• Title/Summary/Keyword: and Turn-off angle

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Design and Drive Characteristics of SRM for HEV (HEV용 SRM의 설계 및 구동특성)

  • Kim, Tae-Hyoung;Ahn, Jin-Woo;An, Young-Joo;Moon, Jae-Won
    • Proceedings of the KIEE Conference
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    • 2005.07b
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    • pp.1141-1143
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    • 2005
  • This paper presents the reasonable design parameters of a SRM for hybrid electric vehicle driving. For the design of SRM, the initial model is designed using the equivalent magnetic circuit method. In order to optimize the SRM for HEV. The initial model is redesigned by FEM with the variation of the stock length and turns of winding. This paper shows that a flat-topped current of a phase can be made from a change of the stack length and the number of turns for high efficiency, high average torque and a lower torque ripple. The change of current falling time as a variation of turn-off angle was shown by FEA. The iron loss and copper loss were described. The torque of the redesigned motor is suitable for low and high speed ranges to drive a HEV that was verified by the speed-torque curve.

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A Three-Phase 618 Structure SRM (3상 6/8극 SRM)

  • Lee Ju-Hyun;Lee Dong-Hee;Chen Hao;Ahn Jin-Woo
    • Proceedings of the KIPE Conference
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    • 2004.07a
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    • pp.254-258
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    • 2004
  • A three-phase 6/8 structure SRM (switched reluctance motor), the design and analysis of the motor are described. The range of the stator pole arc factor and the rotor pole arc factor of the motor are analyzed in the linear region. The optimum range of the stator pole arc factor and the turn-off angle of the main switches in the power converter are given with the 2-D finite element electro-magnetic field calculation of the motor and the nonlinear simulation. Test results of the prototype developed are discussed.

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Design of 65kW Class SRM for HEV (65kW급 HEV용 SRM의 설계)

  • Kim, Tae-Hyoung;Ahn, Jin-Woo;An, Young-Joo;Moon, Jae-Won
    • Proceedings of the KIPE Conference
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    • 2005.07a
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    • pp.562-564
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    • 2005
  • This paper presents the reasonable design parameters of a SRM for hybrid electric vehicle driving. For the design of SRM, the initial model is designed using the equivalent magnetic circuit method. In order to optimize the SRM for HEV. The initial model is redesigned by FEM with the variation of the stock length and turns of winding. This paper shows that a flat-topped current of a phase can be made from a change of the stack length and the number of turns for high efficiency, high average torque and a lower torque ripple. The change of current falling time as a variation of turn-off angle was shown by FEA. The iron loss and copper loss were described. The torque of the redesigned motor is suitable for low and high speed ranges to drive a HEV that was verified by the speed-torque curve.

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Design of 65kw Class Switched Reluctance Motor for HEV Drive (하이브리드 자동차 구동용 65kW급 SR Motor의 설계)

  • Moon Jae-Won;Ahn Jin-Woo
    • The Transactions of the Korean Institute of Electrical Engineers B
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    • v.54 no.8
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    • pp.358-363
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    • 2005
  • This paper presents the reasonable design parameters of a switched reluctance motor to drive a hybrid electric vehicle by using the equivalent magnetic circuit method. The designed motor can be redesigned by using finite element analysis as a variation of the parameter for the purpose of improving performance. This paper shows that a flat-topped current of a phase can be made from a change of the lamination stack length for high average torque and a lower torque ripple. The change of current falling time as a variation of turn-off angle was shown by finite element analysis. The core loss and copper loss were described. The torque of the redesigned motor is suitable for low and high speed ranges to drive a HEV. which is verified by the speed-torque curve.

Excitation Voltage Control with a maximum Conduction Ratio of SRM (SRM의 최대 도통비를 갖는 여자전압 제어기법)

  • Lee, S.H.;Park, S.J.;Ahn, J.W.;Kim, C.U.
    • Proceedings of the KIEE Conference
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    • 2001.07b
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    • pp.977-979
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    • 2001
  • The application of SRM(Switched Reluctance Motor) is dramatically increasing due to a simple mechanical structure, high efficiency and a good high speed characteristics. Generally, turn-off angle of power switch must be limited the demagnetization period. To control high conduction ratio in motor operation and regenerative voltage in the generator operation in the SRM, multi-level voltage control is effective. This paper proposes multi-level inverter to have a maximum conduction ratio of SRM. The proposed method is verified by experiment.

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Sensorless driving strategy of Single-Phase Hybrid SRM basing on Back-EMF detection (역기전력을 이용한 단상 하이브리드 SRM의 위치 추정 방법)

  • Tang, Ying;Lee, Donghee;Ahn, Jin-Woo
    • Proceedings of the KIPE Conference
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    • 2016.07a
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    • pp.521-522
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    • 2016
  • This paper presents a novel scheme to estimate the rotor position of a single-phase hybrid switched reluctance motor (HSRM). The proposed method uses the differential of back-EMF within a position region to estimate rotor position. By detecting the crossing-zero signal of back-EMF differential value, the minimum position of back-EMF corresponding to an absolute rotor position can be captured and used for position estimation four times in every mechanical rotation. In this way, a sensorless operation with adjustable turn on/off angle can be achieved without substantial computation. For the starting, two current comparators are adopted. The experimental verification using a prototype drive system is provided to demonstrate the viability of the proposed sensorless scheme.

