JP2000192959A - Air spindle - Google Patents

Air spindle

Info

Publication number
JP2000192959A
JP2000192959A JP10370173A JP37017398A JP2000192959A JP 2000192959 A JP2000192959 A JP 2000192959A JP 10370173 A JP10370173 A JP 10370173A JP 37017398 A JP37017398 A JP 37017398A JP 2000192959 A JP2000192959 A JP 2000192959A
Authority
JP
Japan
Prior art keywords
bearing
axial
axial bearing
air
air supply
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.)
Withdrawn
Application number
JP10370173A
Other languages
Japanese (ja)
Inventor
Shizuka Yamazaki
静 山▲崎▼
Takashi Haraguchi
隆 原口
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.)
NTN Corp
Original Assignee
NTN Corp
NTN Toyo Bearing 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 NTN Corp, NTN Toyo Bearing Co Ltd filed Critical NTN Corp
Priority to JP10370173A priority Critical patent/JP2000192959A/en
Publication of JP2000192959A publication Critical patent/JP2000192959A/en
Withdrawn legal-status Critical Current

Links

Abstract

PROBLEM TO BE SOLVED: To provide a large air spindle by providing an air spindle having the constitution capable of relieving dimensional accuracy of respective parts. SOLUTION: In this air spindle, for example, a main spindle 10 and a thrust plate 30 are joined at an almost right angle in an angle freely displaceable state, and since an installing angle of the main spindle and the thrust plate is automatically corrected, accuracy of the installing angle of the main spindle and the thrust plate can be relieved. In the air spindle having an axial bearing 50 arranged in a housing 60 in an angle freely displaceable state in the shaft direction of an axial bearing surface, since a shaft directional angle of the axial bearing surface is automatically corrected, plane accuracy of a thrust member and installing accuracy of a rotary shaft member of the thrust member can be relieved.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、エアスピンドル装
置に関するものであり、エアスピンドル装置の大型化に
対応するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an air spindle device, and corresponds to an increase in the size of an air spindle device.

【0002】[0002]

【従来の技術】図7は従来のエアスピンドルの一般的な
構造を示す。
2. Description of the Related Art FIG. 7 shows a general structure of a conventional air spindle.

【0003】このエアスピンドルは、主軸1と、主軸1
の両端に直角に装着されたスラスト板2と、主軸1の外
周面に対向する軸受スリーブ3と、スラスト板2の内側
面に対向するアキシャル軸受部材4と、軸受スリーブ3
とアキシャル軸受部材4とを固定するハウジング5とを
有する。
The air spindle comprises a main shaft 1 and a main shaft 1
A thrust plate 2 mounted at right angles to both ends of the thrust plate, a bearing sleeve 3 facing the outer peripheral surface of the main shaft 1, an axial bearing member 4 facing the inner surface of the thrust plate 2, and a bearing sleeve 3
And a housing 5 for fixing the axial bearing member 4 to the housing.

【0004】軸受スリーブ3は、内径面に主軸の外周面
と微小隙間をもって対向するラジアル軸受面3aが形成
され、ラジアル軸受面3aに開口する複数の給気ノズル
3bを有する。アキシャル軸受部材4は、スラスト板2
と微小隙間をもって対向するアキシャル軸受面4aが形
成され、アキシャル軸受面4aに開口する複数の給気ノ
ズル4bを有する。ハウジング5は、内部に軸受スリー
ブ3及びアキシャル軸受部材4の各給気ノズル(3b,
4b)と連通する給気通路5aが形成されており、給気
通路5aの外側の開口部に給気コネクタ5bが取付けら
れている。
[0004] The bearing sleeve 3 has a radial bearing surface 3a facing the outer peripheral surface of the main shaft with a small gap on the inner diameter surface, and has a plurality of air supply nozzles 3b opened to the radial bearing surface 3a. The axial bearing member 4 includes the thrust plate 2
An axial bearing surface 4a is formed to face with a minute gap, and has a plurality of air supply nozzles 4b opened to the axial bearing surface 4a. The housing 5 has inside each of the air supply nozzles (3 b, 3 b) of the bearing sleeve 3 and the axial bearing member 4.
An air supply passage 5a communicating with the air supply passage 4a is formed, and an air supply connector 5b is attached to an opening outside the air supply passage 5a.

【0005】このエアスピンドルは、給気コネクタ5b
から入った圧縮空気が給気通路5aを通り、給気ノズル
(3b,4b)から吹き出して空気軸受を形成する。
The air spindle is provided with an air supply connector 5b.
Compressed air that has entered through the air supply passage 5a and blows out from the air supply nozzles (3b, 4b) to form an air bearing.

【0006】[0006]

【発明が解決しようとする課題】エアスピンドルの軸受
隙間は数μmの為、各部材の単品精度寸法(例えば、軸
受面の平面度、主軸とスラスト板との直角度等)も数μ
m以下に仕上げる必要である。ところで近年、エアスピ
ンドルの大型化の要求があるが、大型のエアスピンドル
を作成する場合に各部材の単品精度寸法を高精度に加工
するには、設備等の問題や、コスト面、長期間の加工を
要することから実現に限界がある。
Since the clearance between the bearings of the air spindle is several μm, the precision dimensions of each member (for example, the flatness of the bearing surface, the perpendicularity between the main shaft and the thrust plate) are also several μm.
m or less. By the way, in recent years, there has been a demand for a large air spindle, but when manufacturing a large air spindle, processing the single-piece precision dimensions of each member with high accuracy requires problems such as equipment, cost, and long term. There is a limit to the realization due to the need for processing.

【0007】そこで、本発明の目的とするところは、各
部品の寸法精度が緩和できる構成を有するエアスピンド
ルを提供し、大型のエアスピンドルを実現することであ
る。
An object of the present invention is to provide an air spindle having a configuration capable of relaxing the dimensional accuracy of each part, and to realize a large-sized air spindle.

