JPS63259510A - Aeromagnetic bearing type of optical deflector - Google Patents
Aeromagnetic bearing type of optical deflectorInfo
- Publication number
- JPS63259510A JPS63259510A JP62092048A JP9204887A JPS63259510A JP S63259510 A JPS63259510 A JP S63259510A JP 62092048 A JP62092048 A JP 62092048A JP 9204887 A JP9204887 A JP 9204887A JP S63259510 A JPS63259510 A JP S63259510A
- Authority
- JP
- Japan
- Prior art keywords
- magnet
- rotating body
- thrust
- rotor magnet
- excitation
- 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
Links
- 230000003287 optical effect Effects 0.000 title claims description 6
- 230000005284 excitation Effects 0.000 abstract description 5
- BGPVFRJUHWVFKM-UHFFFAOYSA-N N1=C2C=CC=CC2=[N+]([O-])C1(CC1)CCC21N=C1C=CC=CC1=[N+]2[O-] Chemical compound N1=C2C=CC=CC2=[N+]([O-])C1(CC1)CCC21N=C1C=CC=CC1=[N+]2[O-] BGPVFRJUHWVFKM-UHFFFAOYSA-N 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
Classifications
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B26/00—Optical devices or arrangements for the control of light using movable or deformable optical elements
- G02B26/08—Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light
- G02B26/10—Scanning systems
- G02B26/12—Scanning systems using multifaceted mirrors
- G02B26/121—Mechanical drive devices for polygonal mirrors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C32/00—Bearings not otherwise provided for
- F16C32/04—Bearings not otherwise provided for using magnetic or electric supporting means
- F16C32/0406—Magnetic bearings
- F16C32/0408—Passive magnetic bearings
- F16C32/0423—Passive magnetic bearings with permanent magnets on both parts repelling each other
- F16C32/0427—Passive magnetic bearings with permanent magnets on both parts repelling each other for axial load mainly
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/02—Sliding-contact bearings for exclusively rotary movement for radial load only
- F16C17/026—Sliding-contact bearings for exclusively rotary movement for radial load only with helical grooves in the bearing surface to generate hydrodynamic pressure, e.g. herringbone grooves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C32/00—Bearings not otherwise provided for
- F16C32/04—Bearings not otherwise provided for using magnetic or electric supporting means
- F16C32/0402—Bearings not otherwise provided for using magnetic or electric supporting means combined with other supporting means, e.g. hybrid bearings with both magnetic and fluid supporting means
Abstract
Description
【発明の詳細な説明】
(技術分野)
本発明は永久磁石反発式の空気磁気軸受型光偏向器に関
する。DETAILED DESCRIPTION OF THE INVENTION (Technical Field) The present invention relates to a permanent magnet repulsion type air magnetic bearing type optical deflector.
この稲光偏向器はレーザプリンタ、デジタル複写機等の
レーザ光書き込み系に利用される。This lightning deflector is used in laser beam writing systems such as laser printers and digital copying machines.
(従来技術)
第2図に従来例に係る空気磁気軸受型の光偏向器の構成
を示す。(Prior Art) FIG. 2 shows the configuration of a conventional aeromagnetic bearing type optical deflector.
図において、中空回転体1は、中央部にミラー3が、下
部には駆動源となる面対向型のモータのロータマグネッ
ト組立体4,7.8が、上部には磁気軸受を構成するマ
グネット9が装着されて構成しである。In the figure, a hollow rotating body 1 has a mirror 3 in the center, rotor magnet assemblies 4, 7.8 of a surface-facing motor serving as a driving source in the lower part, and magnets 9 constituting a magnetic bearing in the upper part. is installed and configured.
