{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2025,3,3]],"date-time":"2025-03-03T05:34:27Z","timestamp":1740980067120,"version":"3.38.0"},"reference-count":19,"publisher":"SAGE Publications","issue":"7","license":[{"start":{"date-parts":[[2022,4,5]],"date-time":"2022-04-05T00:00:00Z","timestamp":1649116800000},"content-version":"tdm","delay-in-days":0,"URL":"https:\/\/journals.sagepub.com\/page\/policies\/text-and-data-mining-license"}],"funder":[{"DOI":"10.13039\/501100018537","name":"National Science and Technology Major Project","doi-asserted-by":"publisher","award":["J2019-I-0020-0019"],"award-info":[{"award-number":["J2019-I-0020-0019"]}],"id":[{"id":"10.13039\/501100018537","id-type":"DOI","asserted-by":"publisher"}]}],"content-domain":{"domain":["journals.sagepub.com"],"crossmark-restriction":true},"short-container-title":["Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering"],"published-print":{"date-parts":[[2022,8]]},"abstract":"<jats:p> In order to solve the problem of torsional vibration instability of the control system for turboshaft engine caused by low-order torsional vibration modal drift under variable rotor speed effectively, an adaptive torsional vibration suppression method based on the least mean square algorithm is proposed and designed. First, based on Lagrange equation and state space method, the structural dynamic model of torque transmission chain system is established, which takes into account fixed and variable gear ratio. It is beneficial to express the dynamic characteristics of torsional vibration in real time, so that the variation laws of low-order torsional vibration modal under variable rotor speed and gear ratio are revealed. Then, an adaptive torsional vibration filter based on least mean square algorithm is proposed and designed combined with the active control objective of helicopter power system. Finally, the effectiveness of adaptive torsional vibration suppression method is validated based on numerical simulation and hardware-in-loop simulation separately. The results show that compared with the conventional constant-coefficient notch filter, the adaptive torsional vibration filter can decrease the peaks of all low-order torsional vibration frequency by more than 50%. It proves better robustness, more remarkable effectiveness and superior adaptive ability of the adaptive torsional vibration suppression method. <\/jats:p>","DOI":"10.1177\/09596518221087519","type":"journal-article","created":{"date-parts":[[2022,4,5]],"date-time":"2022-04-05T10:42:09Z","timestamp":1649155329000},"page":"1324-1334","update-policy":"https:\/\/doi.org\/10.1177\/sage-journals-update-policy","source":"Crossref","is-referenced-by-count":0,"title":["Design and test of adaptive torsional vibration suppression method for helicopter power system with variable rotor speed"],"prefix":"10.1177","volume":"236","author":[{"ORCID":"https:\/\/orcid.org\/0000-0003-0868-5465","authenticated-orcid":false,"given":"Yong","family":"Wang","sequence":"first","affiliation":[{"name":"College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China"}]},{"given":"Kaiming","family":"Huang","sequence":"additional","affiliation":[{"name":"China Aviation Powerplant Research Institute, AECC, Zhuzhou, China"}]},{"given":"Yerong","family":"Peng","sequence":"additional","affiliation":[{"name":"Nanjing University of Aeronautics and Astronautics, Nanjing, China"}]},{"ORCID":"https:\/\/orcid.org\/0000-0003-1285-4620","authenticated-orcid":false,"given":"Jie","family":"Song","sequence":"additional","affiliation":[{"name":"Nanjing University of Aeronautics and Astronautics, Nanjing, China"}]},{"ORCID":"https:\/\/orcid.org\/0000-0001-9165-9211","authenticated-orcid":false,"given":"Haibo","family":"Zhang","sequence":"additional","affiliation":[{"name":"Nanjing University of Aeronautics and Astronautics, Nanjing, China"}]}],"member":"179","published-online":{"date-parts":[[2022,4,5]]},"reference":[{"volume-title":"ASME 