TW201420907A - Gas-static bearing unit - Google Patents

Gas-static bearing unit Download PDF

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Publication number
TW201420907A
TW201420907A TW102123628A TW102123628A TW201420907A TW 201420907 A TW201420907 A TW 201420907A TW 102123628 A TW102123628 A TW 102123628A TW 102123628 A TW102123628 A TW 102123628A TW 201420907 A TW201420907 A TW 201420907A
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Taiwan
Prior art keywords
bearing
shaft
axial
radial bearing
radial
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TW102123628A
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Chinese (zh)
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TWI622715B (en
Inventor
Satoshi Ueda
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Oiles Industry Co Ltd
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Publication of TWI622715B publication Critical patent/TWI622715B/en

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    • 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
    • F16C32/06Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings
    • F16C32/0603Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings supported by a gas cushion, e.g. an air cushion
    • F16C32/0614Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings supported by a gas cushion, e.g. an air cushion the gas being supplied under pressure, e.g. aerostatic bearings
    • F16C32/0618Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings supported by a gas cushion, e.g. an air cushion the gas being supplied under pressure, e.g. aerostatic bearings via porous material
    • 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
    • F16C32/06Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings
    • F16C32/0603Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings supported by a gas cushion, e.g. an air cushion
    • F16C32/0614Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings supported by a gas cushion, e.g. an air cushion the gas being supplied under pressure, e.g. aerostatic bearings
    • F16C32/0622Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings supported by a gas cushion, e.g. an air cushion the gas being supplied under pressure, e.g. aerostatic bearings via nozzles, restrictors
    • 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
    • F16C32/06Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings
    • F16C32/0681Construction or mounting aspects of hydrostatic bearings, for exclusively rotary movement, related to the direction of load
    • F16C32/0685Construction or mounting aspects of hydrostatic bearings, for exclusively rotary movement, related to the direction of load for radial load only
    • 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
    • F16C32/06Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings
    • F16C32/0681Construction or mounting aspects of hydrostatic bearings, for exclusively rotary movement, related to the direction of load
    • F16C32/0696Construction or mounting aspects of hydrostatic bearings, for exclusively rotary movement, related to the direction of load for both radial and axial load

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Dispersion Chemistry (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)

Abstract

Provided is a compact, gas-static bearing unit for more stably supporting a rotating body without contact using a simple structure, the rotating body rotating at high speed. The opposite ends (113, 12) of an air shaft unit (1) for supporting a pulley (2) without contact are affixed to two shaft holders (3A, 3B). Gas (f) is supplied from the radial bearing surface (1121) of the air shaft unit (1) to the radial bearing gap (60) between the radial bearing surface (1121) and the inner peripheral surface (221) of the pulley (2) to form a gas film within the radial bearing gap (60), and the gas (f) is discharged from the radial bearing gap (60) to the thrust bearing gaps (61a, 61b) between the thrust bearing surfaces (1132, 121) of the air shaft unit (1) and the boss end surfaces (241A, 241B) of the pulley (2), the thrust bearing gaps (61a, 61b) connecting to the radial bearing gap (60). A gas film is also formed within the thrust bearing gaps (61a, 61b) utilizing the discharge gas (f1).

Description

靜壓氣體軸承單元 Hydrostatic gas bearing unit

本發明係關於一種構造簡單且能夠更穩定地非接觸支撐高速旋轉之滑輪(pulley)等零件的兩端支撐式(both end support type)靜壓氣體軸承單元之構造。 The present invention relates to a construction of a both end support type static pressure gas bearing unit which is simple in construction and capable of more stably supporting a high-speed rotating pulley such as a pulley.

在專利文獻1中,係有記載一種以非接觸方式支撐旋轉軸的空氣軸承單元(air bearing unit)(靜壓氣體軸承裝置)。 Patent Document 1 describes an air bearing unit (static gas bearing device) that supports a rotating shaft in a non-contact manner.

在該空氣軸承單元中,係在可供軸(shaft)(旋轉軸)插入之圓筒形的外殼(housing)之內周的兩端側,分別設置有一個分別以個別之軸承面(軸向(thrust)軸承面、徑向(radial)軸承面)來承受軸之軸向荷重及徑向荷重的多孔質引伸模(porous drawing die)(多孔質石墨(graphite)等之多孔質體)之空氣軸承(靜壓空氣軸承)。在此,徑向軸承面,係與軸之外周面相對向,並在與該外周面之間形成徑向軸承間隙,而軸向軸承面,係與形成於軸之外周的凸緣(flange)相對向,並在與該凸緣之間形成軸向軸承間隙。 In the air bearing unit, one end side of the inner circumference of a cylindrical casing into which a shaft (rotation shaft) is inserted is provided with an individual bearing surface (axial direction) (thrust) bearing surface, radial bearing surface) to accommodate the axial load of the shaft and the radial load of the porous drawing die (porous body such as porous graphite) Bearing (static air bearing). Here, the radial bearing surface is opposed to the outer peripheral surface of the shaft and forms a radial bearing gap with the outer peripheral surface, and the axial bearing surface is formed with a flange formed on the outer circumference of the shaft. Opposite and forming an axial bearing gap between the flange.