【0008】[0008]

【課題を解決するための手段】本発明に係るエアスピン
ドルは、回転軸部材と、回転軸部材に角度が変位自在な
状態で略直角に装着されるスラスト部材と、回転軸部材
の外周面と微小なラジアル軸受隙間をもって対向するラ
ジアル軸受面と、ラジアル軸受面に開口形成された給気
ノズルとを有するラジアル軸受部材と、スラスト部材の
端面と微小なアキシャル軸受隙間をもって対向するアキ
シャル軸受面と、アキシャル軸受面に開口された給気ノ
ズルとを有するアキシャル軸受部材とを備え、ラジアル
軸受部材及びアキシャル軸受部材の各給気ノズルより各
軸受隙間に供給される圧縮空気の空気膜によって、回転
軸部材とスラスト部材とを各軸受面に対して非接触支持
するものである。
An air spindle according to the present invention comprises a rotating shaft member, a thrust member mounted at a substantially right angle to the rotating shaft member so that the angle is freely displaceable, and an outer peripheral surface of the rotating shaft member. A radial bearing surface having a small radial bearing gap, a radial bearing member having an air supply nozzle formed in the radial bearing surface, and an axial bearing surface facing the end surface of the thrust member with a small axial bearing gap; An axial bearing member having an air supply nozzle opened to the axial bearing surface, and a rotary shaft member formed by an air film of compressed air supplied to each bearing gap from each air supply nozzle of the radial bearing member and the axial bearing member. And the thrust member are supported in a non-contact manner with respect to each bearing surface.

【0009】また、回転軸部材と、回転軸部材に略直角
に装着されるスラスト部材と、回転軸部材を収容するハ
ウジングと、回転軸部材の外周面と微小なラジアル軸受
隙間をもって対向するラジアル軸受面と、ラジアル軸受
面に開口形成された給気ノズルとを有し、ハウジングに
配設されるラジアル軸受部材と、スラスト部材の端面と
微小なアキシャル軸受隙間をもって対向するアキシャル
軸受面と、アキシャル軸受面に開口された給気ノズルと
を有し、アキシャル軸受面の軸方向に対する角度が変位
自在な状態でハウジングに配設されるアキシャル軸受部
材とを備え、ラジアル軸受部材及びアキシャル軸受部材
の各給気ノズルより各軸受隙間に供給される圧縮空気の
空気膜によって、回転軸部材とスラスト部材とを各軸受
面に対して非接触支持するものである。
Also, a rotating shaft member, a thrust member mounted substantially at right angles to the rotating shaft member, a housing for accommodating the rotating shaft member, and a radial bearing facing the outer peripheral surface of the rotating shaft member with a small radial bearing gap. A radial bearing member disposed in the housing, an axial bearing surface facing the end surface of the thrust member with a small axial bearing gap, and an axial bearing. An axial bearing member disposed in the housing in a state where the angle of the axial bearing surface with respect to the axial direction is freely displaceable, and the supply of the radial bearing member and the axial bearing member is provided. The rotating shaft member and thrust member are not in contact with each bearing surface by the air film of compressed air supplied to each bearing gap from the air nozzle It is intended to equity.

【0010】また、回転軸部材とスラスト部材とが角度
が変位自在な状態で略直角に装着され、かつ、スラスト
部材の端面と微小なアキシャル軸受隙間をもって対向す
るアキシャル軸受面と、アキシャル軸受面に開口された
給気ノズルとを有し、アキシャル軸受面の軸方向に対す
る角度が変位自在な状態でハウジングのアキシャル軸受
領域に配設されるアキシャル軸受部材とを備えるもので
も良い。
[0010] Further, the rotary shaft member and the thrust member are mounted at a substantially right angle in a state where the angle is freely displaceable, and the axial bearing surface and the axial bearing surface facing each other with a small axial bearing gap from the end surface of the thrust member. And an axial bearing member provided in the axial bearing region of the housing in a state where the angle of the axial bearing surface with respect to the axial direction is displaceable.

【0011】例えば、回転軸部材とスラスト部材との装
着構造は、回転軸部材とスラスト部材とが蛇腹部材を介
して装着されているものとしても良い。
For example, the mounting structure of the rotating shaft member and the thrust member may be such that the rotating shaft member and the thrust member are mounted via a bellows member.

【0012】また、アキシャル軸受部材が、アキシャル
軸受面を構成する側の第一部材と、ハウジングに取付け
られる第二部材とで構成され、第一部材と第二部材とが
球面滑り接触で接合されているものとしても良い。
The axial bearing member comprises a first member on the side forming the axial bearing surface and a second member attached to the housing, and the first member and the second member are joined by spherical sliding contact. It may be good.

【0013】また、回転軸部材の軸受側端部と、回転軸
部材の軸受側端部が対向する軸受底部とに互いに引き合
う磁石を配設し、この磁石によって回転軸部材を軸方向
軸受側に引っ張るアキシャル反力を発生させ、このアキ
シャル反力とアキシャル軸受隙間に発生するアキシャル
軸受力との釣り合いによって、所要の軸受隙間を担保す
ることとしても良い。
Further, magnets are provided for attracting each other to a bearing-side end of the rotary shaft member and a bearing bottom of the rotary shaft member facing the bearing-side end, and the magnet is used to move the rotary shaft member toward the axial bearing. A necessary axial clearance may be secured by generating an axial reactive force to be pulled and balancing the axial reactive force with the axial bearing force generated in the axial bearing clearance.

【0014】[0014]

【発明の実施の形態】以下、本発明の一実施形態に係る
エアスピンドルについて図面に基づいて説明する。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An air spindle according to one embodiment of the present invention will be described below with reference to the drawings.

