High force linear actuator for an aeronautical application. Association with a fault tolerant converter.

Ziegler, Nicolas; Matt, D.; Jac, Julien; Martiré, Thierry; Enrici, P.

doi:10.1109/acemp.2007.4510487

Cited by 9 publications

(2 citation statements)

References 1 publication

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“…The results achieved by the TLPM motor presented in this paper, compare excellently with results published in available literature [9,11,15,16] concerning high force density, linear machines. The excellent values of force density are partly dependent on the implementation of the thermal management technique, which was successfully implemented to the TLPM motor in this work.…”

Section: Discussionsupporting

confidence: 85%

“…From the various, linear machine topologies that exist today [5,[7][8][9][10], in general it is the TLPM motor topology with inset permanent magnets (IPM), that offers the best force density performances [11,12]. Considering this, then it was decided to focus the design on such an arrangement, which also has the advantage of facilitating manufacturing (in terms of the moving part, henceforth called the mover) and also reduced the amount of mover, magnetic material required.…”

Section: The Tlpm Motormentioning

confidence: 99%

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Design of a High-Force-Density Tubular Motor

Galea

Buticchi

Empringham

et al. 2014

IEEE Trans. on Ind. Applicat.

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-This paper deals with the design, construction and experimental verification of a high force density, tubular, linear, permanent magnet motor, driven from a high power density matrix converter for an aerospace application. The work also describes the implementation and experimental verification of a novel, thermal management technique for the phase windings of electrical machines. The technique introduces a higher thermal conductivity path between the centre of the slot and the cooling arrangement, thus increasing the heat flow away from the slot centre. An introduction to the design of the motor is first given, after which an introduction to the technique is presented. A study of how the implementation of the technique affects motor performance is then presented. A detailed overview of the construction aspects is highlighted and finally, experimental validation is used to illustrate the comparison between the predicted results and the measured results, obtained from an instrumented, test rig.

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Section: Discussionsupporting

confidence: 85%

Section: The Tlpm Motormentioning

confidence: 99%

Design of a High-Force-Density Tubular Motor

Galea

Buticchi

Empringham

et al. 2014

IEEE Trans. on Ind. Applicat.

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Camber Actuation of an Articulated Wing with Electromechanical Actuators

Giraud

Cronel

Ramos

et al. 2021

Notes on Numerical Fluid Mechanics and Multidisciplinary Design

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Camber Setting of a Morphing Wing with Macro-acuator Feedback Control

Giraud

Raibaudo

Cronel

et al. 2021

Fluid-Structure-Sound Interactions and Control

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This paper relates the camber control of a morphing ap actuated by a macro-actuator composed by ve electromechanical actuators. Controlling the camber of the ap could provide fuel consumption by reaching specic aerodynamic proles. Due to their reliability, electromechanical actuators are used for the macro-actuator. They are located and integrated to resist to realistic aerodynamic forces. Their control is determinant to ensure the ap mission. Based on a simplied model using Lagrange principle leading to macro-actuator feedback control, the strategy deals with the interconnection of the ve electromechanical actuators. Flow simulations are computed around the ap to have more pressure distribution data. Finally, feedback control simulations are provided.

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High force linear actuator for an aeronautical application. Association with a fault tolerant converter.

Cited by 9 publications

References 1 publication

Design of a High-Force-Density Tubular Motor

Design of a High-Force-Density Tubular Motor

Camber Actuation of an Articulated Wing with Electromechanical Actuators

Camber Setting of a Morphing Wing with Macro-acuator Feedback Control

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