在此,針對每一空氣軸承,在外殼之內周面 ,係隔著空氣軸承之徑向軸承面而在軸向軸承面之相反側(外殼之內周面的中央側)於圓周方向形成有排氣用槽,在該排氣用槽之槽底,係形成有貫通至外殼之外周面的排氣孔。又,在軸之外周面,係在空氣軸承之靠近軸向軸承面的位置於圓周方向形成有排氣用槽,而在軸之內部,係形成有連繫該排氣用槽和外殼之內周面的排氣用槽的排氣孔。 Here, for each air bearing, the inner circumference of the outer casing a gas groove is formed in the circumferential direction on the opposite side of the axial bearing surface (the center side of the inner circumferential surface of the outer casing) via the radial bearing surface of the air bearing, and the groove is formed in the groove bottom of the exhaust groove. A vent hole penetrating through the outer peripheral surface of the outer casing is formed. Further, on the outer circumferential surface of the shaft, an exhaust groove is formed in the circumferential direction at a position close to the axial bearing surface of the air bearing, and inside the shaft, a groove for connecting the exhaust and a casing are formed. The exhaust hole of the groove for the exhaust surface on the circumference.

在如此之構成中,供應至空氣軸承的空氣,係從空氣軸承之軸向軸承面及徑向軸承面分別噴出。從軸向軸承面噴出之空氣,係朝向凸緣之外周而流動於軸向軸承間隙內,且從軸向軸承間隙朝向外部釋放出。另一方面,從徑向軸承面噴出之空氣,係朝向靠近軸向軸承面的排氣用槽和軸向軸承面之相反側的排氣用槽,而流動於徑向軸承間隙內,並流入於上述的排氣用槽,且經由排氣孔而排出至外殼之外部。 In such a configuration, the air supplied to the air bearing is ejected from the axial bearing surface and the radial bearing surface of the air bearing, respectively. The air ejected from the axial bearing surface flows into the axial bearing gap toward the outer circumference of the flange, and is released from the axial bearing gap toward the outside. On the other hand, the air ejected from the radial bearing surface flows into the radial bearing gap toward the exhaust groove close to the axial bearing surface and the exhaust groove on the opposite side of the axial bearing surface. The exhaust groove described above is discharged to the outside of the casing through the exhaust hole.

(專利文獻1)日本特開2008-57696號公報 (Patent Document 1) Japanese Patent Laid-Open Publication No. 2008-57696

然而,專利文獻1所述的空氣軸承單元,係有必要針對每一空氣軸承,事先在靠近軸向軸承面之位置、和隔著徑向軸承面而在軸向軸承面之相反側的位置,分別形成用以排出供應至徑向軸承間隙之空氣的排氣用槽。又,有必要事先將用以將已流入於上述之排氣用槽的空氣 排出至外殼之外部的排氣孔,形成於外殼及軸之雙方。更且,在外殼之內周,係有必要事先個別地設置噴出壓縮空氣的軸向軸承面及徑向軸承面。因此,構造複雜化。 However, in the air bearing unit described in Patent Document 1, it is necessary for each air bearing to be placed at a position close to the axial bearing surface and at a position opposite to the axial bearing surface via the radial bearing surface. Exhaust grooves for discharging air supplied to the radial bearing gap are formed, respectively. Further, it is necessary to previously use the air to flow into the above-described exhaust groove. A vent hole that is discharged to the outside of the outer casing is formed on both the outer casing and the shaft. Further, it is necessary to separately provide an axial bearing surface and a radial bearing surface for discharging compressed air in the inner circumference of the outer casing. Therefore, the structure is complicated.

