JP2006153117A - Magnetic bearing - Google Patents

Magnetic bearing Download PDF

Info

Publication number
JP2006153117A
JP2006153117A JP2004343596A JP2004343596A JP2006153117A JP 2006153117 A JP2006153117 A JP 2006153117A JP 2004343596 A JP2004343596 A JP 2004343596A JP 2004343596 A JP2004343596 A JP 2004343596A JP 2006153117 A JP2006153117 A JP 2006153117A
Authority
JP
Japan
Prior art keywords
magnetic flux
axial
rotor
poles
magnetic
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2004343596A
Other languages
Japanese (ja)
Other versions
JP4138735B2 (en
Inventor
Yoji Okada
養二 岡田
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Iwaki Co Ltd
Original Assignee
Iwaki Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Iwaki Co Ltd filed Critical Iwaki Co Ltd
Priority to JP2004343596A priority Critical patent/JP4138735B2/en
Publication of JP2006153117A publication Critical patent/JP2006153117A/en
Application granted granted Critical
Publication of JP4138735B2 publication Critical patent/JP4138735B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/04Bearings not otherwise provided for using magnetic or electric supporting means
    • F16C32/0406Magnetic bearings
    • F16C32/044Active magnetic bearings
    • F16C32/0459Details of the magnetic circuit
    • F16C32/0461Details of the magnetic circuit of stationary parts of the magnetic circuit
    • F16C32/0465Details of the magnetic circuit of stationary parts of the magnetic circuit with permanent magnets provided in the magnetic circuit of the electromagnets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/04Bearings not otherwise provided for using magnetic or electric supporting means
    • F16C32/0406Magnetic bearings
    • F16C32/044Active magnetic bearings
    • F16C32/0444Details of devices to control the actuation of the electromagnets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/04Bearings not otherwise provided for using magnetic or electric supporting means
    • F16C32/0406Magnetic bearings
    • F16C32/044Active magnetic bearings
    • F16C32/0474Active magnetic bearings for rotary movement
    • F16C32/0476Active magnetic bearings for rotary movement with active support of one degree of freedom, e.g. axial magnetic bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/04Bearings not otherwise provided for using magnetic or electric supporting means
    • F16C32/0406Magnetic bearings
    • F16C32/044Active magnetic bearings
    • F16C32/0474Active magnetic bearings for rotary movement
    • F16C32/0489Active magnetic bearings for rotary movement with active support of five degrees of freedom, e.g. two radial magnetic bearings combined with an axial bearing

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To provide a magnetic bearing having excellent controllability and capable of being miniaturized and reducing its weight. <P>SOLUTION: A stator 1 has a plurality of main poles 3 and a plurality of auxiliary poles 4 adjacent to one of the main poles 3 in the peripheral direction and forming a permanent magnet 16 for supplying bias magnetic flux to a tip part. An axial exciting coil 15 for controlling a position in the axial direction of a rotor 2 by increasing intensity of bias magnetic flux at a position in the axial direction and reducing its intensity at another position is formed in each main pole 3. Exciting current flowing in the axial exciting coil 15 is controlled based on outputs detected by a plurality of magnetic flux sensors 17 formed at tips of the plurality of auxiliary poles 4. <P>COPYRIGHT: (C)2006,JPO&NCIPI

Description

本発明は、磁気力によってロータを非接触状態で支持する磁気軸受に関し、特にロータを軸方向(アキシャル方向)に制御することを可能にした磁気軸受に関する。   The present invention relates to a magnetic bearing that supports a rotor in a non-contact state by a magnetic force, and more particularly to a magnetic bearing that can control the rotor in an axial direction (axial direction).

磁気軸受は、回転体を非接触で支持することができるため、制御技術の発展に伴って各種の軸受に利用されてきている。最近では、超小型回転体用の磁気軸受が要望されてきている。しかし、電磁石を利用した磁気軸受は、ロータを浮上させるために大きな電流を必要とするため、消費電力が大きくなってしまう。また、少ない電流で磁気力を大きくするためには、ロータとステータとの間のギャップが小さいことが要求され、高い工作精度が必要となる。   Since the magnetic bearing can support the rotating body in a non-contact manner, it has been used for various bearings with the development of control technology. Recently, there has been a demand for magnetic bearings for micro rotating bodies. However, since the magnetic bearing using an electromagnet requires a large current to float the rotor, the power consumption increases. Further, in order to increase the magnetic force with a small current, it is required that the gap between the rotor and the stator is small, and high machining accuracy is required.

これらの問題を解決する有力な手法として、近年、性能向上が顕著な永久磁石のバイアス磁束を利用したハイブリッド型の磁気軸受が使用されるようになってきた。このハイブリッド型の磁気軸受は、例えば特許文献1〜3により提案されている。
特開2003−21140号公報(段落0053〜0056、図6) 特開2001−41138号公報(段落0011〜0014、図1) 特開平2001−101234号公報(段落0009、図1)
As a promising method for solving these problems, in recent years, a hybrid type magnetic bearing using a bias magnetic flux of a permanent magnet whose performance has been remarkably improved has been used. This hybrid type magnetic bearing is proposed by patent documents 1-3, for example.
JP 2003-21140 (paragraphs 0053 to 0056, FIG. 6) Japanese Patent Laid-Open No. 2001-41138 (paragraphs 0011 to 0014, FIG. 1) Japanese Patent Laid-Open No. 2001-101234 (paragraph 0009, FIG. 1)

しかし、上述した特許文献に開示された磁気軸受では、軸方向(アキシャル)方向の安定性については受動安定に頼らざるを得ず、そのためにロータに軸方向の負荷がかかると、傾いて回転したり、振動が発生したりして制御が困難になるという問題がある。
本発明は、このような問題点に鑑みてなされたもので、軸方向の制御性に優れ、小型化及び軽量化が可能な磁気軸受を提供することを目的とする。
However, in the magnetic bearing disclosed in the above-mentioned patent document, it is necessary to rely on passive stability for the stability in the axial direction (axial direction). For this reason, when an axial load is applied to the rotor, the magnetic bearing is inclined and rotated. There is a problem that control becomes difficult due to vibration or vibration.
The present invention has been made in view of such problems, and an object of the present invention is to provide a magnetic bearing that is excellent in axial controllability and can be reduced in size and weight.

