Design and control of helicopter main reducer vibration isolation platform with magnetorheological dampers
A magnetorheological vibration isolation platform (MRVIP) with cubic structure Stewart mechanism was designed and an effective semiactive control strategy was proposed based on its inverse kinematics characteristics for the helicopter to effectively reduce the vibration of the helicopter rotor trans...
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| Veröffentlicht in: | International journal of mechanics and materials in design 2021-06, Vol.17 (2), p.345-366 |
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| container_end_page | 366 |
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| container_issue | 2 |
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| container_title | International journal of mechanics and materials in design |
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| creator | Jiang, Min Rui, Xiaoting Zhu, Wei Yang, Fufeng Zhang, Yanni |
| description | A magnetorheological vibration isolation platform (MRVIP) with cubic structure Stewart mechanism was designed and an effective semiactive control strategy was proposed based on its inverse kinematics characteristics for the helicopter to effectively reduce the vibration of the helicopter rotor transmitted from the main reducer to the fuselage. Firstly, the structural scheme of the helicopter main reducer MRVIP was proposed. Secondly, the MR damper was manufactured, and the dynamic model was established based on the mechanical test. Thirdly, according to the design requirements of the VIP, the overall structure of the MRVIP was designed. Fourthly, the dynamic simulation model of the MRVIP was established by using 3D drawing software and SimMechanics software. And the vibration characteristics of each direction were analyzed. Finally, a PID-Fuzzy semiactive controller was designed based on the characteristics of the MR damper to improve the performance of the MRVIP. The numerical analysis results showed that compared with the passive MRVIP and the MRVIP based on fuzzy control, the MRVIP with PID-Fuzzy control has the best vibration isolation performance and can effectively reduce the vibration of 6-DOF. |
| doi_str_mv | 10.1007/s10999-021-09529-x |
| format | Article |
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Firstly, the structural scheme of the helicopter main reducer MRVIP was proposed. Secondly, the MR damper was manufactured, and the dynamic model was established based on the mechanical test. Thirdly, according to the design requirements of the VIP, the overall structure of the MRVIP was designed. Fourthly, the dynamic simulation model of the MRVIP was established by using 3D drawing software and SimMechanics software. And the vibration characteristics of each direction were analyzed. Finally, a PID-Fuzzy semiactive controller was designed based on the characteristics of the MR damper to improve the performance of the MRVIP. The numerical analysis results showed that compared with the passive MRVIP and the MRVIP based on fuzzy control, the MRVIP with PID-Fuzzy control has the best vibration isolation performance and can effectively reduce the vibration of 6-DOF.</description><identifier>ISSN: 1569-1713</identifier><identifier>EISSN: 1573-8841</identifier><identifier>DOI: 10.1007/s10999-021-09529-x</identifier><language>eng</language><publisher>Dordrecht: Springer Netherlands</publisher><subject>Airframes ; Characterization and Evaluation of Materials ; Classical Mechanics ; Control systems design ; Dampers ; Design ; Dynamic models ; Engineering ; Engineering Design ; Fuselages ; Fuzzy control ; Helicopter control ; Helicopter design ; Inverse kinematics ; Mechanical tests ; Numerical analysis ; Performance enhancement ; Proportional integral derivative ; Rotary wings ; Semiactive damping ; Software ; Solid Mechanics ; Vibration analysis ; Vibration control ; Vibration isolators</subject><ispartof>International journal of mechanics and materials in design, 2021-06, Vol.17 (2), p.345-366</ispartof><rights>The Author(s), under exclusive licence to Springer Nature B.V. part of Springer Nature 2021</rights><rights>The Author(s), under exclusive licence to Springer Nature B.V. part of Springer Nature 2021.