A Method of Working Process Parameter Optimization of a Unified Engine Core and a Gas Turbine Engine Family Being Created on Its Basis
This paper describes a method for multicriteria optimization of parameters for both the engine core and engine family with modeling the engine operation as a part of aircraft system.
Gespeichert in:
| Veröffentlicht in: | Russian aeronautics 2018, Vol.61 (1), p.78-83 |
|---|---|
| Hauptverfasser: | , , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 83 |
|---|---|
| container_issue | 1 |
| container_start_page | 78 |
| container_title | Russian aeronautics |
| container_volume | 61 |
| creator | Rybakov, V. N. Kuz’michev, V. S. Tkachenko, A. Yu Krupenich, I. N. |
| description | This paper describes a method for multicriteria optimization of parameters for both the engine core and engine family with modeling the engine operation as a part of aircraft system. |
| doi_str_mv | 10.3103/S1068799818010129 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2065445284</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2065445284</sourcerecordid><originalsourceid>FETCH-LOGICAL-c2319-fd16394a1dfa50f99f4ef2871aed7a1812cd4ee698312b3800b8c7e7e2ec08d53</originalsourceid><addsrcrecordid>eNp1kE9PAjEQxTdGExH9AN6aeF7tdP-1R9gAkmAgEeJxU3anWGS32C4H_AB-bruBxIPxNJP5vfcmeUFwD_QxAho9vQJNeSYEB06BAhMXQQ9EFIeZoHDpd4_Djl8HN85tKU1SFrNe8D0gL9i-m4oYRd6M_dDNhiysKdE5spBW1tiiJfN9q2v9JVttmk4pyarRSmNFRs1GN0hyY5HIpvJkIh1ZHuy6O5_pWNZ6dyRD7NJzi7L1Tp80bR0ZSqfdbXCl5M7h3Xn2g9V4tMyfw9l8Ms0Hs7BkEYhQVZBGIpZQKZlQJYSKUTGegcQqk8CBlVWMmAoeAVtHnNI1LzPMkGFJeZVE_eDhlLu35vOAri225mAb_7JgNE3iOGE89io4qUprnLOoir3VtbTHAmjR1V38qdt72MnjvLbZoP1N_t_0A18rgPY</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2065445284</pqid></control><display><type>article</type><title>A Method of Working Process Parameter Optimization of a Unified Engine Core and a Gas Turbine Engine Family Being Created on Its Basis</title><source>Springer Nature - Complete Springer Journals</source><creator>Rybakov, V. N. ; Kuz’michev, V. S. ; Tkachenko, A. Yu ; Krupenich, I. N.</creator><creatorcontrib>Rybakov, V. N. ; Kuz’michev, V. S. ; Tkachenko, A. Yu ; Krupenich, I. N.</creatorcontrib><description>This paper describes a method for multicriteria optimization of parameters for both the engine core and engine family with modeling the engine operation as a part of aircraft system.</description><identifier>ISSN: 1068-7998</identifier><identifier>EISSN: 1934-7901</identifier><identifier>DOI: 10.3103/S1068799818010129</identifier><language>eng</language><publisher>Moscow: Pleiades Publishing</publisher><subject>Aircraft and Rocket Engine Theory ; Aircraft components ; Automotive Engineering ; Engineering ; Gas turbine engines ; Optimization ; Process parameters</subject><ispartof>Russian aeronautics, 2018, Vol.61 (1), p.78-83</ispartof><rights>Allerton Press, Inc. 2018</rights><rights>Copyright Springer Science & Business Media 2018</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c2319-fd16394a1dfa50f99f4ef2871aed7a1812cd4ee698312b3800b8c7e7e2ec08d53</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.3103/S1068799818010129$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.3103/S1068799818010129$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,776,780,27903,27904,41467,42536,51297</link.rule.ids></links><search><creatorcontrib>Rybakov, V. N.</creatorcontrib><creatorcontrib>Kuz’michev, V. S.</creatorcontrib><creatorcontrib>Tkachenko, A. Yu</creatorcontrib><creatorcontrib>Krupenich, I. N.</creatorcontrib><title>A Method of Working Process Parameter Optimization of a Unified Engine Core and a Gas Turbine Engine Family Being Created on Its Basis</title><title>Russian aeronautics</title><addtitle>Russ. Aeronaut</addtitle><description>This paper describes a method for multicriteria optimization of parameters for both the engine core and engine family with modeling the engine operation as a part of aircraft system.