• 제목/요약/키워드: High thrust

검색결과 581건 처리시간 0.181초

Development of High Thrust Linear Motor for Machine Tool (공작기계용 고추력 리니어모터 개발)

  • 정재한;박재한;정시욱
    • Proceedings of the Korean Society of Machine Tool Engineers Conference
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    • 한국공작기계학회 2004년도 추계학술대회 논문집
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    • pp.363-368
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    • 2004
  • Due to various advantages over the conventional linear motion device such as ball-screw, linear motors have been used in wide variety of industrial applications for years. Driven by increased demand for precision machine tools, the importance of high positioning accuracy, high stiffness and high thrust are greatly increasing. The merits of linear motor are high speed, high acceleration and good positioning accurcy. In addition, Linear motor for high quality machine tool call for high thrust, high stiffness. In this paper, thrust ripple, detent force and thermal behavior are considered for the development of high performance linear motor whose thrust is up to 10,000N. This paper presents a comprehensive study for an iron core type linear motor characteristics that include the influence of PM position on thrust, thrust ripple by detent force and motor dynamics as well.

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Development of High Thrust Linear Motor for Machine Tool (공작기계용 고추력 리니어모터 개발)

  • 정재한;박재완;박재한;정시욱
    • Proceedings of the Korean Society of Machine Tool Engineers Conference
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    • 한국공작기계학회 2002년도 추계학술대회 논문집
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    • pp.423-428
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    • 2002
  • Due to various advantages over the conventional linear motion device such as ball-screw, linear motors have been used in wide variety of industrial applications for years. Driven by increased demand for precision machine tools, the importance of high positioning accuracy, high stiffness and high thrust are greatly increasing. The merits of linear motor are high speed, high acceleration and good positioning accurcy. In addition, Linear motor for high quality machine tool call for high thrust, high stiffness. In this paper, thrust ripple, detent force and thermal behavior are considered for the development of high performance linear motor whose thrust is up to 4,000N. This paper presents a comprehensive study for an iron core type linear motor characteristics that include the influence of PM position on thrust, thrust ripple by detent force and motor dynamics as well.

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Development of High Thrust Linear Motor for Machine Tool II (공작기계용 고출격 리니어모터 개발 II)

  • 정재한;박재한;정시욱
    • Proceedings of the Korean Society of Machine Tool Engineers Conference
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    • 한국공작기계학회 2004년도 춘계학술대회 논문집
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    • pp.347-353
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    • 2004
  • Due to various advantages over the conventional linear motion device such as ball-screw, linear motors have been used in wide variety of industrial applications for years. Driven by increased demand for precision machine tools, the importance of high positioning accuracy, high stiffness and high thrust are greatly increasing. The merits of linear motor are high speed high acceleration and good positioning accuracy. In addiction, Linear motor for high qualify machine tool call for high thrust, high stiffness. In this paper, thrust ripple, detent force and thermal behavior are considered for the development of high performance linear motor whose thrust is up to 1,900N. This paper presents a comprehensive study for an iron core type linear motor characteristics that include the influence of PM position on thrust ripple by detent force and motor dynamics as well.

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Development of Iron Core type Linear Motor for Machine Tool (공작기계용 철심형 니니어모터 기술개발)

  • 정재한;박재완
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 한국정밀공학회 1997년도 추계학술대회 논문집
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    • pp.33-36
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    • 1997
  • The merits of linear motor are high speed, high acceleration and goad positioning accuracy. In addition, Linear motor for high quality machme tool call for high thrust, high stiffness. In using linear motor we also consider thrust ripple, detent force and thermal behavior. In this research, Iron core type single sided linear DC motor(LDM) is designed which thrust is 6,000 N. To accomplish this design, Various research is hlfilled l~ke the relation of thrust and permanent magnet position angle, the variation of detent force and thrust ripple, dynamic characteristics, and so on.

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Development of Iron Core type Linear Motor for Machine Tool(2) (공작기계용 철심형 리니어모터 기술개발(2))

  • 정재한;박재완;박재한
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 한국정밀공학회 2002년도 춘계학술대회 논문집
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    • pp.82-85
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    • 2002
  • Due to various advantages over the conventional linear motion device such as ball-screw, linear motors have been used in wide variety of industrial applications for years. Driven by increased demand for precision machine tools, the importance of high positioning accuracy, high stiffness and high thrust are greatly increasing. In this paper, thrust ripple, detent force and thermal behavior are considered for the development of high performance linear motor whose thrust is up to 4, 000N. This paper presents a comprehensive study for an iron core type linear motor characteristics that include the influence of PM position on thrust thrust ripple by detent farce and motor dynamics as well.