本発明に係る磁気軸受は、ステータと、このステータに磁気力によって非接触状態で支持されて回転軸を中心に回転するロータとを有する磁気軸受において、前記ステータは、前記ロータに所定のギャップを介して対向し軸方向成分を含む磁束が集中する磁束集中部を有し且つ前記ステータの周方向に所定の間隔で配置される複数の主極、及び先端部において前記ロータに所定のギャップを介して対向し且つ前記複数の主極に対して前記周方向にずれた位置に配置される複数の補極とを含み、前記補極の先端部を第1極性とし隣接する前記主極の磁束集中部を第2極性とするようなバイアス磁束を供給する永久磁石と、前記複数の主極に設けられ前記バイアス磁束の強度を前記軸方向の一方の側においては強め他方の側では弱めることにより前記ロータの軸方向の位置を制御するアキシャル制御磁束を発生させるアキシャル励磁コイルと、前記複数の補極の先端に設けられる複数の磁束センサと、前記複数の磁束センサの検出信号に基づいて前記アキシャル励磁コイルに流れる励磁電流を制御する制御部とを備えたことを特徴とする。   The magnetic bearing according to the present invention is a magnetic bearing having a stator and a rotor that is supported by the stator in a non-contact state by a magnetic force and rotates about a rotation axis. The stator has a predetermined gap in the rotor. A plurality of main poles that are opposed to each other and have a magnetic flux concentrating portion in which a magnetic flux including an axial component is concentrated, and are arranged at predetermined intervals in the circumferential direction of the stator, and a tip of the rotor via a predetermined gap And a plurality of complementary poles arranged at positions shifted in the circumferential direction with respect to the plurality of main poles, and a magnetic flux concentration of the main poles adjacent to each other with a tip portion of the complementary pole as a first polarity A permanent magnet for supplying a bias magnetic flux with the second polarity as a portion, and a strength of the bias magnetic flux provided on the plurality of main poles on one side in the axial direction and on the other side An axial excitation coil for generating an axial control magnetic flux for controlling the axial position of the rotor, a plurality of magnetic flux sensors provided at the tips of the plurality of auxiliary poles, and the axial based on detection signals of the plurality of magnetic flux sensors And a control unit for controlling the excitation current flowing in the excitation coil.

本発明によれば、軸方向の制御性に優れ、小型化及び軽量化が可能な磁気軸受を提供することが可能になる。   ADVANTAGE OF THE INVENTION According to this invention, it becomes possible to provide the magnetic bearing which is excellent in controllability of an axial direction, and can be reduced in size and weight.

まず、図1を参照して、本発明の第1の実施の形態に係る磁気軸受を説明する。図1(a)は、この磁気軸受の軸方向からみた平面図であり、同図(b)は同図(a)におけるA−A’断面図である。磁気軸受は、外側に配置された環状のステータ1と、このステータ1の内側に配置されたロータ2とを有する。   First, a magnetic bearing according to a first embodiment of the present invention will be described with reference to FIG. FIG. 1A is a plan view of the magnetic bearing as viewed from the axial direction, and FIG. 1B is a cross-sectional view taken along line A-A ′ in FIG. The magnetic bearing has an annular stator 1 disposed outside and a rotor 2 disposed inside the stator 1.

ステータ1は継鉄11から構成されている。継鉄11は、積層鋼板等の磁性材料からなり、環状部12と、2つの主突極部13と、2つの補突極部14とを有する。一方、ロータ2は、少なくとも外周面に積層鋼板や電磁材料等の磁性体を配したもので、ステータ1の内側に回転軸2aを軸心として回転可能に配置されている。   The stator 1 is composed of a yoke 11. The yoke 11 is made of a magnetic material such as a laminated steel plate, and has an annular portion 12, two main salient pole portions 13, and two auxiliary salient pole portions 14. On the other hand, the rotor 2 has a magnetic material such as a laminated steel plate or electromagnetic material disposed on at least an outer peripheral surface thereof, and is disposed inside the stator 1 so as to be rotatable about a rotating shaft 2a.

2つの主突極部13は、この環状部12の内側から中心に向けて突出し、ロータ2の外周面と所定のギャップを介して対向する磁気集中部を有しており、周方向に180°の間隔で配置されている。また、図1(b)に示すように、主突極部13は、ロータ2の軸方向(Z軸方向)と平行な軸を中心に巻回されたアキシャル励磁コイル15を備えている。この主突極部13とアキシャル励磁コイル15とにより2つの主極3(3(1)、3(2))が形成されている。アキシャル励磁コイル15は、後述する磁束センサ17の検出出力に基づき励磁電流の大きさ及び向きを変化させることにより、ロータ2の軸方向の位置制御を行うためのものである。   The two main salient pole portions 13 protrude from the inside of the annular portion 12 toward the center, and have a magnetic concentration portion facing the outer peripheral surface of the rotor 2 via a predetermined gap, and 180 ° in the circumferential direction. Are arranged at intervals. Further, as shown in FIG. 1B, the main salient pole portion 13 includes an axial excitation coil 15 wound around an axis parallel to the axial direction (Z-axis direction) of the rotor 2. The main salient pole portion 13 and the axial excitation coil 15 form two main poles 3 (3 (1), 3 (2)). The axial excitation coil 15 is for performing axial position control of the rotor 2 by changing the magnitude and direction of the excitation current based on the detection output of the magnetic flux sensor 17 described later.