</description><subject>Aircraft and Rocket Engine Theory</subject><subject>Aircraft components</subject><subject>Automotive Engineering</subject><subject>Engineering</subject><subject>Gas turbine engines</subject><subject>Optimization</subject><subject>Process parameters</subject><issn>1068-7998</issn><issn>1934-7901</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2018</creationdate><recordtype>article</recordtype><recordid>eNp1kE9PAjEQxTdGExH9AN6aeF7tdP-1R9gAkmAgEeJxU3anWGS32C4H_AB-bruBxIPxNJP5vfcmeUFwD_QxAho9vQJNeSYEB06BAhMXQQ9EFIeZoHDpd4_Djl8HN85tKU1SFrNe8D0gL9i-m4oYRd6M_dDNhiysKdE5spBW1tiiJfN9q2v9JVttmk4pyarRSmNFRs1GN0hyY5HIpvJkIh1ZHuy6O5_pWNZ6dyRD7NJzi7L1Tp80bR0ZSqfdbXCl5M7h3Xn2g9V4tMyfw9l8Ms0Hs7BkEYhQVZBGIpZQKZlQJYSKUTGegcQqk8CBlVWMmAoeAVtHnNI1LzPMkGFJeZVE_eDhlLu35vOAri225mAb_7JgNE3iOGE89io4qUprnLOoir3VtbTHAmjR1V38qdt72MnjvLbZoP1N_t_0A18rgPY</recordid><startdate>2018</startdate><enddate>2018</enddate><creator>Rybakov, V. N.</creator><creator>Kuz’michev, V. S.</creator><creator>Tkachenko, A. Yu</creator><creator>Krupenich, I. N.</creator><general>Pleiades Publishing</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>2018</creationdate><title>A Method of Working Process Parameter Optimization of a Unified Engine Core and a Gas Turbine Engine Family Being Created on Its Basis</title><author>Rybakov, V. N. ; Kuz’michev, V. S. ; Tkachenko, A. Yu ; Krupenich, I. N.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c2319-fd16394a1dfa50f99f4ef2871aed7a1812cd4ee698312b3800b8c7e7e2ec08d53</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2018</creationdate><topic>Aircraft and Rocket Engine Theory</topic><topic>Aircraft components</topic><topic>Automotive Engineering</topic><topic>Engineering</topic><topic>Gas turbine engines</topic><topic>Optimization</topic><topic>Process parameters</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Rybakov, V. N.</creatorcontrib><creatorcontrib>Kuz’michev, V. S.</creatorcontrib><creatorcontrib>Tkachenko, A. Yu</creatorcontrib><creatorcontrib>Krupenich, I. N.</creatorcontrib><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Russian aeronautics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Rybakov, V. N.</au><au>Kuz’michev, V. S.</au><au>Tkachenko, A. Yu</au><au>Krupenich, I. N.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A Method of Working Process Parameter Optimization of a Unified Engine Core and a Gas Turbine Engine Family Being Created on Its Basis</atitle><jtitle>Russian aeronautics</jtitle><stitle>Russ. Aeronaut</stitle><date>2018</date><risdate>2018</risdate><volume>61</volume><issue>1</issue><spage>78</spage><epage>83</epage><pages>78-83</pages><issn>1068-7998</issn><eissn>1934-7901</eissn><abstract>This paper describes a method for multicriteria optimization of parameters for both the engine core and engine family with modeling the engine operation as a part of aircraft system.</abstract><cop>Moscow</cop><pub>Pleiades Publishing</pub><doi>10.3103/S1068799818010129</doi><tpages>6</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 1068-7998 |
| ispartof | Russian aeronautics, 2018, Vol.61 (1), p.78-83 |
| issn | 1068-7998 1934-7901 |
| language | eng |
| recordid | cdi_proquest_journals_2065445284 |
| source | Springer Nature - Complete Springer Journals |
| subjects | Aircraft and Rocket Engine Theory Aircraft components Automotive Engineering Engineering Gas turbine engines Optimization Process parameters |
| title | A Method of Working Process Parameter Optimization of a Unified Engine Core and a Gas Turbine Engine Family Being Created on Its Basis |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-24T23%3A07%3A18IST&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=A%20Method%20of%20Working%20Process%20Parameter%20Optimization%20of%20a%20Unified%20Engine%20Core%20and%20a%20Gas%20Turbine%20Engine%20Family%20Being%20Created%20on%20Its%20Basis&rft.jtitle=Russian%20aeronautics&rft.au=Rybakov,%20V.%20N.&rft.date=2018&rft.volume=61&rft.issue=1&rft.spage=78&rft.epage=83&rft.pages=78-83&rft.issn=1068-7998&rft.eissn=1934-7901&rft_id=info:doi/10.3103/S1068799818010129&rft_dat=%3Cproquest_cross%3E2065445284%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=2065445284&rft_id=info:pmid/&rfr_iscdi=true |