• Title/Summary/Keyword: Starter Motor Shaft

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A Study on the Starter Control of the Turbo Generator (터보 제너레이터의 시동기 제어에 관한 연구)

  • 박승엽;노민식
    • Journal of Institute of Control, Robotics and Systems
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    • v.10 no.3
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    • pp.286-293
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    • 2004
  • This paper presents the result of a study on the starter control for a turbo generator. Because a starter in gear box type turbo-generator system is composed of gearbox and brush DC motor, it should be replaced with High Speed Generator(HSG)) in HSG type Turbo-generator. There-ore, it is necessary to design a new starting algorithm and starter. In gearbox type system, brush DC motor is rotated to the designed speed using low voltage-high current battery power. After brush DC motor speed is increased to several times by gearbox, gas turbine engine can be rotated to designed starting speed. If we implement a starter with High Speed Generator(HSG), it is necessary to drive high-speed generator to high-speed motor. High-speed generator with permanent magnet on rotor has a low leakage inductance fur driving high-speed rotation, and it is necessary high DC link voltage for inverter when High-speed generator is driven to high speed. This paper presents result of development of the boost converter for converting high voltage DC from low battery voltage and design of the inverter for controlling a high frequency current to be injected to motor winding. Also, we show performance of the designed starter by driving the turbo generator.

The Study on Operability Improvement of the start motor for Auxiliary Power Unit of Rotorcraft (회전익 항공기 보조동력장치 시동모터 운용성 개선연구)

  • Lee, Gwang-Eun;Kang, Byoung-Soo;Na, Seong-Hyeon
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.22 no.2
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    • pp.774-780
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    • 2021
  • The auxiliary power unit (APU) of a rotorcraft starts the engine during operation/flying. The APU is composed of a gas turbine engine type. The starting principle of the component is that the electric start motor generates the power required for starting by rotating the shaft. In this study, quality improvement was performed by applying an over-running clutch (ORC) between the APU and the starter motor to secure the operability of the starter motor of the APU mounted on the rotorcraft. The starter motor has the main role of starting the APU, but during operation, it is rotated without load by the rotational force of the APU gear shaft, resulting in friction at the brush. This phenomenon causes abrasion of the brush of the starter motor. Consequently, when the APU operation time increases, the brush life decreases, and the operability of the APU is affected. In this study, an ORC that separates the interlocking between the start motor brush abrasion and the APU operation time was applied to improve the operability/durability of the APU starter motor. The effect was verified through a test, and the technical feasibility of the design change was analyzed.

Development of the Starting Algorithm and Starter for Turbo Generator (터보 제너레이터의 시동 알고리즘 및 시동기 개발)

  • 노민식;박승엽
    • The Transactions of the Korean Institute of Power Electronics
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    • v.9 no.1
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    • pp.17-24
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    • 2004
  • The starter of the turbo generator is composed of a high speed generator(HSG), an inverter and a boost converter instead of a gearbox, a DC motor and a low-voltage battery in the starter of the turbo shaft generation system. Because turbo generator is needed a high speed motoring at start-up, high speed generator has a low leakage inductance and inverter need a high DC link voltage. In this study, for developing the stater of a turbo generator, a boost converter with a high capacity was developed to convert high voltage from a low battery voltage. And for controlling a high frequency current to be injected to a motor winding with a low leakage inductance, the inverter with a high precision and a high speed operation was designed and for a stable ignition, the starting algorithm of a turbo generator was proposed. Turbo generator was started by the starter developed to verify the performances.

Development of crank shaft mounted ISG(Integrated Starter Generator) (크랭크축 직결형 42V기동/발전기(ISG)의 개발)

  • Bae Bon-ho;Yun Seok-Young;Sul Seung-ki
    • Proceedings of the KIPE Conference
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    • 2002.07a
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    • pp.653-656
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    • 2002
  • This paper presents the development of 15G(Integrate Starter Generator). The ISG is the crank shaft mount type and it is installed at tile flywheel. The wide operating range of ISG requires large constant power speed ratio, good overload performance and high efficiency. High saliency ratio permanent magnet motor is developed for the ISG applications and 500A MOSFET inverter is designed to derive the ISG. The characteristic of developed ISG is investigated using the special test-bed for the 42V PowerNet and the detailed results is presented

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자동차 스타트 모터용 샤프트의 헬리컬 스플라인 전조공정에 관한 유한요소해석

  • 고대철;이정민;김호관;김병민
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2004.05a
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    • pp.250-250
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    • 2004
  • 자동차의 시동을 걸기 위해서는 맨 처음 엔진을 강제로 가동시키는 기계장치가 있어야 하며, 이를 시동모터라 한다. 시동모터는 모터부와 그 부속장치 그리고 발생된 힘을 엔진으로 전달하는 동력전달 기구로 구성되어 있다. 동력전달기구는 플라이 휠이라는 부품을 크랭크 축 끝단에 장착한 후 그 원주상에 링 기어를 만들고, 시동모터의 축에 피니언이라는 작은 기어를 맞물리게 하여 시동 키를 돌리면 이 기어가 회전되는 원리를 이용하고 있다. 피니언 기어는 작고 반대로 플라이 휠에 장착되어 있는 링 기어는 크기 때문에 일정한 기어비가 형성되어 큰 부하의 엔진회전이 가능하다.(중략)

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