一方固定軸11は、上部に磁気軸受用マグネット10が
装着されている。またこの固定軸11の表面には動圧空
気軸受のためのへリングボーン溝11a、llbを2対
有している。そして固定軸11の下端部はハウジング1
2に圧入固着あるいは焼きバメなどの方法で堅固に固定
されている。On the other hand, the fixed shaft 11 has a magnetic bearing magnet 10 attached to its upper part. Further, the surface of the fixed shaft 11 has two pairs of herringbone grooves 11a and 11b for dynamic pressure air bearings. The lower end of the fixed shaft 11 is connected to the housing 1.
2 by a method such as press-fitting or shrink-fitting.
スラスト磁気軸受は回転軸上端部及び固定軸11上端部
、及びケース13の上端部にその機能を有している。磁
気軸受は共に永久磁石で構成され、msは互いに向かい
合う面を同極とし、マグネット9は上下から反発させら
れ、回転体1を弾上させている。また、マグネットホル
ダー14はネジ部14aを有し、このネジ部の回転によ
り、ホルダー14内に収容されているマグネット15が
上下し、マグネット9との距離を変化させることによっ
て、マグネット9を取り付けた回転体1の浮上量を調整
することが出来る。The thrust magnetic bearing has its function at the upper end of the rotating shaft, the upper end of the fixed shaft 11, and the upper end of the case 13. Both of the magnetic bearings are made of permanent magnets, the faces of the ms facing each other have the same polarity, and the magnets 9 are repelled from above and below, causing the rotating body 1 to bounce up. Moreover, the magnet holder 14 has a threaded part 14a, and by rotating this threaded part, the magnet 15 housed in the holder 14 moves up and down, and by changing the distance from the magnet 9, the magnet 9 can be attached. The flying height of the rotating body 1 can be adjusted.
マグネット9,10.15はそれぞれホルダー14.1
6.17に収納されている。Magnets 9 and 10.15 are each holder 14.1
It is stored in 6.17.
以上の様な構成とした場合、モータ部が面対向型である
為、ロータマグネット4はどうしても径が大きくなって
しまい、高速回転させた場合、遠心力の影響によりロー
タマグネット4が破壊する恐れが多分にある。In the above configuration, since the motor part is a surface facing type, the diameter of the rotor magnet 4 inevitably becomes large, and when rotating at high speed, there is a risk that the rotor magnet 4 will be destroyed due to the influence of centrifugal force. Most likely.
さらにモータ部の励磁切換によるスラスト方向の振動を
生じてしまい、スラスト磁気軸受の外乱となってしまう
欠点もあった。Furthermore, there is also the drawback that vibration in the thrust direction occurs due to excitation switching of the motor section, which causes disturbance to the thrust magnetic bearing.
一方、モータ方式が上述の様な面対向型でな(インナー
ロータ型のものも公知である。On the other hand, the motor system is not the above-mentioned surface facing type (inner rotor type is also known).
しかしながら、従来のインナーロータ型のものは、中空
回転体の上端部に樹脂製で中央に空気の流通路を有する
スラスト止めを設けた構成を採用している(例えば特開
昭59−49516号)。However, the conventional inner rotor type has a structure in which a thrust stop made of resin and having an air flow path in the center is provided at the upper end of the hollow rotating body (for example, Japanese Patent Application Laid-open No. 59-49516). .
従ってこの様な従来例では上端部(スラスト止め部)が
接触している為、特に超高速回転(3万〜4万rpm)
の場合、起動停止が変型なると摩耗粉を生じ、回転不能
となり易いという不具合がある。Therefore, in such conventional examples, the upper end (thrust stop part) is in contact, so it cannot be rotated at particularly high speeds (30,000 to 40,000 rpm).
In this case, there is a problem in that if the start/stop is deformed, abrasion powder is generated and rotation is likely to become impossible.
(目的)
本発明は従来例の上述した欠点を解消し、安定して超高
速回転可能な光偏向器を提供することを目的とする。(Objective) An object of the present invention is to eliminate the above-mentioned drawbacks of the conventional example and to provide an optical deflector that can stably rotate at an ultra-high speed.