【0015】図1に示すように、本実施形態に係るエア
スピンドルは、主軸10と、蛇腹部材20と、スラスト
板30と、ラジアル軸受40と、アキシャル軸受50
と、ハウジング60とを主要構成要素とする。なお、説
明の便宜上、図1中ハウジング60に対してスラスト板
30が設定される側を上として、上下の方向を定義す
る。
As shown in FIG. 1, the air spindle according to this embodiment includes a main shaft 10, a bellows member 20, a thrust plate 30, a radial bearing 40, and an axial bearing 50.
And the housing 60 as main components. For convenience of description, the up and down direction is defined with the side on which the thrust plate 30 is set with respect to the housing 60 in FIG.

【0016】主軸10は、円筒状の部材で、上端部に蛇
腹部材20を嵌合する被嵌合部12が形成され、下端に
磁性金属材料で構成される金属板14がボルトで締結さ
れる。
The main shaft 10 is a cylindrical member having an upper end formed with a fitting portion 12 into which a bellows member 20 is fitted, and a lower end to which a metal plate 14 made of a magnetic metal material is fastened by bolts. .

【0017】図2に示すように、蛇腹部材20は、金属
製の管体で、外径面に周方向の溝部22が複数設けられ
ており、この溝部22の拡縮によって任意の角度に曲が
る構成を有する。蛇腹部材20の下端は、主軸10の被
嵌合部12に対応する嵌合部24が形成されている。ま
た、蛇腹部材20の上端は、スラスト板30を固定する
ためのボルト孔26が形成されている。
As shown in FIG. 2, the bellows member 20 is a metal tube having a plurality of circumferential grooves 22 provided on an outer diameter surface thereof. Having. A fitting portion 24 corresponding to the fitted portion 12 of the main shaft 10 is formed at a lower end of the bellows member 20. Further, a bolt hole 26 for fixing the thrust plate 30 is formed at the upper end of the bellows member 20.

【0018】スラスト板30は、円板状の部材で、蛇腹
部材20と中心を一致させた状態において、蛇腹部材2
0のボルト孔26に対応する位置にボルト孔32が形成
される。
The thrust plate 30 is a disc-shaped member, and the bellows member 2
A bolt hole 32 is formed at a position corresponding to the zero bolt hole 26.

【0019】ラジアル軸受40は、軸受スリーブ42と
配管スリーブ44とで構成される内外2重のスリーブ構
造を有する。軸受スリーブ42は配管スリーブ44の内
径面に嵌合固定される。軸受スリーブ42の内径面は、
主軸10の外径面10aと微小なラジアル隙間を介して
対向するラジアル軸受面42aが形成される。軸受スリ
ーブ42の外径面は、ラジアル軸受面42aに開口する
複数の給気ノズル42bが設けられる。配管スリーブ4
4は、軸受スリーブ42を嵌合固定した状態において軸
受スリーブ42の各給気ノズル42bと連通するよう
に、内部に給気通路44aが形成される。給気通路44
aは配管スリーブ44の下端に開口しており、この開口
部には給気コネクタ44bが取付られる。
The radial bearing 40 has a double inner and outer sleeve structure composed of a bearing sleeve 42 and a piping sleeve 44. The bearing sleeve 42 is fitted and fixed to the inner diameter surface of the piping sleeve 44. The inner diameter surface of the bearing sleeve 42 is
A radial bearing surface 42a is formed to face the outer diameter surface 10a of the main shaft 10 via a small radial gap. The outer diameter surface of the bearing sleeve 42 is provided with a plurality of air supply nozzles 42b that open to the radial bearing surface 42a. Piping sleeve 4
4 has an air supply passage 44a formed therein so as to communicate with each air supply nozzle 42b of the bearing sleeve 42 when the bearing sleeve 42 is fitted and fixed. Air supply passage 44
“a” is open at the lower end of the piping sleeve 44, and an air supply connector 44b is attached to this opening.

【0020】図3に示すように、アキシャル軸受50
は、アキシャル軸受板52と、スペーサ54と、取付軸
部56と、球面軸受58とを有し、図4に示すように、
スラスト板30の下面において、6つのアキシャル軸受
50が均等に配設されている。
As shown in FIG. 3, the axial bearing 50
Has an axial bearing plate 52, a spacer 54, a mounting shaft 56, and a spherical bearing 58, as shown in FIG.
On the lower surface of the thrust plate 30, six axial bearings 50 are evenly arranged.

【0021】アキシャル軸受板52は、円板状の部材で
上面にアキシャル軸受面52aが形成される。アキシャ
ル軸受板52の内部には、アキシャル軸受面52aに開
口する複数の給気ノズル52bと、各給気ノズル52b
と連通し下面の中心部に開口した給気通路52cとが形
成される。スペーサ54は、円板状の部材で、中心部に
給気孔54aが形成され、中心を一致させてアキシャル
軸受板52の下面に取付られる。取付軸部56は略円筒
形の箱状体で、下面は開口しており、上面は中央部に給
気孔が形成され、中心を一致させてスペーサ54の下面
に取付られる。取付軸部56の給気孔には箱状体の内部
側に給気コネクタ56aが取付られる。取付軸部56の
給気コネクタ56aは、取付軸部56の給気孔、スペー
サ54の給気孔54a、及び、スラスト軸受板52の給
気通路52cと連通する。球面軸受58は、互いに球面
滑り接触を行う内径部材58aと、外径部材58bとで
構成される。内径部材58aは取付軸部56の外径に対
応した内径を有して取付軸部56が嵌合固定される取付
穴58cが形成される。
The axial bearing plate 52 is a disk-shaped member and has an axial bearing surface 52a formed on the upper surface. Inside the axial bearing plate 52, a plurality of air supply nozzles 52b opening to the axial bearing surface 52a, and each air supply nozzle 52b
And an air supply passage 52c opened at the center of the lower surface. The spacer 54 is a disc-shaped member, and has an air supply hole 54a formed at the center thereof. The spacer 54 is attached to the lower surface of the axial bearing plate 52 so that the centers thereof are aligned. The mounting shaft portion 56 is a substantially cylindrical box-shaped body, the lower surface is open, the upper surface is formed with an air supply hole at the center, and is mounted on the lower surface of the spacer 54 so that the centers match. An air supply connector 56a is mounted in the air supply hole of the mounting shaft portion 56 inside the box. The air supply connector 56a of the mounting shaft 56 communicates with the air supply hole of the mounting shaft 56, the air supply hole 54a of the spacer 54, and the air supply passage 52c of the thrust bearing plate 52. The spherical bearing 58 includes an inner diameter member 58a and an outer diameter member 58b that make spherical sliding contact with each other. The inner diameter member 58a has an inner diameter corresponding to the outer diameter of the mounting shaft portion 56, and has a mounting hole 58c in which the mounting shaft portion 56 is fitted and fixed.