また、補突極部14は、主突極部13から周方向に90°ずれた位置に形成されており、その先端には永久磁石16が装着されている。この補突極部14と永久磁石16とにより、2つの補極4(4(1)〜4(2))が形成されている。永久磁石16は、主極3にバイアス磁束φbを提供するためのものである。永久磁石16は、第1の極性(例えばS極)をロータ2に向かう先端側にして装着されている。S極が先端側の場合、バイアス磁束φbは、補突極部14の底部から環状部12を介して隣接する主突極部13に至り、更にロータ2を介して補突極部14に戻る経路に形成される。これにより、主極3の先端である磁束集中部はN極となる。   Further, the supplementary salient pole part 14 is formed at a position shifted by 90 ° in the circumferential direction from the main salient pole part 13, and a permanent magnet 16 is attached to the tip thereof. The complementary salient pole portion 14 and the permanent magnet 16 form two complementary poles 4 (4 (1) to 4 (2)). The permanent magnet 16 is for providing a bias magnetic flux φb to the main pole 3. The permanent magnet 16 is mounted with the first polarity (for example, the S pole) set to the tip side toward the rotor 2. When the south pole is on the tip side, the bias magnetic flux φb reaches from the bottom of the auxiliary salient pole part 14 to the adjacent main salient pole part 13 via the annular part 12 and then returns to the auxiliary salient pole part 14 via the rotor 2. Formed in the path. Thereby, the magnetic flux concentration part which is the front-end | tip of the main pole 3 turns into N pole.

また、各補極4(i)の先端すなわち永久磁石16の先端には、磁束を検出するための磁束センサ17A(i)、17B(i)が装着されている(i=1、2)。この磁束センサ17は、例えばホール素子等である。1つの永久磁石16に装着される磁束センサ17A(i)、17B(i)は、図1(b)に示すように、軸方向(Z方向)に関し異なる位置に装着されている。ここでは、磁束センサ17A(i)が、17B(i)よりもZ方向に関し上側に存在するものとする。   Further, magnetic flux sensors 17A (i) and 17B (i) for detecting magnetic flux are attached to the tip of each auxiliary pole 4 (i), that is, the tip of the permanent magnet 16 (i = 1, 2). The magnetic flux sensor 17 is, for example, a Hall element. The magnetic flux sensors 17A (i) and 17B (i) attached to one permanent magnet 16 are attached at different positions in the axial direction (Z direction) as shown in FIG. 1 (b). Here, it is assumed that the magnetic flux sensor 17A (i) is present above the Z direction with respect to 17B (i).

図1(b)にも示すように、ロータ2の少なくとも外周面側は円板状に形成され、その外周面の軸方向幅は、少なくとも主突極部13の軸方向幅よりも小さく設定されている。このため、バイアス磁束φbは、主極3とロータ2の間のギャップ部分においては、主極3の上側から下方向に向かう磁束φbaと、主極3の下側から上方向に向かう磁束φbbとなる。
アキシャル励磁コイル15に励磁電流が流れていない場合には、この磁束φbaとφbbの軸方向成分が均等であり相殺されるので、軸方向成分の磁束は発生せず、ロータ2にも軸方向の力は加わらない。
As shown in FIG. 1B, at least the outer peripheral surface side of the rotor 2 is formed in a disc shape, and the axial width of the outer peripheral surface is set to be at least smaller than the axial width of the main salient pole portion 13. ing. Therefore, in the gap portion between the main pole 3 and the rotor 2, the bias magnetic flux φb is a magnetic flux φba that goes from the upper side of the main pole 3 to the lower side, and a magnetic flux φbb that goes from the lower side of the main pole 3 to the upper side. Become.
When no excitation current flows through the axial excitation coil 15, the axial components of the magnetic fluxes φba and φbb are equal and cancel each other, so that no magnetic flux of the axial component is generated and the rotor 2 also has an axial direction. No power is applied.

アキシャル励磁コイル15に励磁電流が例えば図1(b)に示す方向に流れている場合には、図1に矢印で示す方向にアキシャル制御磁束φcaが形成される。このアキシャル制御磁束φcaは、磁束φbbを強める一方、磁束φbaを弱めるように作用する。これにより、ロータ2には図1(b)に示すように下向き(Z軸負方向)の力Fが加わり、ロータ2は下方向に移動する。アキシャル励磁コイル15の励磁電流が図1(b)とは逆方向に流れる場合、力Fも図1(b)とは逆に下向きとなる。このように、アキシャル励磁コイル15の励磁電流の大きさ及び向きを制御することにより、ロータ2の軸方向の位置制御が可能となる。励磁電流の制御は、磁束センサ17の検出出力に基づき、制御回路102により行われる。例えば、上側の磁束センサ17A(1)と17A(2)の和と、下側の磁束センサ17B(1)、17B(2)の和との差をコンパレータ101で演算し、この演算出力に基づき、制御回路102において励磁電流の制御を行うことができる。   When an exciting current flows through the axial exciting coil 15 in the direction shown in FIG. 1B, for example, the axial control magnetic flux φca is formed in the direction shown by the arrow in FIG. The axial control magnetic flux φca acts to strengthen the magnetic flux φbb while weakening the magnetic flux φba. Thereby, a downward force (Z-axis negative direction) force F is applied to the rotor 2 as shown in FIG. 1B, and the rotor 2 moves downward. When the exciting current of the axial exciting coil 15 flows in the direction opposite to that shown in FIG. 1B, the force F also becomes downward as opposed to FIG. In this way, by controlling the magnitude and direction of the excitation current of the axial excitation coil 15, the axial position of the rotor 2 can be controlled. The excitation current is controlled by the control circuit 102 based on the detection output of the magnetic flux sensor 17. For example, the difference between the sum of the upper magnetic flux sensors 17A (1) and 17A (2) and the sum of the lower magnetic flux sensors 17B (1) and 17B (2) is calculated by the comparator 101, and based on this calculation output The control circuit 102 can control the excitation current.