又,因軸側之排氣孔,係為了連繫軸之外周 面的排氣用槽和外殼之內周面的排氣用槽而沿著軸之軸心方向所形成,故而軸需要某種程度的厚度。因此,當軸重量化時,軸就有可能例如因自重而撓曲。因形成於外殼內周的空氣軸承(靜壓空氣軸承)的徑向軸承面與軸之外周面之間的徑向軸承間隙係非常狹窄,故而當軸發生撓曲時,軸和軸承就會接觸,而有無法穩定地保持軸的可能性。 Moreover, the vent hole on the shaft side is for the outer circumference of the shaft. Since the surface of the exhaust groove and the exhaust groove of the inner peripheral surface of the outer casing are formed along the axial direction of the shaft, the shaft needs a certain thickness. Therefore, when the shaft is weighted, it is possible for the shaft to flex, for example, due to its own weight. Since the radial bearing gap between the radial bearing surface of the air bearing (static air bearing) formed on the inner circumference of the outer casing and the outer circumferential surface of the shaft is very narrow, when the shaft is deflected, the shaft and the bearing are in contact. There is a possibility that the shaft cannot be stably maintained.

可是,當以空氣軸承來保持高速旋轉的滑輪 等之旋轉體時,有時在供氣時會發生自激振動(self-excited vibration)。當系統藉此共振時,就會妨礙到例如搬運物之穩定行走等。 However, when using air bearings to keep the pulley rotating at high speed When the body is rotated, self-excited vibration may occur during air supply. When the system is thereby resonated, it hinders, for example, stable walking of the article or the like.

本發明係有鑒於上述情事而開發完成者,其 目的在於提供一種構造簡單且更穩定地非接觸支撐高速旋轉之旋轉體的兩端支撐式靜壓氣體軸承單元之構造。 The present invention has been developed in view of the above circumstances, and It is an object of the invention to provide a construction of a two-end supported static pressure gas bearing unit that is simple in construction and more stable in non-contact support of a high-speed rotating rotating body.

為了解決上述課題,在本發明中,係使旋轉體插入於形成於該旋轉體之軸向的軸插入孔內,且將以非接觸式方式支撐該旋轉體的軸單元,利用從軸向兩側夾入旋轉體之軸插入孔的位置來加以固定。又,藉由從與旋轉體之軸插入孔內的內周面相對向之形成於軸單元(shaft unit)之外周面的徑向軸承面噴出的氣體,而在徑向軸承面與旋轉體之軸插入孔的內周面之間的徑向軸承間隙內形成氣體膜,且使該氣體,從徑向軸承間隙,排出至軸單元之軸向軸承面與旋轉體之各端面之間的徑向軸承間隙內。亦利用該被排出的氣體在軸向軸承間隙內形成氣體膜。 In order to solve the above problems, in the present invention, the rotating body is inserted into the shaft insertion hole formed in the axial direction of the rotating body, and the shaft unit that supports the rotating body in a non-contact manner is used. The side is clamped into the position of the shaft insertion hole of the rotating body to be fixed. Further, the shaft unit is formed by being opposed to the inner peripheral surface of the hole inserted into the hole from the shaft of the rotating body (shaft) a gas that is ejected from the radial bearing surface of the outer peripheral surface, and a gas film is formed in a radial bearing gap between the radial bearing surface and the inner peripheral surface of the shaft insertion hole of the rotating body, and the gas is made from the diameter The bearing clearance is discharged into the radial bearing gap between the axial bearing surface of the shaft unit and each end surface of the rotating body. The gas to be discharged is also used to form a gas film in the axial bearing gap.

例如,本發明係一種係藉由夾介存在於徑向軸承間隙和第一及第二軸向軸承間隙的氣體膜以非接觸方式支撐朝向繞軸心之方向旋轉的旋轉體之靜壓氣體軸承單元,其具備:軸單元,其係插入於貫通前述旋轉體之兩端面的軸插入孔內;以及軸保持手段,其係以前述旋轉體之軸插入孔的兩側之位置來保持前述軸單元,前述軸單元,係具有:徑向軸承面,其係對向於前述軸插入孔之內周面,並在與該內周面之間形成前述徑向軸承間隙,且對前述徑向軸承間隙噴出用以形成前述氣體膜的氣體;及第一軸向軸承面,其係與前述徑向軸承面相鄰,且對向於前述旋轉體之一方的端面,並在與該端面之間,形成與前述徑向軸承間隙之一方的端側連繫的前述第一軸向軸承間隙;以及第二軸向軸承面,其係與前述徑向軸承面相鄰,且對向於前述旋轉體之另一方的端面,並在與該端面之間,形成與前述徑向軸承間隙之另一方的端側連繫的前述第二軸 向軸承間隙,前述氣體,係朝向前述第一軸向軸承間隙及前述第二軸向軸承間隙流動於前述徑向軸承間隙內,並從該徑向軸承間隙分別排出至前述第一軸向軸承間隙及前述第二軸向軸承間隙,且在該第一軸向軸承間隙內及該第二軸向軸承間隙分別形成前述氣體膜。 For example, the present invention is a static pressure gas bearing that supports a rotating body that rotates in a direction around an axis by a gas film interposed between a radial bearing gap and first and second axial bearing gaps in a non-contact manner. The unit includes: a shaft unit that is inserted into a shaft insertion hole that penetrates both end faces of the rotating body; and a shaft holding means that holds the shaft unit at positions on both sides of the shaft insertion hole of the rotating body The shaft unit has a radial bearing surface that is opposite to an inner circumferential surface of the shaft insertion hole, and forms the aforementioned radial bearing clearance between the inner circumferential surface and the radial bearing clearance. Discharging a gas for forming the gas film; and a first axial bearing surface adjacent to the radial bearing surface and facing an end surface of one of the rotating bodies and formed between the end surface and the end surface a first axial bearing gap associated with one end side of the radial bearing gap; and a second axial bearing surface adjacent to the radial bearing surface and opposite to the rotating body One end face, In between the end surfaces, formed with the other of the radial bearing gap of the associated end of the second shaft To the bearing gap, the gas flows into the radial bearing gap toward the first axial bearing gap and the second axial bearing gap, and is discharged from the radial bearing gap to the first axial bearing gap And the second axial bearing gap, and the gas film is formed in the first axial bearing gap and the second axial bearing gap, respectively.