1995 international gas turbine and aeroengine congress and exposition","author":"Wong TH","key":"bibr1-09596518221087519"},{"volume-title":"Proceedings of the ASME gas turbine conference","author":"Mist\u00e9 GA","key":"bibr2-09596518221087519"},{"volume-title":"Parametric instability investigation and stability based design for transmission systems containing face-gear drives","year":"2012","author":"Peng M","key":"bibr3-09596518221087519"},{"doi-asserted-by":"publisher","key":"bibr4-09596518221087519","DOI":"10.4050\/JAHS.43.76"},{"doi-asserted-by":"publisher","key":"bibr5-09596518221087519","DOI":"10.2514\/1.J050756"},{"doi-asserted-by":"publisher","key":"bibr6-09596518221087519","DOI":"10.1108\/AEAT-09-2012-0150"},{"volume-title":"Research on the integrated control method of variable speed helicopter\/engine under multiple configurations","year":"2020","author":"Chen M","key":"bibr7-09596518221087519"},{"volume-title":"57th annual forum of AHS","author":"Smith BJ","first-page":"1617","key":"bibr8-09596518221087519"},{"year":"2004","author":"Hu JZ","journal-title":"Methods and apparatus for estimating gas turbine engine governor dynamics","key":"bibr9-09596518221087519"},{"year":"2006","author":"Desai MC","journal-title":"Engine control system","key":"bibr10-09596518221087519"},{"issue":"3","key":"bibr11-09596518221087519","first-page":"606","volume":"21","author":"Li S","year":"2006","journal-title":"J Aerosp Power"},{"doi-asserted-by":"publisher","key":"bibr12-09596518221087519","DOI":"10.1007\/s13272-016-0191-6"},{"unstructured":"Welch GE, McVetta AB, Stevens MA, et al. Variable-speed power-turbine research at Glenn research center. NASA\/TM-2012-217605, 2012.","key":"bibr13-09596518221087519"},{"volume-title":"Proceedings of the American helicopter society 2nd international aeromechanics specialists conference","author":"Hopkins SA","key":"bibr14-09596518221087519"},{"issue":"1","key":"bibr15-09596518221087519","first-page":"158","volume":"38","author":"Miao LZ","year":"2017","journal-title":"J Prop Technol"},{"unstructured":"Hu HY. Basic mechanical vibration. 1st ed. Beijing, China: Beijing University of Aeronautics and Astronautics Press, 2005, pp.81\u201385.","key":"bibr16-09596518221087519"},{"issue":"5","key":"bibr17-09596518221087519","first-page":"360","volume":"8","author":"Mane V","year":"2011","journal-title":"Int J Comp Sci Iss"},{"issue":"5","key":"bibr18-09596518221087519","first-page":"2520","volume":"7","author":"Dixit S","year":"2017","journal-title":"Int J Electr Comput Eng"},{"issue":"1","key":"bibr19-09596518221087519","first-page":"139","volume":"28","author":"Khan S","year":"2016","journal-title":"Sci Int"}],"container-title":["Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering"],"original-title":[],"language":"en","link":[{"URL":"https:\/\/journals.sagepub.com\/doi\/pdf\/10.1177\/09596518221087519","content-type":"application\/pdf","content-version":"vor","intended-application":"text-mining"},{"URL":"https:\/\/journals.sagepub.com\/doi\/full-xml\/10.1177\/09596518221087519","content-type":"application\/xml","content-version":"vor","intended-application":"text-mining"},{"URL":"https:\/\/journals.sagepub.com\/doi\/pdf\/10.1177\/09596518221087519","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2025,3,2]],"date-time":"2025-03-02T09:49:42Z","timestamp":1740908982000},"score":1,"resource":{"primary":{"URL":"https:\/\/journals.sagepub.com\/doi\/10.1177\/09596518221087519"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2022,4,5]]},"references-count":19,"journal-issue":{"issue":"7","published-print":{"date-parts":[[2022,8]]}},"alternative-id":["10.1177\/09596518221087519"],"URL":"https:\/\/doi.org\/10.1177\/09596518221087519","relation":{},"ISSN":["0959-6518","2041-3041"],"issn-type":[{"type":"print","value":"0959-6518"},{"type":"electronic","value":"2041-3041"}],"subject":[],"published":{"date-parts":[[2022,4,5]]}}}