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- Publisher Website: 10.1109/ChiCC.2015.7259953
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Conference Paper: Application of inerter to aircraft landing gear suspension
Title | Application of inerter to aircraft landing gear suspension |
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Authors | |
Keywords | Aircraft landing gear Inerter Shimmy vibration Suspension |
Issue Date | 2015 |
Publisher | Institute of Electrical and Electronics Engineers. The Journal's web site is located at http://www.ieeexplore.ieee.org/xpl/conhome.jsp?punumber=1001331 |
Citation | The 34th Chinese Control Conference (CCC 2015), Hangzhou, China, 28-30 July 2015. In Chinese Control Conference, 2015, p. 2066-2071 How to Cite? |
Abstract | The inerter was recently proposed as a two-terminal mechanical element with the property that the force across the element is proportional to the relative acceleration of its two terminals. Improvement has been observed through introducing inerters into various suspension systems. In this paper, the investigation is focused on the shimmy vibration in the aircraft landing gears and the performance variation with the application of inerters. By the method of simulation, the performance changes have been observed and analyzed. |
Description | Open Access |
Persistent Identifier | http://hdl.handle.net/10722/217418 |
ISSN | 2020 SCImago Journal Rankings: 0.152 |
DC Field | Value | Language |
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dc.contributor.author | Dong, X | - |
dc.contributor.author | Liu, Y | - |
dc.contributor.author | Chen, MZ | - |
dc.date.accessioned | 2015-09-18T05:58:56Z | - |
dc.date.available | 2015-09-18T05:58:56Z | - |
dc.date.issued | 2015 | - |
dc.identifier.citation | The 34th Chinese Control Conference (CCC 2015), Hangzhou, China, 28-30 July 2015. In Chinese Control Conference, 2015, p. 2066-2071 | - |
dc.identifier.issn | 1934-1768 | - |
dc.identifier.uri | http://hdl.handle.net/10722/217418 | - |
dc.description | Open Access | - |
dc.description.abstract | The inerter was recently proposed as a two-terminal mechanical element with the property that the force across the element is proportional to the relative acceleration of its two terminals. Improvement has been observed through introducing inerters into various suspension systems. In this paper, the investigation is focused on the shimmy vibration in the aircraft landing gears and the performance variation with the application of inerters. By the method of simulation, the performance changes have been observed and analyzed. | - |
dc.language | eng | - |
dc.publisher | Institute of Electrical and Electronics Engineers. The Journal's web site is located at http://www.ieeexplore.ieee.org/xpl/conhome.jsp?punumber=1001331 | - |
dc.relation.ispartof | Chinese Control Conference | - |
dc.rights | Chinese Control Conference. Copyright © Institute of Electrical and Electronics Engineers. | - |
dc.rights | ©2015 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works. | - |
dc.subject | Aircraft landing gear | - |
dc.subject | Inerter | - |
dc.subject | Shimmy vibration | - |
dc.subject | Suspension | - |
dc.title | Application of inerter to aircraft landing gear suspension | - |
dc.type | Conference_Paper | - |
dc.identifier.email | Chen, MZ: mzqchen@hku.hk | - |
dc.identifier.authority | Chen, MZ=rp01317 | - |
dc.description.nature | link_to_OA_fulltext | - |
dc.identifier.doi | 10.1109/ChiCC.2015.7259953 | - |
dc.identifier.scopus | eid_2-s2.0-84946574059 | - |
dc.identifier.hkuros | 250978 | - |
dc.identifier.spage | 2066 | - |
dc.identifier.epage | 2071 | - |
dc.publisher.place | United States | - |
dc.customcontrol.immutable | sml 151109 | - |
dc.identifier.issnl | 1934-1768 | - |