• The Transactions of the Korean Institute of Electrical Engineers B
• /
• v.52 no.7
• /
• pp.320-326
• /
• 2003

Slotless Permanent Magnet Linear Synchronous Motor (PMLSM) has good control ability but thrust density is low. So, this paper proposes inserted core type of slotless PMLSM to improve its thrust density. Inserting the core between windings of each phase, detent force is generated by the difference of magnetic resistance in an air gap. To minimize detent force, this paper applies the neural network to inserted core type of slotless PMLSM. The, Magnetic pole ratio, the width of the inserted core and the width of the coil are selected as a design parameter to minimize detent force. In comparison with inserted core type one, thrust ripple greatly decreases by minimizing detent force and also thrust increases in this optimal model.

• Proceedings of the KIEE Conference
• /
• 1997.07a
• /
• pp.6-8
• /
• 1997

This paper describes on the dynamic characteristic analysis of a inverter-fed linear synchronous motor with surface type permanent magnet using time-stepped finite element method. We can certify that the proposed simulation method can be used at the dynamic characteristic analysis of other inverter-fed linear motor.

• Proceedings of the KIEE Conference
• /
• 1997.07a
• /
• pp.192-194
• /
• 1997

This paper propose an efficient space harmonic analysis method for magnetic field. Permanent magnet and primary core considered slot are replaced by EMC(equivalent magnetizing current). And the resultant air gap flux density is calculated by superposition due to the permanent magnet and EMC. We analyze the harmonic distribution of air gap flux density taking into account slot for PMLSM.

• Proceedings of the KIEE Conference
• /
• 1997.07a
• /
• pp.165-167
• /
• 1997

This paper centers on a method which can reduce calculating time and maintain accuracy of whole model FE analysis with one pole model for short secondary Permanent Magnet Linear Synchronous Motor(PMLSM). We use one pole model which considers the number of pole of stator and mover respectively in order to replace whole model to one pole model and calculate flux linkage and back e.m.f. with accuracy. Also we verify the validity of proposed method with comparision of results of whole and one pole model.

• Proceedings of the KIEE Conference
• /
• 1998.07a
• /
• pp.322-324
• /
• 1998

This paper describes the characteristics analysis of surface permanent magnet linear synchronous motor with conductive sheet secondary using time-stepped finite element method. The detent force, normal force, back-emf and dynamic characteristics as speed, thrust and current are described.

• Proceedings of the KIEE Conference
• /
• 1999.07a
• /
• pp.139-141
• /
• 1999

This paper presents the design schemes for the improvement of force characteristics in Controlled permanent magnet linear synchronous motor (CPMLSM). The dependence of motor performance on various design schemes, such as the slot shapes, magnetizing patterns of PM and skewing, have been investigated in detail by using FEM and experiment. From this study, it is known that in the various design schemes, skewing is most efficient in the aspects of force characteristic, efficiency and force density.

• Proceedings of the KIEE Conference
• /
• 2000.07b
• /
• pp.757-759
• /
• 2000

The problem in improving the positioning precision of a permanent magnet linear synchronous motor(PMLSM) is the large detent force caused by the permanent magnet. The detent force is thought to arise from the difference of the position of a permanent magnet end and a tooth position. In this paper, Three methods of reducing detent force is presented The first method is adjusting the width of permanent magnet. The second method is varying the shape of armature teeth. The third method is the arrangement of the permanent magnet end. This paper compares with the ratio of reducing the detent force according to the three methods.

• Proceedings of the KIEE Conference
• /
• 1998.07a
• /
• pp.316-318
• /
• 1998

This paper describes the direct thrust control of permanent magnet linear synchronous motor (PMLSM) with the secondary aluminium sheet. The time stepped finite element method and moving mesh technique are used for simulating dynamic characteristics of the PMLSM. The secondary back-iron conductivity as well as the initial flux linkage due to permanent magnet are considered in the simulation.

• The Transactions of the Korean Institute of Electrical Engineers B
• /
• v.49 no.8
• /
• pp.514-521
• /
• 2000

This paper presents a direct thrust control scheme for permanent magnet linear synchronous motor(PMLSM) by using digital signal processor(DSP). And a simulation method for the direct thrust control of a permanent magnet linear synchronous motor using the equivalent circuit is presented. The detent force that was obtained by cubic spline method is considered in the simulation. Thrust correction coefficient is utilized to estimate actual thrust on the direct thrust control, which considers the longitudinal end effect due to the finite core length of the permanent magnet linear synchronous motor. The motor self inductance, the initial flux linkage by the permanent magnet is calculated in advance by the finite element analysis, and then the direct control simulation is carried out. As the results, thrust, current and speed are shwon.

• The Transactions of the Korean Institute of Electrical Engineers B
• /
• v.50 no.2
• /
• pp.53-58
• /
• 2001

This paper describes a moving mesh technique for dynamic characteristics analysis of permanent magnet linear synchronous motor with the secondary aluminium sheet. The moving mesh technique applied to the linear induction motor can be used to analyze the linear synchronous motor with the rectangular permanent magnet. But in case of the permanent magnet with taper, the shape of the permanent magnet is presented. The time-stepped finite element method is used for the dynamic characteristics simulation of the permanent magnet linear synchronous motor, The results of application example(hysteresis current controlled inverter fed control) such as thrust, current and flux plots are shown.