図2に、本発明の第2の実施の形態に係る3極型の磁気軸受を示す。図1の構成要素と同一の構成要素については同一の符号を付し、その詳細な説明は省略する。この磁気軸受は、ロータ2の軸方向の位置制御に加え、ロータ2の傾き制御(チルト制御)、及びステータ1の径方向(ラジアル方向)の制御も行うことを可能にしたものである。すなわち、主極3は、ステータ1の周方向に120°間隔で形成され、補極4は各主極3から60°ずれた位置に、周方向に120°間隔で形成される。主極3には、径方向を軸心として巻回されたラジアル励磁コイル18が設置されている。このラジアル励磁コイル18は、バイアス磁束φbにより形成された主極3の先端(磁束集中部)の磁極を強めたり弱めたりするためのラジアル励磁磁束φrを発生させるためのものである。ラジアル励磁磁束φrの変化に基づいて主極3の磁極が制御されることにより、ロータ2の径方向の位置制御が行われる。
また、この実施の形態では、3つの主極3に設けられた3つのアキシャル励磁コイル120に流れる励磁電流を各々異ならせることにより、ロータ2の軸方向の位置制御だけでなく、傾き(X軸方向のチルト角θx、Y軸方向のチルト角θy)の制御も行うことができる。
FIG. 2 shows a three-pole magnetic bearing according to the second embodiment of the present invention. The same components as those in FIG. 1 are denoted by the same reference numerals, and detailed description thereof is omitted. This magnetic bearing makes it possible to perform tilt control (tilt control) of the rotor 2 and control in the radial direction (radial direction) of the stator 1 in addition to position control of the rotor 2 in the axial direction. That is, the main poles 3 are formed at intervals of 120 ° in the circumferential direction of the stator 1, and the auxiliary poles 4 are formed at positions shifted by 60 ° from the main poles 3 at intervals of 120 ° in the circumferential direction. The main pole 3 is provided with a radial excitation coil 18 wound around the radial direction as an axis. The radial excitation coil 18 is for generating a radial excitation magnetic flux φr for strengthening or weakening the magnetic pole at the tip (magnetic flux concentrating portion) of the main pole 3 formed by the bias magnetic flux φb. The position of the rotor 2 in the radial direction is controlled by controlling the magnetic pole of the main pole 3 based on the change in the radial excitation magnetic flux φr.
In this embodiment, the excitation currents flowing through the three axial excitation coils 120 provided on the three main poles 3 are made different from each other, so that not only the axial position control of the rotor 2 but also the inclination (X axis The tilt angle θx in the direction and the tilt angle θy in the Y-axis direction can also be controlled.

ラジアル励磁コイル18の励磁電流は、アキシャル励磁コイル15と同様に、磁束センサ17の検出出力に基づいて制御される。
この制御を行うための制御回路を含む制御系の構成を、図3に示す。この制御系は、アキシャル制御系100と、ラジアル制御系200とから構成される。
アキシャル制御系100は、コンパレータ101A−C、座標変換回路103、制御回路102’、座標変換回路104、及びパワーアンプ105A−Cから構成される。コンパレータ101A―Cは、それぞれ補極4(i)に設置された磁束センサ17A(i)及び17B(i)の検出出力の差分を演算するものである。
座標変換回路103は、この磁束センサ17で検出された検出出力に基づき、図3に示すXY座標を基準とした軸方向変位(Z)、チルト角(θx、θy)を求め、z方向変位信号、θx方向変位信号、及びθy方向変位信号を制御回路102’に出力する。制御回路102’は、これら変位信号に基づいて、例えばPID制御信号を出力する。座標変換回路104は、このPID制御信号を、アキシャル励磁コイル15の位置に対応した3相の座標系の信号に変換し、これをパワーアンプ105A−Cで増幅してアキシャル励磁コイル15に印加する。チルト角θx、θyが検出された場合には、3つのアキシャル励磁コイル15に流れる励磁電流の大きさを互いに異ならせることにより、ロータ2のチルト角の制御を行うことができる。
The excitation current of the radial excitation coil 18 is controlled based on the detection output of the magnetic flux sensor 17 in the same manner as the axial excitation coil 15.
A configuration of a control system including a control circuit for performing this control is shown in FIG. This control system includes an axial control system 100 and a radial control system 200.
The axial control system 100 includes a comparator 101A-C, a coordinate conversion circuit 103, a control circuit 102 ′, a coordinate conversion circuit 104, and a power amplifier 105A-C. The comparators 101A-C calculate the difference between the detection outputs of the magnetic flux sensors 17A (i) and 17B (i) installed on the complementary pole 4 (i), respectively.
The coordinate conversion circuit 103 obtains an axial displacement (Z) and a tilt angle (θx, θy) with reference to the XY coordinates shown in FIG. 3 based on the detection output detected by the magnetic flux sensor 17, and a z-direction displacement signal. , Θx direction displacement signal and θy direction displacement signal are output to the control circuit 102 ′. The control circuit 102 ′ outputs, for example, a PID control signal based on these displacement signals. The coordinate conversion circuit 104 converts the PID control signal into a three-phase coordinate system signal corresponding to the position of the axial excitation coil 15, amplifies the signal by the power amplifier 105 </ b> A-C, and applies it to the axial excitation coil 15. . When the tilt angles θx and θy are detected, the tilt angle of the rotor 2 can be controlled by making the magnitudes of the excitation currents flowing through the three axial excitation coils 15 different from each other.