依據本發明,因其是利用於以下之目的:從徑向軸承間隙排出的壓縮氣體,在供應至形成於旋轉體之各端面與軸單元之軸向軸承面之間的軸向軸承間隙之後才被排氣,且在軸向軸承間隙形成氣體膜,該徑向軸承間隙係形成於旋轉體之軸插入孔的內周面、和與旋轉體之軸插入孔的內周面相對向之形成於軸單元之外周面的徑向軸承面之間,故而沒有必要另外設置用以排出來自徑向軸承間隙之壓縮氣體的溝槽及孔、或是將壓縮氣體噴出至軸向軸承間隙的軸向軸承面。又,因非接觸支撐旋轉體之軸單元兩端被固定,故而即便是在軸單元隨著旋轉體之尺寸而長條化的情況,仍可以抑制其撓曲,且可以防止旋轉體與軸單元之接觸。因此,可以實現一種構造簡單且能夠更穩定地非接觸支撐高速旋轉之旋轉體的兩端支撐式靜壓氣體軸承單元之構造。 According to the present invention, it is used for the purpose of compressing gas discharged from the radial bearing gap after being supplied to the axial bearing gap formed between the end faces of the rotating body and the axial bearing faces of the shaft unit. Is exhausted, and a gas film is formed in the axial bearing gap, and the radial bearing gap is formed on the inner circumferential surface of the shaft insertion hole of the rotating body and is formed opposite to the inner circumferential surface of the shaft insertion hole of the rotating body. Between the radial bearing faces of the outer peripheral surface of the shaft unit, it is not necessary to separately provide grooves and holes for discharging compressed gas from the radial bearing gap, or axial bearings for discharging compressed gas to the axial bearing gap. surface. Further, since both ends of the shaft unit of the non-contact supporting rotating body are fixed, even when the shaft unit is elongated with the size of the rotating body, the deflection can be suppressed, and the rotating body and the shaft unit can be prevented. Contact. Therefore, it is possible to realize a configuration of a two-end supported static pressure gas bearing unit which is simple in construction and can more stably support the rotating body which is rotated at a high speed without contact.