</rights><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c319t-5aaba7917b5a15caafdf4522da99b56d3453b821d284d82df8aa856023282b303</citedby><cites>FETCH-LOGICAL-c319t-5aaba7917b5a15caafdf4522da99b56d3453b821d284d82df8aa856023282b303</cites><orcidid>0000-0002-6114-7685</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1007/s10999-021-09529-x$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1007/s10999-021-09529-x$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,776,780,27903,27904,41467,42536,51297</link.rule.ids></links><search><creatorcontrib>Jiang, Min</creatorcontrib><creatorcontrib>Rui, Xiaoting</creatorcontrib><creatorcontrib>Zhu, Wei</creatorcontrib><creatorcontrib>Yang, Fufeng</creatorcontrib><creatorcontrib>Zhang, Yanni</creatorcontrib><title>Design and control of helicopter main reducer vibration isolation platform with magnetorheological dampers</title><title>International journal of mechanics and materials in design</title><addtitle>Int J Mech Mater Des</addtitle><description>A magnetorheological vibration isolation platform (MRVIP) with cubic structure Stewart mechanism was designed and an effective semiactive control strategy was proposed based on its inverse kinematics characteristics for the helicopter to effectively reduce the vibration of the helicopter rotor transmitted from the main reducer to the fuselage. Firstly, the structural scheme of the helicopter main reducer MRVIP was proposed. Secondly, the MR damper was manufactured, and the dynamic model was established based on the mechanical test. Thirdly, according to the design requirements of the VIP, the overall structure of the MRVIP was designed. Fourthly, the dynamic simulation model of the MRVIP was established by using 3D drawing software and SimMechanics software. And the vibration characteristics of each direction were analyzed. Finally, a PID-Fuzzy semiactive controller was designed based on the characteristics of the MR damper to improve the performance of the MRVIP. The numerical analysis results showed that compared with the passive MRVIP and the MRVIP based on fuzzy control, the MRVIP with PID-Fuzzy control has the best vibration isolation performance and can effectively reduce the vibration of 6-DOF.</description><subject>Airframes</subject><subject>Characterization and Evaluation of Materials</subject><subject>Classical Mechanics</subject><subject>Control systems design</subject><subject>Dampers</subject><subject>Design</subject><subject>Dynamic models</subject><subject>Engineering</subject><subject>Engineering Design</subject><subject>Fuselages</subject><subject>Fuzzy control</subject><subject>Helicopter control</subject><subject>Helicopter design</subject><subject>Inverse kinematics</subject><subject>Mechanical tests</subject><subject>Numerical analysis</subject><subject>Performance enhancement</subject><subject>Proportional integral derivative</subject><subject>Rotary wings</subject><subject>Semiactive damping</subject><subject>Software</subject><subject>Solid Mechanics</subject><subject>Vibration analysis</subject><subject>Vibration control</subject><subject>Vibration isolators</subject><issn>1569-1713</issn><issn>1573-8841</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><recordid>eNp9kMtOwzAURC0EEqXwA6wssTb4ETf2EpWnVIkNrK2b2EldpXGwUyh_j0uQ2LGaudLMXOkgdMnoNaO0vEmMaq0J5YxQLbkm-yM0Y7IURKmCHR_8QhNWMnGKzlLaUCooU2qGNncu-bbH0Ftch36MocOhwWvX-ToMo4t4C77H0dldnY8PX0UYfeixT6Gb3JC1CXGLP_24zvG2d2OIaxe60PoaOmxhO7iYztFJA11yF786R28P96_LJ7J6eXxe3q5ILZgeiQSooNSsrCQwWQM0tikk5xa0ruTCikKKSnFmuSqs4rZRAEouKBdc8UpQMUdX0-4Qw_vOpdFswi72-aXhGQ3XJZOHFJ9SdQwpRdeYIfotxC_DqDkwNRNTk5maH6Zmn0tiKqUc7lsX_6b_aX0DQAp8ug</recordid><startdate>20210601</startdate><enddate>20210601</enddate><creator>Jiang, Min</creator><creator>Rui, Xiaoting</creator><creator>Zhu, Wei</creator><creator>Yang, Fufeng</creator><creator>Zhang, Yanni</creator><general>Springer Netherlands</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><orcidid>https://orcid.org/0000-0002-6114-7685</orcidid></search><sort><creationdate>20210601</creationdate><title>Design and control of helicopter main