(構成)
本発明はインナーロータ型のモータ方式を前位とし、従
来例の如く、中空回転体に接触するスラスト止めを設け
ることなく、中空回転体の上端部のマグネットを、上下
のマグネットで隙間をおいて挾み、動圧軸受けを構成し
たものである。(Structure) The present invention uses an inner rotor type motor system at the front, and instead of providing a thrust stop that contacts the hollow rotating body as in the conventional example, the magnet at the upper end of the hollow rotating body is connected to the upper and lower magnets with a gap between the upper and lower magnets. The two are sandwiched together to form a dynamic pressure bearing.
以下、第1図に基づき本発明の一実施例を説明する。An embodiment of the present invention will be described below with reference to FIG.
第1図において、回転軸21にスラストマグネットホル
ダー22とスラストマグネット23を上部に配し、ミラ
ー25、ミラー押さえ24、さらにロータマグネット2
Gとバランス修正用リング27を装着し、回転体を構成
している。In FIG. 1, a thrust magnet holder 22 and a thrust magnet 23 are arranged on the rotating shaft 21, a mirror 25, a mirror holder 24, and a rotor magnet 2.
G and a balance correction ring 27 are attached to form a rotating body.
固定軸28は上部にきスラストマグネットホルダー29
とスラストマグネット30を配し、台座31に下端部で
圧入固着あるいは焼きバメなどの方法で堅固に固定され
ている。The fixed shaft 28 is located at the top and the thrust magnet holder 29
and a thrust magnet 30, which are firmly fixed to the pedestal 31 at the lower end by a method such as press-fitting or shrink-fitting.
28a、28bは固定軸28の外周面に設けた上部、下
部へリング溝である。28a and 28b are upper and lower ring grooves provided on the outer peripheral surface of the fixed shaft 28.
上述した様に本発明におけるモータ方式はインナーロー
タ型である。As mentioned above, the motor system in the present invention is an inner rotor type.
即ち、ロータマグネット26とコイル部32でモータ部
を構成しており、励磁切り換えにより、回転体(各部材
21〜27を組み立てたもの)は回転する。That is, the rotor magnet 26 and the coil section 32 constitute a motor section, and the rotating body (assembly of the members 21 to 27) rotates by switching the excitation.
従って、ロータマグネット26の径は従来と比較し、格
段に小さくする事が可能となる。さらにモータ部の励磁
切り換えによる振動はラジアル方向となり、実用上外乱
とはならない(軸受剛性はスラスト軸軸受に比ベラシア
ル動圧軸受の方が格段に高いので)。Therefore, the diameter of the rotor magnet 26 can be made much smaller than the conventional one. Furthermore, the vibration caused by excitation switching in the motor section is in the radial direction, and does not cause any disturbance in practice (because the bearing rigidity of a vertical hydrodynamic bearing is much higher than that of a thrust shaft bearing).
尚、33はケース、34はケースに取りつけた上部マグ
ネット、35はケース上蓋である。In addition, 33 is a case, 34 is an upper magnet attached to the case, and 35 is a case top lid.
(効果)
本発明は以上述べた通りであり、本発明によれば、回転
体の駆動方式をインナーロータ型とし、かつ3個の永久
磁石反発式を用いたスラスト磁気軸受で空気磁気軸受光
偏向器を構成した為、(1)超高速回転時にも面対向型
と比べ遠心力が小さくできる為、ロータマグネットの破
壊の恐れがなく、安定した回転が可能となる。(Effects) The present invention is as described above, and according to the present invention, the driving system of the rotating body is an inner rotor type, and the thrust magnetic bearing using three permanent magnet repulsion type is used for air magnetic bearing light deflection. (1) Even during ultra-high speed rotation, the centrifugal force can be smaller than that of the surface-facing type, so there is no risk of damage to the rotor magnet, and stable rotation is possible.
(2)スラスト方向の振動がない為、回転体の上下動が
極力押さえられ、安定した光の偏向が可能となる。(2) Since there is no vibration in the thrust direction, vertical movement of the rotating body is suppressed as much as possible, allowing stable light deflection.