1‧‧‧氣壓軸單元 1‧‧‧Pneumatic shaft unit

2‧‧‧滑輪 2‧‧‧ pulley

3A、3B‧‧‧軸座 3A, 3B‧‧‧ shaft seat

4‧‧‧空氣軸承單元 4‧‧‧Air bearing unit

11‧‧‧氣壓軸 11‧‧‧Pneumatic shaft

12‧‧‧軸向板 12‧‧‧Axial plate

13‧‧‧螺帽 13‧‧‧ Nuts

21‧‧‧凸緣部 21‧‧‧Flange

22‧‧‧氣壓軸插入用孔 22‧‧‧Pneumatic shaft insertion hole

23‧‧‧輪轂之外周面 23‧‧·The outer circumference of the hub

24A、24B‧‧‧輪轂 24A, 24B‧‧ wheels

25A、25B‧‧‧滑輪之端面 End face of 25A, 25B‧‧‧ pulley

31‧‧‧軸固定孔 31‧‧‧Axis fixing hole

32‧‧‧上側塊體材料 32‧‧‧Upper block material

33‧‧‧下側塊體材料 33‧‧‧Lower block material

34‧‧‧螺栓 34‧‧‧Bolts

40‧‧‧聯結器 40‧‧‧Connector

41‧‧‧供氣管 41‧‧‧ gas supply pipe

111‧‧‧背墊金屬 111‧‧‧Back pad metal

112‧‧‧多孔質燒結層 112‧‧‧Porous sintered layer

113‧‧‧基底部 113‧‧‧ base

114‧‧‧徑向軸承部 114‧‧‧ Radial bearing department

115‧‧‧桿部 115‧‧‧ pole

116‧‧‧通氣路 116‧‧‧ Ventilation Road

117‧‧‧供氣口 117‧‧‧ gas supply port

118‧‧‧螺紋部 118‧‧‧Threading Department

121‧‧‧軸向板之端面(軸向軸承面) 121‧‧‧Axial plate end face (axial bearing surface)

122‧‧‧軸向板之端面 122‧‧‧End face of the axial plate

123‧‧‧軸插入用孔 123‧‧‧Axis insertion hole

221‧‧‧滑輪之內周面 221‧‧‧The inner circumference of the pulley

241A、241B‧‧‧輪轂之端面 End face of 241A, 241B‧‧

1121‧‧‧多孔質燒結層之外周面(徑向軸承面) 1121‧‧‧The outer surface of the porous sintered layer (radial bearing surface)

1131‧‧‧基底部之端面 1131‧‧‧End of the base

1132‧‧‧基底部之端面(段差面、軸向軸承面) 1132‧‧‧End face of the base (segment surface, axial bearing surface)

1141‧‧‧徑向軸承部之端面(段差面) 1141‧‧‧End face of radial bearing (segment surface)

1142‧‧‧徑向軸承部之外周面 1142‧‧‧Outer peripheral surface of radial bearing

1143‧‧‧環狀槽 1143‧‧‧ring groove

1144‧‧‧孔 1144‧‧ hole

1151‧‧‧螺紋部 1151‧‧‧Threaded Department

11411‧‧‧邊緣部 11411‧‧‧Edge

f、f1‧‧‧壓縮空氣 f, f1‧‧‧ compressed air

O‧‧‧軸心 O‧‧‧Axis

r1‧‧‧氣壓軸插入用孔之內徑 R1‧‧‧Inner diameter of the air shaft insertion hole

R1‧‧‧徑向軸承部之外徑 R1‧‧‧ outside diameter of radial bearing

r2‧‧‧直徑 R2‧‧‧ diameter

s1‧‧‧軸向軸承間隙之厚度 S1‧‧‧ thickness of axial bearing clearance

s2‧‧‧徑向軸承間隙之厚度 S2‧‧‧ thickness of radial bearing clearance

t1‧‧‧下側塊體材料與上側塊體材料之間隔 t1‧‧‧Interval between the lower block material and the upper block material

t2‧‧‧厚度 T2‧‧‧ thickness

t3‧‧‧輪轂的端面間之距離(滑輪之長度) Distance between the end faces of the t3‧‧·wheels (length of the pulley)

t4‧‧‧徑向軸承部之長度 T4‧‧‧The length of the radial bearing

第1圖係本發明一實施形態之兩端支撐式空氣軸承單元4的外觀圖(無滑輪2)。 Fig. 1 is an external view of a two-end supported air bearing unit 4 according to an embodiment of the present invention (without pulley 2).

第2圖係本發明一實施形態之組裝有滑輪2之狀態的兩端支撐式空氣軸承單元4之側視圖。 Fig. 2 is a side view of the end-support air bearing unit 4 in a state in which the pulley 2 is assembled according to an embodiment of the present invention.

第3圖(A)係滑輪2之前視圖;第3圖(B)係第3圖(A)之A-A剖視圖。 Fig. 3(A) is a front view of the pulley 2; Fig. 3(B) is a cross-sectional view taken along line A-A of Fig. 3(A).

第4圖係本發明一實施形態之氣壓軸單元1的零件展開圖。 Fig. 4 is a developed view of a part of a pneumatic shaft unit 1 according to an embodiment of the present invention.

第5圖(A)係氣壓軸11之前視圖;第5圖(B)係第5圖(A)之B-B剖視圖;第5圖(C)係氣壓軸11之仰視圖;第5圖(D)係徑向軸承部114之放大部分剖視圖。 Fig. 5(A) is a front view of the air pressure shaft 11; Fig. 5(B) is a BB sectional view of Fig. 5(A); Fig. 5(C) is a bottom view of the air pressure shaft 11; Fig. 5(D) An enlarged partial cross-sectional view of the radial bearing portion 114.

第6圖(A)係軸向板12之前視圖;第6圖(B)係第6圖(A)之C-C剖視圖。 Fig. 6(A) is a front view of the axial plate 12; Fig. 6(B) is a cross-sectional view taken along line C-C of Fig. 6(A).