reducer vibration isolation platform with magnetorheological dampers</title><author>Jiang, Min ; Rui, Xiaoting ; Zhu, Wei ; Yang, Fufeng ; Zhang, Yanni</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c319t-5aaba7917b5a15caafdf4522da99b56d3453b821d284d82df8aa856023282b303</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Airframes</topic><topic>Characterization and Evaluation of Materials</topic><topic>Classical Mechanics</topic><topic>Control systems design</topic><topic>Dampers</topic><topic>Design</topic><topic>Dynamic models</topic><topic>Engineering</topic><topic>Engineering Design</topic><topic>Fuselages</topic><topic>Fuzzy control</topic><topic>Helicopter control</topic><topic>Helicopter design</topic><topic>Inverse kinematics</topic><topic>Mechanical tests</topic><topic>Numerical analysis</topic><topic>Performance enhancement</topic><topic>Proportional integral derivative</topic><topic>Rotary wings</topic><topic>Semiactive damping</topic><topic>Software</topic><topic>Solid Mechanics</topic><topic>Vibration analysis</topic><topic>Vibration control</topic><topic>Vibration isolators</topic><toplevel>online_resources</toplevel><creatorcontrib>Jiang, Min</creatorcontrib><creatorcontrib>Rui, Xiaoting</creatorcontrib><creatorcontrib>Zhu, Wei</creatorcontrib><creatorcontrib>Yang, Fufeng</creatorcontrib><creatorcontrib>Zhang, Yanni</creatorcontrib><collection>CrossRef</collection><jtitle>International journal of mechanics and materials in design</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Jiang, Min</au><au>Rui, Xiaoting</au><au>Zhu, Wei</au><au>Yang, Fufeng</au><au>Zhang, Yanni</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Design and control of helicopter main reducer vibration isolation platform with magnetorheological dampers</atitle><jtitle>International journal of mechanics and materials in design</jtitle><stitle>Int J Mech Mater Des</stitle><date>2021-06-01</date><risdate>2021</risdate><volume>17</volume><issue>2</issue><spage>345</spage><epage>366</epage><pages>345-366</pages><issn>1569-1713</issn><eissn>1573-8841</eissn><abstract>A magnetorheological vibration isolation platform (MRVIP) with cubic structure Stewart mechanism was designed and an effective semiactive control strategy was proposed based on its inverse kinematics characteristics for the helicopter to effectively reduce the vibration of the helicopter rotor transmitted from the main reducer to the fuselage. Firstly, the structural scheme of the helicopter main reducer MRVIP was proposed. Secondly, the MR damper was manufactured, and the dynamic model was established based on the mechanical test. Thirdly, according to the design requirements of the VIP, the overall structure of the MRVIP was designed. Fourthly, the dynamic simulation model of the MRVIP was established by using 3D drawing software and SimMechanics software. And the vibration characteristics of each direction were analyzed. Finally, a PID-Fuzzy semiactive controller was designed based on the characteristics of the MR damper to improve the performance of the MRVIP. The numerical analysis results showed that compared with the passive MRVIP and the MRVIP based on fuzzy control, the MRVIP with PID-Fuzzy control has the best vibration isolation performance and can effectively reduce the vibration of 6-DOF.</abstract><cop>Dordrecht</cop><pub>Springer Netherlands</pub><doi>10.1007/s10999-021-09529-x</doi><tpages>22</tpages><orcidid>https://orcid.org/0000-0002-6114-7685</orcidid></addata></record> |
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| subjects | Airframes Characterization and Evaluation of Materials Classical Mechanics Control systems design Dampers Design Dynamic models Engineering Engineering Design Fuselages Fuzzy control Helicopter control Helicopter design Inverse kinematics Mechanical tests Numerical analysis Performance enhancement Proportional integral derivative Rotary wings Semiactive damping Software Solid Mechanics Vibration analysis Vibration control Vibration isolators |
| title | Design and control of helicopter main reducer vibration isolation platform with magnetorheological dampers |
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