【0022】ハウジング60は、円形の部材で、ラジア
ル軸受取付部62と、アキシャル軸受取付部64とを有
する。ラジアル軸受取付部62は、ハウジング60の中
心部において軸方向略円形に中抜き形成される。ラジア
ル軸受取付部62は、上端部に肩部62aが形成され、
下端部に下部支持板66が取付られる。下部支持板66
は、円板状の部材で、中央部に磁石66aが配設され、
また、ラジアル軸受40の配管スリーブ44に設けられ
る給気コネクタ44bに対応する位置に給気ホース(図
示省略)を挿入するための挿入孔66bが形成される。
アキシャル軸受取付部64は、ハウジング60の中心部
の周囲に周方向6個所に、軸方向略円形に中抜き形成さ
れる。アキシャル軸受取付部64の上端は、アキシャル
軸受50の球面軸受58の外径部材58bに対応する肩
部64aが形成される。
The housing 60 is a circular member and has a radial bearing mounting portion 62 and an axial bearing mounting portion 64. The radial bearing mounting part 62 is formed in the center of the housing 60 so as to be hollow in a substantially circular shape in the axial direction. The radial bearing mounting portion 62 has a shoulder portion 62a formed at an upper end portion,
A lower support plate 66 is attached to the lower end. Lower support plate 66
Is a disk-shaped member, in which a magnet 66a is disposed in the center,
An insertion hole 66b for inserting an air supply hose (not shown) is formed at a position corresponding to the air supply connector 44b provided on the piping sleeve 44 of the radial bearing 40.
The axial bearing mounting portions 64 are formed at six locations in the circumferential direction around the center of the housing 60 so as to be hollowed out in a substantially circular shape in the axial direction. A shoulder 64 a corresponding to the outer diameter member 58 b of the spherical bearing 58 of the axial bearing 50 is formed at the upper end of the axial bearing mounting portion 64.

【0023】このエアスピンドルは、以下のように組み
立てられる。
This air spindle is assembled as follows.

【0024】ラジアル軸受40は、ハウジング60のラ
ジアル軸受取付部62の肩部62aに装着されボルト締
結によって取付られる。アキシャル軸受50は、ハウジ
ング60のアキシャル軸受取付部64の肩部64aに球
面軸受58の外径部材58bが嵌合され、抜け止めによ
って固定される。主軸10は、ラジアル軸受40のラジ
アル軸受面42aに所定のラジアル軸受隙間を介して配
設される。蛇腹部材20は、主軸10の上端に嵌合固定
される。スラスト板30は、蛇腹部材20と中心を一致
させた状態でボルト締結される。なお、このときスラス
ト板30の下面においてアキシャル軸受隙間を均一にす
るため、周方向に6枚設定される各アキシャル軸受50
の上面が同一平面を構成し得るように、各アキシャル軸
受50のスペーサ54の厚さを調整する。
The radial bearing 40 is mounted on a shoulder 62a of a radial bearing mounting portion 62 of the housing 60 and is mounted by bolting. In the axial bearing 50, the outer diameter member 58b of the spherical bearing 58 is fitted to the shoulder 64a of the axial bearing mounting portion 64 of the housing 60, and is fixed by retaining. The main shaft 10 is disposed on a radial bearing surface 42a of the radial bearing 40 with a predetermined radial bearing gap. The bellows member 20 is fitted and fixed to the upper end of the main shaft 10. The thrust plate 30 is bolted with the bellows member 20 centered. At this time, in order to make the axial bearing gap uniform on the lower surface of the thrust plate 30, six axial bearings 50 set in the circumferential direction are provided.
The thickness of the spacer 54 of each axial bearing 50 is adjusted so that the upper surfaces of the axial bearings 50 can form the same plane.

【0025】ラジアル軸受40には、ハウジング60の
下面に形成される挿入孔66bより給気ホース(図示省
略)を挿入し、給気コネクタ44bに圧縮空気が送られ
る。圧縮空気は、給気コネクタ44bより給気通路44
aを通って、ラジアル軸受面42aに開口する給気ノズ
ル42bより吹き出て、ラジアル軸受隙間に空気膜を形
成し、主軸10を非接触支持する。
An air supply hose (not shown) is inserted into the radial bearing 40 through an insertion hole 66b formed on the lower surface of the housing 60, and compressed air is sent to the air supply connector 44b. The compressed air is supplied from the air supply connector 44b to the air supply passage 44.
a through the air supply nozzle 42b opening in the radial bearing surface 42a to form an air film in the radial bearing gap, thereby supporting the main shaft 10 in a non-contact manner.