第7圖係顯示對氣壓軸11供氣中的滑輪2之支撐狀態的示意圖。 Fig. 7 is a view showing the state of support of the pulley 2 in the supply of air to the pneumatic shaft 11.

以下,一邊參照附圖,一邊就本發明之實施形態加以說明。 Hereinafter, embodiments of the present invention will be described with reference to the accompanying drawings.

首先,就本實施形態之兩端支撐式靜壓氣體軸承單元之全體構造加以說明。在此,係列舉適用於送出光纖、碳纖維等線材的滑輪2等之在軸心O方向為長條狀的旋轉體之非接觸支撐的兩端支撐式空氣軸承單元4作為 一例。 First, the overall structure of the both-end supported static pressure gas bearing unit of the present embodiment will be described. Here, a series of supported air bearing units 4 for non-contact support of a rotating body such as a pulley 2 for sending an optical fiber or a carbon fiber, etc., which are elongated in the direction of the axis O, are used. An example.

第1圖係本實施形態之兩端支撐式空氣軸承 單元4的外觀圖,第2圖係組裝有支撐對象之滑輪2之狀態的兩端支撐式空氣軸承單元4之側視圖。 Figure 1 is a two-end supported air bearing of this embodiment The external view of the unit 4, and Fig. 2 is a side view of the end-supporting air bearing unit 4 in a state in which the pulley 2 for supporting the object is assembled.

如圖示般,本實施形態之兩端支撐式空氣軸 承單元4,係具備:以能夠旋轉之方式非接觸支撐在軸心O方向為長條狀之滑輪2的氣壓軸單元(air shaft unit)1;以及兩端支撐氣壓軸單元1的二台軸座3A、3B。 As shown in the figure, the two-end supported air shaft of this embodiment The receiving unit 4 includes: an air shaft unit 1 that rotatably supports the pulley 2 that is elongated in the direction of the axis O in a rotatable manner; and two shafts that support the pneumatic shaft unit 1 at both ends Block 3A, 3B.

如後述般,氣壓軸單元1,係氣壓軸11和軸 向板12和螺帽13之組裝體(參照第4圖),滑輪2,係在形成於滑輪2之軸向的氣壓軸插入用孔22內插入有氣壓軸11(形成有多孔質燒結層112的徑向軸承部114)之後,藉由隔著軸向板12將氣壓軸11(桿部115之螺紋部1151)與螺帽13之緊固能在非接觸狀態下以能夠旋轉之方式組裝於氣壓軸單元1。 As will be described later, the pneumatic shaft unit 1, the pneumatic shaft 11 and the shaft In the assembly of the plate 12 and the nut 13 (see FIG. 4), the pulley 2 is inserted into the air shaft insertion hole 22 formed in the axial direction of the pulley 2, and the pneumatic shaft 11 is inserted (the porous sintered layer 112 is formed). After the radial bearing portion 114), the pneumatic shaft 11 (the threaded portion 1151 of the rod portion 115) and the nut 13 can be rotatably assembled in a non-contact state via the axial plate 12 Pneumatic shaft unit 1.

另一方面,二台軸座3A、3B,係例如以相應 於氣壓軸單元1之長度的間隔相對向的方式配置固定於石材板(stone plate)等之台座上。各軸座3A、3B,係以與滑輪2之最大直徑相應的高度之位置,來保持軸心O朝向大致平行於台座的氣壓軸單元1之端部(軸向板12、氣壓軸11之基底部113)。 On the other hand, the two axle bases 3A, 3B are, for example, corresponding The pedestal fixed to a stone plate or the like is disposed so as to face the interval of the length of the pneumatic shaft unit 1. Each of the shaft seats 3A, 3B maintains the axis O toward the end of the pneumatic shaft unit 1 substantially parallel to the pedestal (the base of the axial plate 12 and the pneumatic shaft 11 at a position corresponding to the maximum diameter of the pulley 2). Part 113).