ラジアル制御系200は、加算器201A−Cと、座標変換回路202と、制御回路203と、パワーアンプ204A−Cから構成される。
コンパレータ201A−Cは、それぞれ、1つの補極4(i)に設置された2つの磁束センサ17A(i)及び17B(i)の検出出力の和を出力する。座標変換回路202は、この磁束センサ17で検出された検出出力に基づき、図3に示すXY座標を基準としたX方向変位(x)、Y方向変位(y)を求め、X方向変位信号、Y方向変位信号を制御回路203に出力する。
制御回路203は、これら変位信号に基づいて、ラジアル励磁コイル18の位置に対応した3相の座標系に従ったPID制御信号を生成し、これをパワーアンプ204A−Cで増幅してラジアル励磁コイル18に印加する。
The radial control system 200 includes an adder 201A-C, a coordinate conversion circuit 202, a control circuit 203, and a power amplifier 204A-C.
Each of the comparators 201A-C outputs the sum of the detection outputs of the two magnetic flux sensors 17A (i) and 17B (i) installed on one complementary pole 4 (i). The coordinate conversion circuit 202 obtains an X-direction displacement (x) and a Y-direction displacement (y) based on the XY coordinates shown in FIG. 3 based on the detection output detected by the magnetic flux sensor 17, and obtains an X-direction displacement signal, A Y direction displacement signal is output to the control circuit 203.
Based on these displacement signals, the control circuit 203 generates a PID control signal in accordance with a three-phase coordinate system corresponding to the position of the radial excitation coil 18, and amplifies the PID control signal with the power amplifier 204A-C to generate the radial excitation coil. 18 is applied.

図4は、本発明の第3の実施の形態に係る4極型の磁気軸受の構成を示す。
この磁気軸受は、4つの主極3(i)が、図4に示すXY座標系において、周方向に0°、90°、180°、170°と90°間隔で形成される。主極3(i)から45°周方向にずれた位置に、45°、135°、225°、315°と90°間隔で4つの補極(i)が形成されている。その他は上記の実施の形態と同様である。
FIG. 4 shows the configuration of a four-pole magnetic bearing according to the third embodiment of the present invention.
In the magnetic bearing, four main poles 3 (i) are formed at intervals of 0 °, 90 °, 180 °, and 170 ° in the circumferential direction in the XY coordinate system shown in FIG. Four complementary poles (i) are formed at intervals of 45 °, 135 °, 225 °, 315 ° and 90 ° at positions shifted from the main pole 3 (i) by 45 ° in the circumferential direction. Others are the same as in the above embodiment.

この図4の実施の形態の制御を行うための制御回路を含む制御系の構成を、図5に示す。アキシャル制御系100は、コンパレータ101A’−C’、制御回路102A’−C’、及び演算増幅器106A−Cから構成される。
コンパレータ101A’は、各補極4(i)に設置された磁束センサ17A(i)(i=1〜4)の検出出力の総和と、磁束センサ17B(i)(i=1〜4)の検出出力の総和の差分を演算するものである。この差分は、ロータ2のZ方向変位信号として制御回路102A’に出力される。
また、コンパレータ101B’は、補極4(1)、4(4)の上側の磁束センサ17A(1)及び17A(4)の検出出力の和と、下側の磁束センサ17B(1)及び17B(4)の和との差分を演算するものである。この差分は、ロータ2のθx方向変位信号として制御回路102B’に出力される。
また、コンパレータ101C’は、補極4(1)、4(2)の上側の磁束センサ17A(1)及び17A(2)の検出出力の和と、下側の磁束センサ17B(1)及び17B(2)の和との差分を演算するものである。この差分は、ロータ2のθy方向変位信号として制御回路102C’に出力される。
FIG. 5 shows the configuration of a control system including a control circuit for performing the control of the embodiment of FIG. The axial control system 100 includes a comparator 101A′-C ′, a control circuit 102A′-C ′, and an operational amplifier 106A-C.
The comparator 101A ′ includes the sum of the detection outputs of the magnetic flux sensors 17A (i) (i = 1 to 4) installed in the respective complementary electrodes 4 (i) and the magnetic flux sensors 17B (i) (i = 1 to 4). The difference between the sums of the detection outputs is calculated. This difference is output to the control circuit 102A ′ as a Z direction displacement signal of the rotor 2.
Further, the comparator 101B ′ includes the sum of the detection outputs of the upper magnetic flux sensors 17A (1) and 17A (4) of the complementary poles 4 (1) and 4 (4) and the lower magnetic flux sensors 17B (1) and 17B. The difference with the sum of (4) is calculated. This difference is output to the control circuit 102B ′ as a displacement signal of the rotor 2 in the θx direction.
Further, the comparator 101C ′ includes the sum of the detection outputs of the upper magnetic flux sensors 17A (1) and 17A (2) of the complementary poles 4 (1) and 4 (2) and the lower magnetic flux sensors 17B (1) and 17B. The difference from the sum of (2) is calculated. This difference is output to the control circuit 102C ′ as a displacement signal of the rotor 2 in the θy direction.

制御回路102A’〜C’は、これら変位信号に基づいて、ラジアル励磁コイル18の位置に対応した3相の座標系に従ったPID制御信号を生成する。演算増幅器106A−Dは、このPID制御信号に基づいて各アキシャル励磁コイル15の励磁電流を制御する。   Based on these displacement signals, the control circuits 102 </ b> A ′ to C ′ generate a PID control signal according to a three-phase coordinate system corresponding to the position of the radial excitation coil 18. The operational amplifiers 106A-D control the excitation current of each axial excitation coil 15 based on this PID control signal.

図6は、本発明の第4の実施の形態に係る3極型の磁気軸受を示す。この実施の形態では、永久磁石16を各補極4の先端に形成する代わりに、ロータ2の外周面全体に亘って永久磁石16’を形成する点において、上記の実施の形態と異なっている。ラジアル制御系200は、第2の実施の形態とほぼ同様である。ただし、主極3、補極4のXY座標系に対する位置が異なっているため、座標変換回路202での変換式は第2の実施の形態とは異なっている。   FIG. 6 shows a three-pole magnetic bearing according to the fourth embodiment of the present invention. This embodiment differs from the above embodiment in that the permanent magnet 16 'is formed over the entire outer peripheral surface of the rotor 2 instead of forming the permanent magnet 16 at the tip of each auxiliary pole 4. . The radial control system 200 is almost the same as in the second embodiment. However, since the positions of the main pole 3 and the complementary pole 4 with respect to the XY coordinate system are different, the conversion formula in the coordinate conversion circuit 202 is different from that in the second embodiment.