【0026】また、アキシャル軸受50には、ハウジン
グ60のアキシャル軸受取付部64の下面より給気ホー
ス(図示省略)が挿入され給気コネクタ56bに圧縮空
気が送られる。圧縮空気は、給気コネクタ56bより給
気孔54a及び給気通路52cを通って、アキシャル軸
受面52aに開口する給気ノズル52bより吹き出て、
アキシャル軸受隙間に空気膜を形成し、スラスト板30
を非接触支持する。
An air supply hose (not shown) is inserted into the axial bearing 50 from the lower surface of the axial bearing mounting portion 64 of the housing 60, and compressed air is sent to the air supply connector 56b. The compressed air passes through the air supply hole 54a and the air supply passage 52c from the air supply connector 56b, and blows out from the air supply nozzle 52b opened on the axial bearing surface 52a.
An air film is formed in the axial bearing gap, and the thrust plate 30 is formed.
In a non-contact manner.

【0027】このエアスピンドルは、ラジアル軸受40
のラジアル軸受面42aと、主軸10の外径面10aと
の間にラジアル軸受隙間が形成され、アキシャル軸受5
0のアキシャル軸受面52aと、スラスト板30の下面
30aとの間にアキシャル軸受隙間が形成される。この
ため、ラジアル軸受40のラジアル軸受面42a、主軸
10の外径面10a、アキシャル軸受50のアキシャル
軸受面52a、及び、スラスト板30の下面30aは寸
法精度を厳しく管理する必要がある。
This air spindle has a radial bearing 40
A radial bearing gap is formed between the radial bearing surface 42 a of the main shaft 10 and the outer diameter surface 10 a of the main shaft 10.
An axial bearing gap is formed between the zero axial bearing surface 52a and the lower surface 30a of the thrust plate 30. Therefore, it is necessary to strictly control the dimensional accuracy of the radial bearing surface 42a of the radial bearing 40, the outer diameter surface 10a of the main shaft 10, the axial bearing surface 52a of the axial bearing 50, and the lower surface 30a of the thrust plate 30.

【0028】しかし、このエアスピンドルは、蛇腹部材
20が任意に曲がることによって、主軸10とスラスト
板30との装着角度が変位自在な状態であり、ラジアル
軸受隙間とアキシャル軸受隙間の空気膜より力を受け、
主軸10とスラスト板30との角度が自動的に修正され
て、所要のラジアル軸受隙間が保持されるので、主軸1
0とスラスト板30との装着角度の精度を緩和できる。
However, this air spindle is in a state in which the mounting angle between the main shaft 10 and the thrust plate 30 is freely displaceable by the bending of the bellows member 20 arbitrarily, so that the air film in the radial bearing gap and the axial bearing gap is more powerful. Receiving
Since the angle between the main shaft 10 and the thrust plate 30 is automatically corrected to maintain a required radial bearing clearance, the main shaft 1
The accuracy of the mounting angle between 0 and the thrust plate 30 can be relaxed.

【0029】また、各アキシャル軸受50は、球面軸受
58を介してハウジング60に取付けられているため、
アキシャル軸受面52aの軸方向角度が変位自在な状態
であり、ラジアル軸受隙間とアキシャル軸受隙間の空気
膜より力を受け、アキシャル軸受面52aの軸方向角が
自動的に修正され、スラスト板30の下面との間で所要
のアキシャル軸受隙間が担保されるので、スラスト板3
0の平面精度やスラスト板30と主軸10との装着角度
の精度を緩和できる。
Since each axial bearing 50 is mounted on the housing 60 via the spherical bearing 58,
The axial angle of the axial bearing surface 52a is freely displaceable. The axial bearing angle of the axial bearing surface 52a is automatically corrected by receiving a force from the air film in the radial bearing gap and the axial bearing gap. Since a required axial bearing clearance is secured between the thrust plate 3 and the lower surface.
The flatness of zero and the accuracy of the mounting angle between the thrust plate 30 and the spindle 10 can be reduced.

【0030】また、このタイプのエアスピンドルは、軸
方向において主軸10とスラスト板30の自重と、アキ
シャル軸受隙間に発生するアキシャル軸受力とを釣り合
わせて所要のアキシャル軸受隙間を設定することもでき
る。しかし、主軸10とスラスト板の自重と、アキシャ
ル軸受力とのバランスが悪い場合はこれを補正する必要
がある。また、強制的に軸方向の釣り合いを担保した方
が、エアスピンドルの動作が安定する。そこで、この実
施形態のエアスピンドルは、主軸10の金属板14と、
主軸10の金属板14が対向するハウジング60の下部
支持板66の磁石66aとによって、互いに引き合い主
軸を軸方向下側に引っ張るアキシャル反力を発生させ、
このアキシャル反力とアキシャル軸受隙間に発生するア
キシャル軸受力とを釣り合わせることによって、より安
定した軸受隙間を担保することとした。
In this type of air spindle, the required axial bearing gap can be set by balancing the own weight of the main shaft 10 and the thrust plate 30 in the axial direction with the axial bearing force generated in the axial bearing gap. . However, if the balance between the weight of the main shaft 10 and the thrust plate and the axial bearing force is poor, it is necessary to correct this. In addition, the operation of the air spindle is more stable when the balance in the axial direction is secured. Therefore, the air spindle of this embodiment includes a metal plate 14 of the main shaft 10 and
The metal plate 14 of the main shaft 10 and the magnet 66a of the lower support plate 66 of the housing 60 facing each other generate an axial reaction force that attracts each other and pulls the main shaft downward in the axial direction.
By balancing the axial reaction force and the axial bearing force generated in the axial bearing gap, a more stable bearing gap is secured.

【0031】このように、このエアスピンドルは、スラ
スト板の平面精度や主軸とスラスト板との装着角度に生
じ得る多少の寸法誤差を許容できるので、低コストな大
型の空気軸受を実現することができる。
As described above, this air spindle can tolerate a slight dimensional error that may occur in the plane accuracy of the thrust plate and the mounting angle between the main shaft and the thrust plate, so that a low-cost large air bearing can be realized. it can.