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Harmonic Intensity Reduction Technique for Single Phase Switched Reluctance Motor Drives Using a New Random PWM Scheme

  • Nguyen, Minh-Khai;Jung, Young-Gook;Yang, Hyong-Yeol;Lim, Young-Cheol
    • Journal of Power Electronics
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    • v.10 no.1
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    • pp.51-57
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    • 2010
  • This paper proposes a new random switching strategy using a DSP TMS320F2812 to reduce the harmonics spectra of single phase switched reluctance motors. The proposed method combines the random turn-on/off angle technique and the random pulse width modulation technique. A harmonic spread factor (HSF) is used to evaluate the random modulation scheme. In order to confirm the effectiveness of the proposed method an experiment was conducted. The experimental results show that the harmonic intensity of the output voltage for the proposed method is better than that for conventional methods.

Kinematic Comparisons between Yang-1 and Yang-2 Vaults in Men's Artistic Gymnastics (남자 체조 YANG-1과 YANG-2 도마 동작의 운동학적 비교)

  • Park, Cheol-Hee;Kim, Young-Kwan
    • Korean Journal of Applied Biomechanics
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    • v.24 no.4
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    • pp.317-327
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    • 2014
  • As a single subject study, it was purposed to investigate kinematic differences between Yang Hak Seon vault (i.e., handspring forward and salto forward straight with triple twist, Yang-1 vault hereafter) and Tsukahara $1260^{\circ}$ twist with salto forward straight (Yang-2 vault hereafter) in gymnastics. Yang Hak-Seon (23 years, 160 cm, and 52 kg) voluntarily participated in this study. Motion capture system, consisting of fourteen cameras, were used to measure Yang-2 vault with the sampling rate of 200 Hz. Twenty six reflective markers were placed on major anatomical points of 15 body segments. Successful two trials of Yang-2 vault were collected and analyzed for the comparison. Compared Yang-1 results were based on the previous study of Park and Song (2012). Results indicated superior linear kinematics of Yang-1 vault to those of Yang-2 vault before the touchdown of vault table. However, Yang-2 vault revealed superior angular kinematics to Yang 1 vault showing more trunk twist angle (a triple and a half twist) and its faster angular velocity during the airborne. The Yang 2 vault could has advantage of increasing angular motion than Yang 1 vault as a result of a half turn off the springboard onto the vault table and a sequential touchdown of the hands.

A New Cryptographic Algorithm for Safe Route Transversal of Data in Smart Cities using Rubik Cube

  • Chhabra, Arpit;Singhal, Niraj;Bansal, Manav;Rizvi, Syed Vilayat
    • International Journal of Computer Science & Network Security
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    • v.22 no.8
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    • pp.113-122
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    • 2022
  • At the point when it is check out ourselves, it might track down various information in each turn or part of our lives. Truth be told, information is the new main thrust of our advanced civilization and in this every day, "information-driven" world, security is the significant angle to consider to guarantee dependability and accessibility of our organization frameworks. This paper includes a new cryptographic algorithm for safe route traversal for data of smart cities which is a contemporary, non-hash, non-straight, 3D encryption execution intended for having information securely scrambled in the interim having a subsequent theoretical layer of safety over it. Encryption generally takes an information string and creates encryption keys, which is the way to unscramble as well. In the interim in another strategy, on the off chance that one can sort out the encryption key, there are opportunities to unravel the information scrambled inside the information string. Be that as it may, in this encryption framework, the work over an encryption key (which is created naturally, henceforth no pre-assurance or uncertainty) just as the calculation produces a "state" in a way where characters are directed into the Rubik block design to disregard the information organization.

Constant speed, variable ascension rate, helical trajectories for airplanes

  • Labonte, Gilles
    • Advances in aircraft and spacecraft science
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    • v.5 no.1
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    • pp.73-105
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    • 2018
  • A particular type of constant speed helical trajectory, with variable ascension rate, is proposed. Such trajectories are candidates of choice as motion primitives in automatic airplane trajectory planning; they can also be used by airplanes taking off or landing in limited space. The equations of motion for airplanes flying on such trajectories are exactly solvable. Their solution is presented, together with an analysis of the restrictions imposed on the geometrical parameters of the helical paths by the dynamical abilities of an airplane. The physical quantities taken into account are the airplane load factor, its lift coefficient, and the thrust its engines can produce. Formulas are provided for determining all the parameters of trajectories that would be flyable by a particular airplane, the final altitude reached, and the duration of the trajectory. It is shown how to construct speed interval tables, which would appreciably reduce the calculations to be done on board the airplane. Trajectories are characterized by their angle of inclination, their radius, and the rate of change of their inclination. Sample calculations are shown for the Cessna 182, a Silver Fox like unmanned aerial vehicle, and the F-16 Fighting Falcon.