各軸座3A、3B,係分別具有:例如以螺栓固 定於台座之具有凸緣35的下側塊體材料(block material)33;及載置於下側塊體材料33之上面的上側塊 體材料32;以及用以調整下側塊體材料33之上面與上側塊體材料32之底面之間隔t1的二支螺栓34。在下側塊體材料33之上面與上側塊體材料32之底面係分別於厚度t2方向形成有半圓形剖面的溝槽,且藉由上述的溝槽相對向而在預定之高度的位置形成有軸固定孔31。二支螺栓34,係在軸固定孔31兩側的位置,經由上側塊體材料32之螺栓孔而鎖緊連結於下側塊體材料33之螺紋孔。 Each of the axle seats 3A, 3B has: for example, bolted a lower block material 33 having a flange 35 at the pedestal; and an upper block placed above the lower block material 33 The body material 32; and two bolts 34 for adjusting the interval t1 between the upper surface of the lower block material 33 and the bottom surface of the upper block material 32. A groove having a semi-circular cross section is formed on the upper surface of the lower block material 33 and the bottom surface of the upper block material 32 in the thickness t2 direction, and is formed at a predetermined height by the above-mentioned grooves facing each other. The shaft fixing hole 31. The two bolts 34 are fastened to the screw holes of the lower block material 33 via the bolt holes of the upper block material 32 at positions on both sides of the shaft fixing hole 31.

在對向配置的二台軸座3A、3B之軸固定孔 31分別插入有氣壓軸單元1之端部(軸向板12、氣壓軸11之基底部113),且二支螺栓34緊固於各自的軸座3A、3B,藉此下側塊體材料33與上側塊體材料32之間隔t1會變窄,而氣壓軸單元1之兩端部(軸向板12、氣壓軸11之基底部113)可固定。藉此,組裝於氣壓軸單元1之滑輪2,係能在預定之高度的位置以在非接觸狀態下能夠繞軸心O方向旋轉的方式保持。 Shaft fixing holes for two shaft seats 3A, 3B arranged in opposite directions 31 is inserted into the end of the pneumatic shaft unit 1 (the axial plate 12, the base portion 113 of the pneumatic shaft 11), and the two bolts 34 are fastened to the respective shaft seats 3A, 3B, whereby the lower block material 33 The interval t1 from the upper block material 32 is narrowed, and both end portions of the pneumatic shaft unit 1 (the axial plate 12 and the base portion 113 of the pneumatic shaft 11) can be fixed. Thereby, the pulley 2 assembled to the pneumatic shaft unit 1 can be held at a predetermined height position so as to be rotatable about the axis O in a non-contact state.

另外,本實施形態中,雖然是使用以二支螺 栓34來調整具有凸緣35的下側塊體材料33與上側塊體材料32之間隔t1的二台軸座3A、3B,但是若能夠在其兩端部(軸向板12、氣壓軸11之基底部113)保持氣壓軸單元1的話,亦可使用任何形態的軸座。 In addition, in the present embodiment, although two snails are used The pin 34 adjusts the two shaft seats 3A, 3B having the interval t1 between the lower block material 33 of the flange 35 and the upper block material 32, but if it can be at both ends (axial plate 12, pneumatic shaft 11) When the base portion 113) holds the pneumatic shaft unit 1, any type of shaft seat can be used.

其次,說明滑輪2、及以能夠繞軸心O旋轉之方式非接觸支撐該滑輪2的氣壓軸單元1之詳細。 Next, the details of the pulley 2 and the pneumatic shaft unit 1 that supports the pulley 2 in a non-contact manner so as to be rotatable about the axis O will be described.

第3圖(A)係滑輪2之前視圖;第3圖(B)係第3圖(A)之A-A剖視圖。 Fig. 3(A) is a front view of the pulley 2; Fig. 3(B) is a cross-sectional view taken along line A-A of Fig. 3(A).

如圖示般,支撐對象之滑輪2,係具有例如在 軸心O方向上較直徑r2更長之略呈長條狀的圓柱形,且在其外周面23,係於圓周方向舖設有線材。又,在滑輪2,於軸心O通過的位置,係形成有從一方之端面25A貫通至另一方之端面25B的氣壓軸插入用孔22,且在該氣壓插入用孔22內,以能夠滑動之方式插入有氣壓軸11之具有多孔質燒結層112的徑向軸承部114。 As shown, the pulley 2 supporting the object has, for example, A slightly elongated cylindrical shape in the direction of the axis O is longer than the diameter r2, and a wire material is laid on the outer peripheral surface 23 in the circumferential direction. In the pulley 2, a pneumatic shaft insertion hole 22 penetrating from one end surface 25A to the other end surface 25B is formed at a position where the shaft center O passes, and is slidable in the air pressure insertion hole 22. In this manner, the radial bearing portion 114 having the porous sintered layer 112 of the pneumatic shaft 11 is inserted.