【0032】以上、本発明に係るエアスピンドルの一実
施形態について説明したが、本発明に係るエアスピンド
ルは、係る実施形態に限定されず種々の変更が可能であ
る。
The embodiment of the air spindle according to the present invention has been described above. However, the air spindle according to the present invention is not limited to the embodiment and can be variously modified.

【0033】例えば、エアスピンドルは、主軸とスラス
ト板との装着角度のみ変位自在な構成とし、所要の軸受
隙間を担保するものとしても良い。また、アキシャル軸
受の軸方向角度のみ変位自在な構成とし、所要の軸受隙
間を担保するものとしても良い。
For example, the air spindle may be configured so that only the mounting angle between the main shaft and the thrust plate can be displaced, and a required bearing clearance is ensured. Further, the axial bearing of the axial bearing may be configured to be displaceable only in the axial direction, and a required bearing clearance may be secured.

【0034】また、アキシャル軸受は、図5に示す構成
のものでも良い。
The axial bearing may have the structure shown in FIG.

【0035】このアキシャル軸受70は、アキシャル軸
受板72と、取付軸部材74と、スペーサ76とを有す
る。アキシャル軸受板72は、円板状の部材で、上面に
アキシャル軸受面72aが形成され、内部にアキシャル
軸受面72aに開口する複数の給気ノズル72bと、各
給気ノズル72bと連通し、アキシャル軸受板72の下
面中央部に開口する給気通路72cとを有する。アキシ
ャル軸受板72の下面は、中心部に球面状の窪み72d
が形成されている。
The axial bearing 70 has an axial bearing plate 72, a mounting shaft member 74, and a spacer 76. The axial bearing plate 72 is a disc-shaped member, and has an axial bearing surface 72a formed on the upper surface. The axial bearing plate 72 communicates with the plurality of air supply nozzles 72b opening inside the axial bearing surface 72a and the air supply nozzles 72b. An air supply passage 72c is provided at the center of the lower surface of the bearing plate 72. The lower surface of the axial bearing plate 72 has a spherical recess 72d at the center.
Are formed.

【0036】取付軸部材74は、略円形の箱状体で、下
面が開口しており、上面はアキシャル軸受板72下面の
球面に対応した球面形状74aを有し、その中心部に給
気孔74bが形成され、この給気孔74bの下端開口部
には給気コネクタ74cが取付られる。また、取付軸部
材74の周側上部に半径方向に突出した鍔部74dを設
け、鍔部74dにボルト孔を形成する。
The mounting shaft member 74 is a substantially circular box-like body having an open lower surface, an upper surface having a spherical shape 74a corresponding to the spherical surface of the lower surface of the axial bearing plate 72, and an air supply hole 74b at the center thereof. The air supply connector 74c is attached to the lower end opening of the air supply hole 74b. In addition, a flange 74d protruding in the radial direction is provided on the upper part on the peripheral side of the mounting shaft member 74, and a bolt hole is formed in the flange 74d.

【0037】スペーサ76は、取付軸部材74の外周面
に挿入可能なリング状の板材で、アキシャル軸受板72
の取付高さを調整するものである。
The spacer 76 is a ring-shaped plate member that can be inserted into the outer peripheral surface of the mounting shaft member 74, and includes an axial bearing plate 72.
Is to adjust the mounting height.

【0038】このアキシャル軸受70は、ハウジング6
0' のアキシャル軸受取付部64'に、スペーサ76を
介して取付軸部材74をボルト(図示省略)で締結し、
取付軸部材74の球面状の上面にアキシャル軸受板72
を載置したものである。このとき、各アキシャル軸受板
72の上面が同一平面を構成し得るように、各スペーサ
76の厚さを調整する。このアキシャル軸受70は、ア
キシャル軸受板72の下面と取付軸部材74の上面とが
球面滑り接触を行うことによって、アキシャル軸受面7
2aの軸方向角度が変位自在な状態であり、上述のアキ
シャル軸受と同様にラジアル軸受隙間とアキシャル軸受
隙間の空気膜より力を受け、アキシャル軸受面52aの
軸方向角が自動的に修正されるので、スラスト板の平面
精度や主軸とスラスト板との装着角度の精度を緩和でき
る。
The axial bearing 70 is provided in the housing 6
The mounting shaft member 74 is fastened to the axial bearing mounting portion 64 ′ of 0 ′ via a spacer 76 with a bolt (not shown),
An axial bearing plate 72 is provided on the spherical upper surface of the mounting shaft member 74.
Is placed. At this time, the thickness of each spacer 76 is adjusted so that the upper surface of each axial bearing plate 72 can form the same plane. The axial bearing 70 has an axial bearing surface 7 by making a spherical sliding contact between the lower surface of the axial bearing plate 72 and the upper surface of the mounting shaft member 74.
The axial angle of 2a is freely displaceable. Like the above-described axial bearing, the axial angle of the axial bearing surface 52a is automatically corrected by receiving the force from the radial bearing gap and the air film in the axial bearing gap. Therefore, the accuracy of the plane of the thrust plate and the accuracy of the mounting angle between the main shaft and the thrust plate can be reduced.

【0039】また、主軸とスラスト板との接合部は、蛇
腹部材に換えて図6に示す接合構造としても良い。
The joint between the main shaft and the thrust plate may have a joint structure shown in FIG. 6 instead of the bellows member.

