Electrification of a landing gear – actuators with toothed coupling
| Autor: | Julien Jac, Nicolas Ziegler, Philippe Enrici, Daniel Matt, Florian Dumas |
|---|---|
| Přispěvatelé: | Institut d’Electronique et des Systèmes (IES), Université de Montpellier (UM)-Centre National de la Recherche Scientifique (CNRS), Groupe énergie et matériaux (GEM), Université de Montpellier (UM)-Centre National de la Recherche Scientifique (CNRS)-Université de Montpellier (UM)-Centre National de la Recherche Scientifique (CNRS), ERNEO, Laboratoire de Génie Electrique de Grenoble (G2ELab), Institut polytechnique de Grenoble - Grenoble Institute of Technology (Grenoble INP )-Centre National de la Recherche Scientifique (CNRS)-Université Grenoble Alpes [2016-2019] (UGA [2016-2019]) |
| Rok vydání: | 2018 |
| Předmět: |
Coupling
business.product_category Stator Computer science 020208 electrical & electronic engineering Mechanical engineering 02 engineering and technology Linear motor 7. Clean energy [SPI.TRON]Engineering Sciences [physics]/Electronics Airplane law.invention Hydraulic cylinder law 0202 electrical engineering electronic engineering information engineering Electrical and Electronic Engineering business Actuator Dimensioning ComputingMilieux_MISCELLANEOUS Landing gear |
| Zdroj: | IET Electric Power Applications IET Electric Power Applications, Institution of Engineering and Technology, 2018, 12 (6), pp.739-746. ⟨10.1109/TMAG.2018.2877995⟩ |
| ISSN: | 1751-8679 1751-8660 |
| Popis: | This study presents the design of an electric motorisation for a landing gear. The concept of More Electric Aircraft is currently with one of the major concerns of all aircraft manufacturers and equipment suppliers throughout the world. The objective consists of eliminating, to the greatest extent possible, the use of any actuator containing fluid pressure and increasing the use of electric actuators. This applies to all airplane orders and accessories. The choice of this motorisation was to design synchronous machines with toothed coupling. When actuators of very high mass performance are required, the use of this type of actuator is an interesting solution, compared with conventional actuators with polar coupling. The principles used in our design method are based on two-dimensional finite-element simulations. The study and the calculation can be performed in two dimensions from a simple element called an elementary pattern, representing the interaction of magnets with stator teeth. Following a summary presentation of this type of actuator and its dimensioning, two prototypes are presented. To replace the hydraulic cylinders in the landing gear of an A320 aircraft, a vernier machine, and a multi-air gap linear motor has been dimensioned, manufactured and tested. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
|
Plný text