and Coatings</topic><topic>Decision making</topic><topic>Early warning systems</topic><topic>Emission</topic><topic>Ferrography</topic><topic>Flow charts</topic><topic>Helicopters</topic><topic>Materials Science</topic><topic>Quality Control</topic><topic>Reliability</topic><topic>Safety and Risk</topic><topic>Scientific imaging</topic><topic>Solid Mechanics</topic><topic>Spectrometry</topic><topic>Spectroscopy</topic><topic>Steering</topic><topic>Swash plate mechanisms</topic><topic>Technical Article---Peer-Reviewed</topic><topic>Tribology</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Kruchinin, R.</creatorcontrib><creatorcontrib>Baron, G.</creatorcontrib><creatorcontrib>Fishman, D.</creatorcontrib><creatorcontrib>Shemesh, G.</creatorcontrib><creatorcontrib>Levi, O.</creatorcontrib><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Materials Business File</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Materials Research Database</collection><collection>Civil Engineering Abstracts</collection><jtitle>Journal of failure analysis and prevention</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Kruchinin, R.</au><au>Baron, G.</au><au>Fishman, D.</au><au>Shemesh, G.</au><au>Levi, O.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Monitoring Helicopter Swash Plates Assemblies by Integration of Ferrography and Atomic Emission Spectrometry</atitle><jtitle>Journal of failure analysis and prevention</jtitle><stitle>J Fail. Anal. and Preven</stitle><date>2022-08-01</date><risdate>2022</risdate><volume>22</volume><issue>4</issue><spage>1442</spage><epage>1456</epage><pages>1442-1456</pages><issn>1547-7029</issn><eissn>1728-5674</eissn><eissn>1864-1245</eissn><abstract>Helicopters Swash Plates Assembly allows helicopter steering movement and is defined as a safety system. This system experiences wear and high loads during flight. Following a failure of an assembly that caused a helicopter forced landing, a novel method was developed to monitor the system for early warning based on integration of the Ferrography and Atomic Emission Spectrometry methods. The critical values of metal concentration and particle size in a sample were determined for Ferrography and Atomic Emission Spectrometry methods, respectively. The valuable results allowed developing a decision-making flowchart. The integration of the methods yielded complementary detectability and extended detection range. Over a period of 7.5 years, 37 different assemblies were monitored, yielding a wide data base of 1618 samples. Recently, four assemblies were removed from helicopters following the method alerts and found as True Positive cases, in addition one control assembly was dismantled and found True Negative. Nowadays, this method is implemented on helicopters in service.</abstract><cop>New York</cop><pub>Springer US</pub><doi>10.1007/s11668-022-01409-6</doi><tpages>15</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 1547-7029 |
| ispartof | Journal of failure analysis and prevention, 2022-08, Vol.22 (4), p.1442-1456 |
| issn | 1547-7029 1728-5674 1864-1245 |
| language | eng |
| recordid | cdi_proquest_journals_2719458786 |
| source | SpringerLink Journals |
| subjects | Assemblies Assembly Characterization and Evaluation of Materials Chemistry and Materials Science Classical Mechanics Corrosion and Coatings Decision making Early warning systems Emission Ferrography Flow charts Helicopters Materials Science Quality Control Reliability Safety and Risk Scientific imaging Solid Mechanics Spectrometry Spectroscopy Steering Swash plate mechanisms Technical Article---Peer-Reviewed Tribology |
| title | Monitoring Helicopter Swash Plates Assemblies by Integration of Ferrography and Atomic Emission Spectrometry |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-14T10%3A19%3A33IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Monitoring%20Helicopter%20Swash%20Plates%20Assemblies%20by%20Integration%20of%20Ferrography%20and%20Atomic%20Emission%20Spectrometry&rft.jtitle=Journal%20of%20failure%20analysis%20and%20prevention&rft.au=Kruchinin,%20R.&rft.date=2022-08-01&rft.volume=22&rft.issue=4&rft.spage=1442&rft.epage=1456&rft.pages=1442-1456&rft.issn=1547-7029&rft.eissn=1728-5674&rft_id=info:doi/10.1007/s11668-022-01409-6&rft_dat=%3Cproquest_cross%3E2719458786%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2719458786&rft_id=info:pmid/&rfr_iscdi=true |