【0040】この接合構造は、主軸10' 上端に周方向
の複数箇所にポケット孔82を設け、ボルト孔84を一
個所設ける。そして、ポケット孔82に弾性体86と鋼
球88とを入れる。このとき鋼球88は、主軸10' の
上端より少し突出させる。主軸10' とスラスト板3
0' とをボルトで締結する。この際、弾性体86の弾性
変形によって、主軸10' とスラスト板30' との装着
角度は変位自在な状態であり、ラジアル軸受隙間とアキ
シャル軸受隙間の空気膜より力を受け、主軸10' とス
ラスト板30' との装着角度が自動的に修正されるの
で、上述の蛇腹部材と同様、主軸10' とスラスト板3
0' との装着角度の精度を緩和できる。
In this joint structure, pocket holes 82 are provided at a plurality of positions in the circumferential direction at the upper end of the main shaft 10 ', and one bolt hole 84 is provided. Then, an elastic body 86 and a steel ball 88 are put into the pocket hole 82. At this time, the steel ball 88 slightly protrudes from the upper end of the main shaft 10 '. Main shaft 10 'and thrust plate 3
0 'with bolts. At this time, due to the elastic deformation of the elastic body 86, the mounting angle between the main shaft 10 'and the thrust plate 30' is in a displaceable state, and receives a force from the air film in the radial bearing gap and the axial bearing gap, and the main shaft 10 ' Since the mounting angle with the thrust plate 30 'is automatically corrected, similarly to the above-mentioned bellows member, the main shaft 10' and the thrust plate 3 '
The accuracy of the mounting angle with 0 'can be relaxed.

【0041】また、本実施形態のエアスピンドルを用い
れば、大型のエアスピンドルを構成することができるの
で、例えば、図1に示すように、主軸10の外径面にロ
ータ16を設け、かつ、ラジアル軸受40の軸受スリー
ブ42にステータコイル46を設けることによって、大
型のモータ装置を実現することができる。
If the air spindle of the present embodiment is used, a large air spindle can be constructed. For example, as shown in FIG. 1, a rotor 16 is provided on the outer surface of the main shaft 10, and By providing the stator coil 46 on the bearing sleeve 42 of the radial bearing 40, a large-sized motor device can be realized.

【0042】[0042]

【発明の効果】本発明に係るエアスピンドルの内、回転
軸部材とスラスト部材との角度が変位自在な状態で略直
角に装着されたものは、回転軸部材とスラスト部材との
直角度が自動的に修正されて、所要の軸受隙間が保持さ
れるので、回転軸部材とスラスト部材との装着部の精度
を緩和できる。
The air spindle according to the present invention, which is mounted at a substantially right angle so that the angle between the rotating shaft member and the thrust member is freely displaceable, is such that the perpendicularity between the rotating shaft member and the thrust member is automatically adjusted. And the required bearing clearance is maintained, so that the accuracy of the mounting portion between the rotary shaft member and the thrust member can be reduced.

【0043】また、アキシャル軸受面の軸方向に対する
角度が変位自在な状態でハウジングのアキシャル軸受領
域に配設されるアキシャル軸受部材を備えるものは、ア
キシャル軸受面の軸方向角が自動的に修正されて、所要
の軸受隙間が確保されるので、スラスト部材の平面精度
やスラスト部材と回転軸部材との装着角度の精度を緩和
できる。
In the case where the axial bearing member is provided in the axial bearing region of the housing such that the angle of the axial bearing surface with respect to the axial direction is freely displaceable, the axial angle of the axial bearing surface is automatically corrected. As a result, the required bearing clearance is ensured, so that the planar accuracy of the thrust member and the accuracy of the mounting angle between the thrust member and the rotary shaft member can be reduced.

【0044】また、回転軸部材の軸受側端部と、回転軸
部材の軸受側端部が対向する軸受底部とに互いに引き合
う磁石を配設したものは、この磁石によって回転軸部材
を軸方向軸受側に引っ張るアキシャル反力を発生させる
ことができるので、このアキシャル反力とアキシャル軸
受隙間に発生するアキシャル軸受力とが釣り合うことに
よって、より安定した軸受隙間を担保することができ
る。
Further, in the case where magnets are attracted to each other at a bearing end of the rotating shaft member and a bearing bottom portion at which the bearing end of the rotating shaft member is opposed, the rotating shaft member is axially supported by the magnet. Since an axial reaction force pulling to the side can be generated, a more stable bearing gap can be secured by balancing the axial reaction force with the axial bearing force generated in the axial bearing gap.

【図面の簡単な説明】[Brief description of the drawings]

【図1】 本発明の一実施形態に係るエアスピンドルの
縦断面図。
FIG. 1 is a longitudinal sectional view of an air spindle according to an embodiment of the present invention.

【図2】 本発明の一実施形態に係るエアスピンドルの
蛇腹部材近傍の縦断面図。
FIG. 2 is a longitudinal sectional view of the vicinity of a bellows member of the air spindle according to the embodiment of the present invention.

【図3】 本発明の一実施形態に係るエアスピンドルの
アキシャル軸受の縦断面図。
FIG. 3 is a longitudinal sectional view of an axial bearing of the air spindle according to the embodiment of the present invention.

【図4】 本発明の一実施形態に係るエアスピンドルの
平面図。
FIG. 4 is a plan view of an air spindle according to one embodiment of the present invention.

【図5】 本発明の他の実施形態に係るエアスピンドル
のアキシャル軸受の縦断面図。
FIG. 5 is a longitudinal sectional view of an axial bearing of an air spindle according to another embodiment of the present invention.

【図6】 本発明の他の実施形態に係るエアスピンドル
の主軸とスラスト板の接合構造を示す縦断面図。
FIG. 6 is a longitudinal sectional view showing a joint structure between a main shaft of an air spindle and a thrust plate according to another embodiment of the present invention.

【図7】 従来のエアスピンドルの縦断面図。FIG. 7 is a longitudinal sectional view of a conventional air spindle.

