Conference
Incremental Modeling and Simulation of Mechanical Power Transmission for More Electric Aircraft Flight Control Electromechanical Actuation System Application
| العنوان: | Incremental Modeling and Simulation of Mechanical Power Transmission for More Electric Aircraft Flight Control Electromechanical Actuation System Application |
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| المؤلفون: | Fu, Jian, Maré, Jean-Charles, Fu, Yongling |
| المساهمون: | School of Mechanical Engineering and Automation, Beihang University (BUAA), Institut Clément Ader (ICA), Institut Supérieur de l'Aéronautique et de l'Espace (ISAE-SUPAERO)-Institut National des Sciences Appliquées - Toulouse (INSA Toulouse), Institut National des Sciences Appliquées (INSA)-Université de Toulouse (UT)-Institut National des Sciences Appliquées (INSA)-Université de Toulouse (UT)-Université Toulouse III - Paul Sabatier (UT3), Université de Toulouse (UT)-Centre National de la Recherche Scientifique (CNRS)-IMT École nationale supérieure des Mines d'Albi-Carmaux (IMT Mines Albi), Institut Mines-Télécom Paris (IMT)-Institut Mines-Télécom Paris (IMT) |
| المصدر: | ASME 2016 International Mechanical Engineering Congress and Exposition Volume 1: ; ASME 2016 International Mechanical Engineering Congress and Exposition ; https://insa-toulouse.hal.science/hal-02046029 ; ASME 2016 International Mechanical Engineering Congress and Exposition, Nov 2016, Phoenix, United States. ⟨10.1115/IMECE2016-66436⟩ |
| بيانات النشر: | HAL CCSD |
| سنة النشر: | 2016 |
| المجموعة: | Université Toulouse III - Paul Sabatier: HAL-UPS |
| مصطلحات موضوعية: | Electromechanical actuator, More electric aircraft, Modelling, Power-by-wire, Power loss, Simulation, Bond Graph, Electro-hydrostatic actuator, [SPI.MECA.STRU]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Structural mechanics [physics.class-ph] |
| جغرافية الموضوع: | Phoenix, United States |
| الوصف: | Volume 1: Advances in Aerospace TechnologyPhoenix, Arizona, USA, November 11–17, 2016Conference Sponsors: ASMEISBN: 978-0-7918-5051-0 ; International audience ; In the field of more electric aircraft, electromechanical actuators (EMAs) are becoming more and more attractive because of their outstanding benefits of aircraft fuel reduction, maintenance costs saving, and system flexibility improvement. For aerospace electromechanical actuator applications, mechanical power transmission is critical for safety, in which reflected inertia to load, heat generated by energy losses and faults due to jamming, free-play and free-run are specific issues. According to the system-engineering process and simulation-aided design, this communication proposes an incremental approach for the virtual prototyping of EMA mechanical power transmission. Resorting to the Bond-graph formalism, the parasitic effects are progressively introduced and realism of models is increased step-by-step. Finally, the numerical implementations are presented and compared with basic, advanced and full models of mechanical power transmission in AMESim environment. Multi-level submodels are available and can be re-used for preliminary sizing, thermal balance verification and response to fault analysis. |
| نوع الوثيقة: | conference object |
| اللغة: | English |
| DOI: | 10.1115/IMECE2016-66436 |
| الاتاحة: | https://insa-toulouse.hal.science/hal-02046029 https://insa-toulouse.hal.science/hal-02046029v1/document https://insa-toulouse.hal.science/hal-02046029v1/file/fu2016.pdf https://doi.org/10.1115/IMECE2016-66436 |
| Rights: | info:eu-repo/semantics/OpenAccess |
| رقم الانضمام: | edsbas.5B395699 |
| قاعدة البيانات: | BASE |
| DOI: | 10.1115/IMECE2016-66436 |
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