また、アキシャル制御系100は、コンパレータ101A”〜C”、制御回路102A”〜C”、及び演算増幅器106A’〜C’を備えている。
コンパレータ101A”は、各補極4(i)に設置された磁束センサ17A(i)(i=1〜3)の検出出力の総和と、磁束センサ17B(i)(i=1〜3)の検出出力の総和との差分を演算するものである。この差分は、ロータ2のZ方向変位信号として制御回路102A”に出力される。
また、コンパレータ101B”は、ロータ2のX軸方向のチルト角θxを検出するため、磁束センサ17A(1)、17B(2)及び17B(3)の総和と、磁束センサ17A(2)、17A(3)及び17B(1)の総和との差分を演算するものである。この差分は、ロータ2のθx方向変位信号として制御回路102B’に出力される。
Further, the axial control system 100 includes comparators 101A ″ to C ″, control circuits 102A ″ to C ″, and operational amplifiers 106A ′ to C ′.
The comparator 101A ″ includes the sum of the detection outputs of the magnetic flux sensors 17A (i) (i = 1 to 3) installed in the respective complementary electrodes 4 (i) and the magnetic flux sensors 17B (i) (i = 1 to 3). This is to calculate a difference from the sum of the detection outputs. This difference is output to the control circuit 102A ″ as a Z direction displacement signal of the rotor 2.
Further, the comparator 101B ″ detects the tilt angle θx of the rotor 2 in the X-axis direction, so that the sum of the magnetic flux sensors 17A (1), 17B (2) and 17B (3) and the magnetic flux sensors 17A (2), 17A The difference between the sum of (3) and 17B (1) is calculated, and this difference is output to the control circuit 102B ′ as a displacement signal in the θx direction of the rotor 2.

また、コンパレータ101C’は、ロータ2のY軸方向のチルト角θyを検出するため、磁束センサ17A(1)、17B(1)、17B(2)及び17A(3)の総和と、磁束センサ17A(2)及び17B(3)の総和との差分を演算するものである。この差分は、ロータ2のθy方向変位信号として制御回路102C’に出力される。   Further, the comparator 101C ′ detects the tilt angle θy of the rotor 2 in the Y-axis direction, and the sum of the magnetic flux sensors 17A (1), 17B (1), 17B (2) and 17A (3), and the magnetic flux sensor 17A. The difference between the sum of (2) and 17B (3) is calculated. This difference is output to the control circuit 102C ′ as a displacement signal of the rotor 2 in the θy direction.

制御回路102A”〜C”は、これらの変位信号に基づいて、ラジアル励磁コイル18の位置に対応した3相の座標系に従ったPID制御信号を生成する。演算増幅器106A’〜C’は、このPID制御信号に基づいて各アキシャル励磁コイル15の励磁電流を制御する。
なお、この図6に示すラジアル制御系200,アキシャル制御系100の構成は、図3に示す構成に置き換えることも可能である。
Based on these displacement signals, the control circuits 102A ″ to C ″ generate PID control signals according to a three-phase coordinate system corresponding to the position of the radial excitation coil 18. The operational amplifiers 106A ′ to C ′ control the excitation current of each axial excitation coil 15 based on the PID control signal.
The configuration of the radial control system 200 and the axial control system 100 shown in FIG. 6 can be replaced with the configuration shown in FIG.

図7は、第2の実施の形態の第1の変形例を示す。この例では、永久磁石16”が、補極4だけでなく主極3の先端にも形成されている点で、第2の実施の形態と異なっている。なお、アキシャル制御系100、及びラジアル制御系200の構成は図6の構成と同様であるが、図3の構成と同様にしてもよいことは言うまでもない。   FIG. 7 shows a first modification of the second embodiment. This example is different from the second embodiment in that the permanent magnet 16 ″ is formed not only at the auxiliary pole 4 but also at the tip of the main pole 3. Note that the axial control system 100 and radial are different. The configuration of the control system 200 is the same as the configuration of FIG. 6, but it goes without saying that it may be the same as the configuration of FIG.

図8は、第2の実施の形態の第2の変形例を示す。この例では、永久磁石16が、ステータの環状部12に環状に埋め込まれている点で、第2の実施の形態と異なっている。この環状の永久磁石に加えて、上記の実施の形態と同様の位置に更に永久磁石を設置することも可能である。なお、アキシャル制御系100、及びラジアル制御系200の構成は、図3、図6の構成のいずれでも採用することができる。   FIG. 8 shows a second modification of the second embodiment. This example is different from the second embodiment in that the permanent magnet 16 is embedded in the annular portion 12 of the stator in an annular shape. In addition to this annular permanent magnet, it is also possible to install a permanent magnet at the same position as in the above embodiment. Note that the configurations of the axial control system 100 and the radial control system 200 may be any of the configurations shown in FIGS. 3 and 6.

以上、発明の実施の形態を説明したが、本発明はこれらに限定されるものではなく、発明の趣旨を逸脱しない範囲内において種々の変更、追加、置換等が可能である。   Although the embodiments of the invention have been described above, the present invention is not limited to these embodiments, and various modifications, additions, substitutions, and the like can be made without departing from the spirit of the invention.