【符号の説明】[Explanation of symbols]

10 主軸 14 金属板 20 蛇腹部材 30 スラスト部材 40 ラジアル軸受 50 アキシャル軸受 58 球面軸受 60 ハウジング 66a 磁石 DESCRIPTION OF SYMBOLS 10 Main shaft 14 Metal plate 20 Bellows member 30 Thrust member 40 Radial bearing 50 Axial bearing 58 Spherical bearing 60 Housing 66a Magnet

Claims (6)

【特許請求の範囲】[Claims] 【請求項1】回転軸部材と、前記回転軸部材に角度が変
位自在な状態で略直角に装着されるスラスト部材と、 前記回転軸部材の外周面と微小なラジアル軸受隙間をも
って対向するラジアル軸受面と、前記ラジアル軸受面に
開口形成された給気ノズルとを有するラジアル軸受部材
と、 前記スラスト部材の端面と微小なアキシャル軸受隙間を
もって対向するアキシャル軸受面と、前記アキシャル軸
受面に開口された給気ノズルとを有するアキシャル軸受
部材とを備え、 前記ラジアル軸受部材及びアキシャル軸受部材の各給気
ノズルより各軸受隙間に供給される圧縮空気の空気膜に
よって、前記回転軸部材とスラスト部材とを各軸受面に
対して非接触支持することを特徴とするエアスピンド
ル。
1. A rotary shaft member, a thrust member mounted to the rotary shaft member at a substantially right angle so that the angle is displaceable, and a radial bearing opposed to an outer peripheral surface of the rotary shaft member with a small radial bearing gap. Surface, a radial bearing member having an air supply nozzle formed in the radial bearing surface, an axial bearing surface facing the end surface of the thrust member with a small axial bearing gap, and an opening in the axial bearing surface. An axial bearing member having an air supply nozzle; and an air film of compressed air supplied to each bearing gap from each air supply nozzle of the radial bearing member and the axial bearing member. An air spindle characterized by being supported in a non-contact manner with respect to each bearing surface.
【請求項2】回転軸部材と、前記回転軸部材に略直角に
装着されるスラスト部材と、 前記回転軸部材を収容するハウジングと、 前記回転軸部材の外周面と微小なラジアル軸受隙間をも
って対向するラジアル軸受面と、前記ラジアル軸受面に
開口形成された給気ノズルとを有し、前記ハウジングに
配設されるラジアル軸受部材と、 前記スラスト部材の端面と微小なアキシャル軸受隙間を
もって対向するアキシャル軸受面と、前記アキシャル軸
受面に開口された給気ノズルとを有し、前記アキシャル
軸受面の軸方向に対する角度が変位自在な状態で前記ハ
ウジングに配設されるアキシャル軸受部材とを備え、 前記ラジアル軸受部材及びアキシャル軸受部材の各給気
ノズルより各軸受隙間に供給される圧縮空気の空気膜に
よって、前記回転軸部材とスラスト部材とを各軸受面に
対して非接触支持することを特徴とするエアスピンド
ル。
2. A rotary shaft member, a thrust member mounted substantially at a right angle to the rotary shaft member, a housing for accommodating the rotary shaft member, and a small radial bearing gap with an outer peripheral surface of the rotary shaft member. A radial bearing member having a radial bearing surface, and an air supply nozzle formed in the radial bearing surface, and a radial bearing member disposed in the housing, and an axial surface facing the end surface of the thrust member with a small axial bearing gap. An axial bearing member having a bearing surface and an air supply nozzle opened to the axial bearing surface, wherein the axial bearing member is disposed in the housing such that an angle of the axial bearing surface with respect to an axial direction is freely displaceable; The rotary shaft member is formed by an air film of compressed air supplied to each bearing gap from each air supply nozzle of the radial bearing member and the axial bearing member. An air spindle for supporting a bearing and a thrust member in a non-contact manner with respect to each bearing surface.
【請求項3】前記回転軸部材とスラスト部材とが角度が
変位自在な状態で略直角に装着されたことを特徴とする
請求項2記載のエアスピンドル。
3. The air spindle according to claim 2, wherein the rotating shaft member and the thrust member are mounted at a substantially right angle so that the angle is freely displaceable.
【請求項4】前記回転軸部材とスラスト部材とが蛇腹部
材を介して装着されていることを特徴とする請求項1記
載のエアスピンドル。
4. The air spindle according to claim 1, wherein the rotating shaft member and the thrust member are mounted via a bellows member.
【請求項5】前記アキシャル軸受部材が、アキシャル軸
受面を構成する側の第一部材と、ハウジングに取付けら
れる第二部材とで構成され、第一部材と第二部材とが球
面滑り接触で接合されていることを特徴とする請求項2
記載のエアスピンドル。
5. The axial bearing member comprises a first member on an axial bearing surface side and a second member attached to a housing, and the first member and the second member are joined by spherical sliding contact. 3. The method according to claim 2, wherein
The described air spindle.
【請求項6】前記回転軸部材の軸受側端部と、回転軸部
材の軸受側端部が対向する軸受底部とに互いに引き合う
磁石を配設し、この磁石によって回転軸部材を軸方向軸
受側に引っ張るアキシャル反力を発生させ、このアキシ
ャル反力とアキシャル軸受隙間に発生するアキシャル軸
受力との釣り合いによって、所要の軸受隙間を担保する
ことを特徴とする請求項1乃至3記載のエアスピンド
ル。
6. A magnet which attracts each other to a bearing-side end of the rotary shaft member and a bearing bottom of the rotary shaft member facing the bearing-side end. The air spindle according to any one of claims 1 to 3, wherein an axial reaction force is generated, and a required bearing clearance is ensured by balancing the axial reaction force and the axial bearing force generated in the axial bearing clearance.
JP10370173A 1998-12-25 1998-12-25 Air spindle Withdrawn JP2000192959A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10370173A JP2000192959A (en) 1998-12-25 1998-12-25 Air spindle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10370173A JP2000192959A (en) 1998-12-25 1998-12-25 Air spindle

Publications (1)

Publication Number Publication Date
JP2000192959A true JP2000192959A (en) 2000-07-11

Family

ID=18496250

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10370173A Withdrawn JP2000192959A (en) 1998-12-25 1998-12-25 Air spindle

Country Status (1)

Country Link
JP (1) JP2000192959A (en)

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