(3)起動停止時にスラスト方向の接触が無い為、摩耗
粉の発生は殆ど無(、回転不能の恐れは極力押さえられ
る。(3) Since there is no contact in the thrust direction when starting and stopping, there is almost no generation of abrasion powder (and the risk of non-rotation is minimized).
等の効果を奏する。It has the following effects.
第1図は本発明の一実施例に係る空気磁気軸受型光偏向
器の縦断面図、第2図は従来例に係る、同縦断面図であ
る。
23.30.34・・・マグネット、26.32・・・
インナーロータ型モータ構成部。
代理人 弁理士 武 顕次部(
第1図
8bFIG. 1 is a longitudinal sectional view of an air magnetic bearing type optical deflector according to an embodiment of the present invention, and FIG. 2 is a longitudinal sectional view of the same according to a conventional example. 23.30.34...Magnet, 26.32...
Inner rotor type motor component. Agent: Patent Attorney Kenji Take (Figure 1, 8b)
Claims (1)
トにより、互いに反発するように挟持されたマグネット
を先端部に持ち、この反発力により浮上し、駆動源によ
り回転される回転体を有する空気磁気軸受型光偏向器で
あつて、回転体のモータ方式がインナーローター型であ
ることを特徴とする空気磁気軸受型光偏向器。An air magnetic bearing that has a magnet at the tip that is held between a magnet at the tip of the fixed shaft and a magnet on the inner surface of the top wall of the case so that they repel each other, and a rotating body that floats due to this repulsive force and is rotated by the drive source. An air magnetic bearing type optical deflector characterized in that the motor system of the rotating body is an inner rotor type.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP62092048A JP2637096B2 (en) | 1987-04-16 | 1987-04-16 | Air magnetic bearing type optical deflector |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP62092048A JP2637096B2 (en) | 1987-04-16 | 1987-04-16 | Air magnetic bearing type optical deflector |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS63259510A true JPS63259510A (en) | 1988-10-26 |
JP2637096B2 JP2637096B2 (en) | 1997-08-06 |
Family
ID=14043631
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP62092048A Expired - Lifetime JP2637096B2 (en) | 1987-04-16 | 1987-04-16 | Air magnetic bearing type optical deflector |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2637096B2 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02119217U (en) * | 1989-02-16 | 1990-09-26 | ||
JPH07167731A (en) * | 1994-10-11 | 1995-07-04 | Ricoh Co Ltd | Method for adjusting balance of hollow rotary body |
US5710470A (en) * | 1991-04-04 | 1998-01-20 | Ebara Corporation | Hydrodynamic bearing assembly |
US6188503B1 (en) | 1998-12-18 | 2001-02-13 | Fuji Xerox Co., Ltd. | Optical deflector and optical scanner |
JP2007139185A (en) * | 2005-10-17 | 2007-06-07 | Nippon Densan Corp | Bearing unit and electric motor including the bearing unit |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS63137560U (en) * | 1987-02-25 | 1988-09-09 |
-
1987
- 1987-04-16 JP JP62092048A patent/JP2637096B2/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS63137560U (en) * | 1987-02-25 | 1988-09-09 |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02119217U (en) * | 1989-02-16 | 1990-09-26 | ||
US5710470A (en) * | 1991-04-04 | 1998-01-20 | Ebara Corporation | Hydrodynamic bearing assembly |
JPH07167731A (en) * | 1994-10-11 | 1995-07-04 | Ricoh Co Ltd | Method for adjusting balance of hollow rotary body |
US6188503B1 (en) | 1998-12-18 | 2001-02-13 | Fuji Xerox Co., Ltd. | Optical deflector and optical scanner |
JP2007139185A (en) * | 2005-10-17 | 2007-06-07 | Nippon Densan Corp | Bearing unit and electric motor including the bearing unit |
Also Published As
Publication number | Publication date |
---|---|
JP2637096B2 (en) | 1997-08-06 |
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