本発明の第1の実施の形態に係る磁気軸受の平面図及び断面図である。It is the top view and sectional view of a magnetic bearing concerning a 1st embodiment of the present invention. 本発明の第2の実施の形態に係る3極型の磁気軸受の平面図及び断面図である。It is a top view and a sectional view of a 3 pole type magnetic bearing concerning a 2nd embodiment of the present invention. 第2の実施の形態の磁気軸受の制御を行うための制御回路を含む制御系の構成を示す。The structure of the control system containing the control circuit for controlling the magnetic bearing of 2nd Embodiment is shown. 本発明の第3の実施の形態に係る4極型の磁気軸受の平面図及び断面図である。It is the top view and sectional view of a 4 pole type magnetic bearing concerning a 3rd embodiment of the present invention. 第3の実施の形態の磁気軸受の制御を行うための制御回路を含む制御系の構成を示す。The structure of the control system containing the control circuit for controlling the magnetic bearing of 3rd Embodiment is shown. 本発明の第4の実施の形態に係る3極型の磁気軸受の平面図及び断面図である。It is the top view and sectional drawing of a 3 pole type magnetic bearing which concern on the 4th Embodiment of this invention. 第2の実施の形態の第1の変形例を示す。The 1st modification of 2nd Embodiment is shown. 第2の実施の形態の第2の変形例を示す。The 2nd modification of 2nd Embodiment is shown.

符号の説明Explanation of symbols

1・・・ステータ、 2・・・ロータ、 3・・・主極、 4・・・補極、 111・・・継鉄、 12・・・環状部、 13・・・主突極部、 14・・・補突極部、 15・・・アキシャル励磁コイル、 16・・・永久磁石、 17・・・磁束センサ、 18・・・ラジアル励磁コイル。   DESCRIPTION OF SYMBOLS 1 ... Stator, 2 ... Rotor, 3 ... Main pole, 4 ... Supplementary pole, 111 ... Relay, 12 ... Annular part, 13 ... Main salient pole part, 14 ... complementary salient poles, 15 ... axial excitation coil, 16 ... permanent magnet, 17 ... magnetic flux sensor, 18 ... radial excitation coil.

Claims (7)

ステータと、このステータに磁気力によって非接触状態で支持されて回転軸を中心に回転するロータとを有する磁気軸受において、
前記ステータは、前記ロータに所定のギャップを介して対向し軸方向成分を含む磁束が集中する磁束集中部を有し且つ前記ステータの周方向に所定の間隔で配置される複数の主極、及び先端部において前記ロータに所定のギャップを介して対向し且つ前記複数の主極に対して前記周方向にずれた位置に配置される複数の補極を含み、
前記補極の先端部を第1極性とし隣接する前記主極の磁束集中部を第2極性とするようなバイアス磁束を供給する永久磁石と、
前記複数の主極に設けられ前記バイアス磁束の強度を前記軸方向の一方の側においては強め他方の側では弱めることにより前記ロータの軸方向の位置を制御するアキシャル制御磁束を発生させるアキシャル励磁コイルと、
前記複数の補極の先端に設けられる複数の磁束センサと、
前記複数の磁束センサの検出信号に基づいて前記アキシャル励磁コイルに流れる励磁電流を制御する制御部と
を備えたことを特徴とする磁気軸受。
In a magnetic bearing having a stator and a rotor that is supported by the stator in a non-contact state by a magnetic force and rotates about a rotation axis,
The stator has a plurality of main poles that are opposed to the rotor via a predetermined gap and have a magnetic flux concentrating portion in which a magnetic flux including an axial component is concentrated, and are arranged at predetermined intervals in the circumferential direction of the stator, and A plurality of complementary poles disposed at positions that are opposed to the rotor via a predetermined gap at the tip and are displaced in the circumferential direction with respect to the plurality of main poles;
A permanent magnet for supplying a bias magnetic flux so that the tip of the auxiliary pole has a first polarity and the magnetic flux concentrating portion of the adjacent main pole has a second polarity;
An axial excitation coil that is provided in the plurality of main poles and generates an axial control magnetic flux that controls the position of the rotor in the axial direction by increasing the intensity of the bias magnetic flux on one side in the axial direction and weakening it on the other side. When,
A plurality of magnetic flux sensors provided at tips of the plurality of complementary poles;
A magnetic bearing comprising: a control unit that controls an excitation current flowing through the axial excitation coil based on detection signals of the plurality of magnetic flux sensors.
前記ステータは、前記ロータより厚く形成される請求項1記載の磁気軸受。   The magnetic bearing according to claim 1, wherein the stator is formed thicker than the rotor. 前記磁束センサは、前記複数の補極の各々において、軸方向の異なる位置に複数個設けられる請求項1記載の磁気軸受。   The magnetic bearing according to claim 1, wherein a plurality of the magnetic flux sensors are provided at different positions in the axial direction in each of the plurality of auxiliary poles. 前記制御部は、前記複数の補極の1つに設けられた前記磁束センサの検出出力の差に基づいて前記アキシャル励磁コイルの励磁電流を制御する請求項3記載の磁気軸受。   The magnetic bearing according to claim 3, wherein the control unit controls an excitation current of the axial excitation coil based on a difference in detection output of the magnetic flux sensor provided in one of the plurality of auxiliary poles. 前記永久磁石は、前記補極の先端に設けられた請求項1記載の磁気軸受。   The magnetic bearing according to claim 1, wherein the permanent magnet is provided at a tip of the auxiliary pole. 前記永久磁石は、前記ロータの外周面に設けられた請求項1記載の磁気軸受。   The magnetic bearing according to claim 1, wherein the permanent magnet is provided on an outer peripheral surface of the rotor. 前記永久磁石は、前記ステータの環状部に設けられた請求項1記載の磁気軸受。   The magnetic bearing according to claim 1, wherein the permanent magnet is provided in an annular portion of the stator.
JP2004343596A 2004-11-29 2004-11-29 Magnetic bearing Active JP4138735B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2004343596A JP4138735B2 (en) 2004-11-29 2004-11-29 Magnetic bearing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2004343596A JP4138735B2 (en) 2004-11-29 2004-11-29 Magnetic bearing

Publications (2)

Publication Number Publication Date
JP2006153117A true JP2006153117A (en) 2006-06-15
JP4138735B2 JP4138735B2 (en) 2008-08-27

Family

ID=36631666

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2004343596A Active JP4138735B2 (en) 2004-11-29 2004-11-29 Magnetic bearing