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Axial Thrust Control of High-speed Centrifugal Pump with Cavity Vanes (캐비티 베인이 있는 고속 원심펌프의 축추력 제어)

  • Kim, Dae-Jin;Choi, Chang-Ho;Noh, Jun-Gu;Kim, Jinhan
    • The KSFM Journal of Fluid Machinery
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    • 제15권6호
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    • pp.46-50
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    • 2012
  • A high-speed centrifugal pump requires more attention to the control of its axial thrust due to the high discharge pressure than a conventional industrial pump. Vanes employed toward the rear cavity of the impeller can be an effective device to control the axial thrust of the pump. The vanes disturb circumferential flow of the cavity and it can modify the axial force acting on the impeller. In this paper, three types of vanes are installed in the high-speed centrifugal pump for liquid rocket engines and the thrust of the pump is measured with an additional thrust measurement unit. According to the results, shapes of cavity vanes have effects on the axial thrust of the pump. As the height of vanes increases, the outlet pressure of the rear floating ring seal decreases which results in a decrease of the thrust. On the other hand, head of the pump is almost same regardless of cavity vanes. Also, the pressure drop of the bypass pipeline increases when vanes are removed.

Development of Iron Core Type Linear Motor for Machine Tool (공작기계용 철심형 리피어모터 기술 개발)

  • Joung, Jae-Han;Park, Jae-Wan;Lee, Sang-Ryong
    • Journal of the Korean Society for Precision Engineering
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    • 제19권9호
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    • pp.82-89
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    • 2002
  • There is an intensifying demand fur linear motors in vast range of industry applications such as in factory automation and semi-conductor manufacturing equipment due to their high positioning accuracy, high static stiffness, high thrust and excellent dynamic characteristics. This paper presents an iron core type linear motor for machine tool whose rated thrust is up to 6000N. For electromagnetic field and dynamic analysis, finite element method (FEM) is implemented to predict motor performance. Various design parameters are considered to reduce thrust ripple and to improve dynamic performance with the least sacrifice of effective thrust. Experimental results on thrust and static stiffness are also followed to confirmed the validity of the analysis.

Thrust Bearing Design for High-Speed Composite Air Spindles (고속 복합재료 공기 주축부를 위한 추력베어링 설계)

  • Bang, Kyung-Geun;Lee, Dai-Gil
    • Transactions of the Korean Society of Mechanical Engineers A
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    • 제26권10호
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    • pp.1997-2007
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    • 2002
  • Composite air spindles are appropriate for the high-speed and the high-precision machining as small hole drilling of printed circuit board (PCB) or wafer cutting for manufacturing semiconductors because of the low rotational inertia, the high damping ratio and the high fundamental natural frequency of composite shaft. The axial load and stiffness of composite air spindles fur drilling operation are determined by the thrust ben ring composed of the air supply part mounted on the housing and the rotating part mounted on the rotating shaft. At high-speed rotation, the rotating part of the thrust bearing should be designed considering the stresses induced by centrifugal force as well as the axial stiffness and the natural frequency of the rotating shaft to void the shaft from failure due to the centrifugal force and resonant vibration. In this work, the air supply part of the thrust bearing was designed considering the bending stiffness of the bearing and the applied load. The rotating part of the thrust bearing was designed through finite element analysis considering the cutting forces during manufacturing as well as the static and dynamic characteristics under both the axial and con trifugal forces during high-speed rotation.

Operating Performance Limitations of Tilting Pad Thrust Bearings Due to Misalignment (정렬불량에 따른 틸팅 패드 스러스트 베어링의 운전 성능 한계 검토)

  • Song, AeHee;Choi, SeongPil;Kim, SeonJin
    • Tribology and Lubricants
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    • 제36권2호
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    • pp.82-87
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    • 2020
  • In thrust bearings, the thrust collar and bearing surface need to be parallel to each other to ensure that all pads share the same load. In rotating machines, the shaft system cannot achieve perfect alignment. Misalignment of the thrust collar results in some pads supporting a higher load than others and excessive loads being placed on some pads. Consequently, high loads and high temperatures may occur in the bearing. Thus, in this study, we aim to analytically evaluate the performance of a misaligned non-equalizing direct lubricated tilting pad thrust bearing. We define the oil film thickness of the misaligned thrust bearing using the Byrant angle. Additionally, we calculate the pressure distribution and temperature distribution of the thrust bearing using the generalized Reynolds equation and energy equation. The design limit of the thrust bearing is defined by the load and temperature. Therefore, we evaluate the allowable misalignment angle as the limit of the maximum load and temperature. The analysis results demonstrate that an increase in the speed and load corresponds to a smaller allowable misalignment angle. However, as this is not the same for all thrust bearings, evaluating the allowable misalignment angle at each thrust bearing is essential.

KSLV-II $1^{st}$ Stage Clustered Engine Arrangement Concept (한국형발사체 1단 클러스터드 엔진 배치 개념)

  • Lee, Han-Ju;Oh, Seung-Hyub
    • Aerospace Engineering and Technology
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    • 제11권1호
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    • pp.78-83
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    • 2012
  • Generally, the first stage of a launch vehicle requires high thrust to achieve a mission. We can use one high thrust level engine or a clustered engine system which made of several small thrust level engines to make high thrust. The first stage propulsion system of KSLV-II has 300tf thrust to satisfy the mission. But it is impractical to make high thrust by one engine at this moment in time. So we should cluster four 75tf class engines which can be applied to make a required thrust for the first stage propulsion system. This article deals with the concept of the first stage clustered engine arrangement of KSLV-II.