Country Status (1)

Country Link
JP (1) JP4138735B2 (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008069964A (en) * 2006-08-18 2008-03-27 Toru Masuzawa Hybrid-type magnetic bearing
JP2010106908A (en) * 2008-10-29 2010-05-13 Oitaken Sangyo Sozo Kiko Magnetic bearing
CN101893038A (en) * 2010-08-04 2010-11-24 南京化工职业技术学院 Permanent magnet biased axial magnetic bearing
CN102155492A (en) * 2011-05-18 2011-08-17 哈尔滨工业大学 Mixed type driving and driven magnetic suspension bearing
CN102829709A (en) * 2012-08-01 2012-12-19 北京海斯德电机技术有限公司 Radial magnetic bearing electrical vortex sensor integrated structure for magnetic levitation high-speed electric machine
CN107035769A (en) * 2017-03-24 2017-08-11 南京航空航天大学 A kind of contactless hub-bearing unit and its magnetic force control method
CN113565875A (en) * 2021-08-24 2021-10-29 珠海格力电器股份有限公司 Homopolar radial magnetic suspension bearing, compressor and air conditioner
CN115263923A (en) * 2022-09-20 2022-11-01 山东天瑞重工有限公司 Permanent magnet biased radial magnetic bearing

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63210414A (en) * 1987-02-24 1988-09-01 Toshiba Corp Magnetic bearing device
JPH0484826U (en) * 1990-11-29 1992-07-23
JPH08121478A (en) * 1994-10-18 1996-05-14 Fuji Xerox Co Ltd Bearing device
JPH11101234A (en) * 1997-09-26 1999-04-13 Seiko Seiki Co Ltd Magnetic bearing device
JP2001041238A (en) * 1999-07-28 2001-02-13 Seiko Seiki Co Ltd Composite type electromagnet and radial magnetic bearing

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63210414A (en) * 1987-02-24 1988-09-01 Toshiba Corp Magnetic bearing device
JPH0484826U (en) * 1990-11-29 1992-07-23
JPH08121478A (en) * 1994-10-18 1996-05-14 Fuji Xerox Co Ltd Bearing device
JPH11101234A (en) * 1997-09-26 1999-04-13 Seiko Seiki Co Ltd Magnetic bearing device
JP2001041238A (en) * 1999-07-28 2001-02-13 Seiko Seiki Co Ltd Composite type electromagnet and radial magnetic bearing

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008069964A (en) * 2006-08-18 2008-03-27 Toru Masuzawa Hybrid-type magnetic bearing
JP2010106908A (en) * 2008-10-29 2010-05-13 Oitaken Sangyo Sozo Kiko Magnetic bearing
CN101893038A (en) * 2010-08-04 2010-11-24 南京化工职业技术学院 Permanent magnet biased axial magnetic bearing
CN102155492A (en) * 2011-05-18 2011-08-17 哈尔滨工业大学 Mixed type driving and driven magnetic suspension bearing
CN102829709A (en) * 2012-08-01 2012-12-19 北京海斯德电机技术有限公司 Radial magnetic bearing electrical vortex sensor integrated structure for magnetic levitation high-speed electric machine
CN107035769A (en) * 2017-03-24 2017-08-11 南京航空航天大学 A kind of contactless hub-bearing unit and its magnetic force control method
CN107035769B (en) * 2017-03-24 2018-11-09 南京航空航天大学 A kind of contactless hub-bearing unit and its magnetic force control method
CN113565875A (en) * 2021-08-24 2021-10-29 珠海格力电器股份有限公司 Homopolar radial magnetic suspension bearing, compressor and air conditioner
CN115263923A (en) * 2022-09-20 2022-11-01 山东天瑞重工有限公司 Permanent magnet biased radial magnetic bearing
CN115263923B (en) * 2022-09-20 2022-12-23 山东天瑞重工有限公司 Permanent magnet biased radial magnetic bearing

Also Published As

Publication number Publication date
JP4138735B2 (en) 2008-08-27

Similar Documents

Publication Publication Date Title
JP4616122B2 (en) Magnetic bearing
EP2239831B1 (en) Magnetic levitaion motor and pump
EP2209186B1 (en) Magnetically-levitated motor and pump
US6885121B2 (en) Controlled radial magnetic bearing
KR100403857B1 (en) Motor of magnetic lifting type
US20110163622A1 (en) Combination Radial/Axial Electromagnetic Actuator
JP6627400B2 (en) Electric motor, control device, and motor control system
WO2011114912A1 (en) Bearingless motor
JP2009506747A (en) Ironless magnetic linear motor with levitation and lateral force capability
JP2005061578A (en) Magnetic bearing
Karutz et al. Novel magnetically levitated two-level motor
JP4138735B2 (en) Magnetic bearing
JP2016501003A (en) Rotating positioning device
JP2007009949A (en) Hybrid type magnetic bearing
WO2022004144A1 (en) Rotary drive device and pump
JP5192271B2 (en) Magnetic bearing device
JP2008069964A (en) Hybrid-type magnetic bearing
JP4513458B2 (en) Magnetic bearing device and flywheel energy storage device including the same
JP2008256084A (en) Magnetic bearing device and magnetic bearing spindle device
JP4138739B2 (en) Magnetic bearing
KR20110072896A (en) Toroidally-wound self-bearing brushless dc motor
US7719152B2 (en) Magnetic levitation actuator
JP2007306785A (en) Bearingless motor and bearingless motor control system
JP4220859B2 (en) Magnetic bearing
EP1072803A2 (en) Magnetic bearing device

Legal Events

Date Code Title Description
A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20080523

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20080603

A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20080605

R150 Certificate of patent or registration of utility model

Ref document number: 4138735

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

Free format text: JAPANESE INTERMEDIATE CODE: R150

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20110613

Year of fee payment: 3

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20120613

Year of fee payment: 4

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20130613

Year of fee payment: 5

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250