在滑輪2之兩端面25A、25B,係分別形成有 包圍氣壓軸插入用孔22的輪轂(boss)24A、24B。各輪轂24A、24B之端面241A、241B係可精加工成平坦。在組裝滑輪2後之狀態(第2圖之狀態)的空氣軸承單元4中,一方之輪轂24A的端面241A,係隔出些微的間隔(軸向軸承間隙),來與氣壓軸11之後述的段差面(軸向軸承面)1132相對向,而另一方之輪轂24B的端面241B係隔出些微的間隔(軸向軸承間隙)來與軸向板12之一方的端面(軸向軸承面)121相對向(參照第5圖、第6圖)。 The end faces 25A and 25B of the pulley 2 are respectively formed with Bosses 24A, 24B surrounding the air shaft insertion hole 22. The end faces 241A, 241B of the hubs 24A, 24B can be finished to be flat. In the air bearing unit 4 in the state after the assembly of the pulley 2 (the state of Fig. 2), the end surface 241A of one of the hubs 24A is separated by a slight interval (axial bearing clearance), and the pneumatic shaft 11 will be described later. The step surface (axial bearing surface) 1132 is opposed to each other, and the other end surface 241B of the hub 24B is separated by a slight interval (axial bearing gap) from one end surface (axial bearing surface) of the axial plate 12 121 Relative direction (refer to Figure 5 and Figure 6).

另外,如圖示般,在滑輪2之兩端部,亦可 形成有從外周面23朝徑向膨出的環狀之凸緣部21。 In addition, as shown in the figure, at both ends of the pulley 2, An annular flange portion 21 that bulges in the radial direction from the outer peripheral surface 23 is formed.

第4圖係氣壓軸單元1之零件展開圖。 Fig. 4 is a developed view of the parts of the pneumatic shaft unit 1.

如圖示般,氣壓軸單元1,係具備:插入於滑輪2之氣壓軸插入用孔22內,且以能夠繞軸心O旋轉之方式非接觸支撐滑輪2的氣壓軸11;及阻止滑輪2從氣壓軸11脫落的軸向板12;以及將軸向板12固定於氣壓軸11的螺帽13。 As shown in the figure, the pneumatic shaft unit 1 includes a pneumatic shaft 11 that is inserted into the air shaft insertion hole 22 of the pulley 2 and that is non-contacting the support pulley 2 so as to be rotatable about the axis O; and the blocking pulley 2 An axial plate 12 that is detached from the pneumatic shaft 11 and a nut 13 that fixes the axial plate 12 to the pneumatic shaft 11.

第5圖(A)係氣壓軸11之前視圖;第5圖(B) 係第5圖(A)之B-B剖視圖;第5圖(C)係氣壓軸11之仰視圖;第5圖(D)係徑向軸承部114之放大部分剖視圖。 Figure 5 (A) is a front view of the pneumatic shaft 11; Figure 5 (B) Fig. 5(A) is a cross-sectional view taken along line B-B; Fig. 5(C) is a bottom view of the pneumatic shaft 11, and Fig. 5(D) is an enlarged partial cross-sectional view of the radial bearing portion 114.

如圖示般,氣壓軸11,係具備:具有段差的 圓筒狀之背墊金屬(back metal)111;以及形成於背墊金屬111之中段部(徑向軸承部)114之外周面1142上的多孔質燒結層112。 As shown, the pneumatic shaft 11 is provided with a step A cylindrical back metal 111; and a porous sintered layer 112 formed on the outer peripheral surface 1142 of the intermediate portion (radial bearing portion) 114 of the backing metal 111.

背墊金屬111,係一體地具備:直徑與滑輪2 之輪轂24A、24B之外徑大致相同的基底部113;及直徑比基底部113還更為小的徑向軸承部114;以及直徑比徑向軸承部114更小的桿(rod)部115。 Back pad metal 111, integrally provided with: diameter and pulley 2 The base portions 113 having substantially the same outer diameter of the hubs 24A and 24B; and a radial bearing portion 114 having a smaller diameter than the base portion 113; and a rod portion 115 having a smaller diameter than the radial bearing portion 114.

在基底部113之一方的端面1131,係形成有 從該端面1131通過基底部113之內部而到達徑向軸承部114之內部的通氣路116。在一方之端面1131的通氣路116之開口部(供氣口)117,係形成有將用以連結泵浦之供氣管41的聯結器(coupler)40(參照第2圖)予以鎖入的螺紋部118。 An end surface 1131 of one of the base portions 113 is formed with The end surface 1131 passes through the inside of the base portion 113 and reaches the air passage 116 inside the radial bearing portion 114. In the opening (air supply port) 117 of the air passage 116 of the one end surface 1131, a thread that locks a coupler 40 (refer to Fig. 2) for connecting the pumping air supply pipe 41 is formed. Part 118.

該基底部113,係插入於一方之軸座3A的軸 固定孔31內,直到另一方之端部1132從一方之軸座3A的軸固定孔31朝向另一方之軸座3B側突出的位置為止(參照第2圖)。在此狀態下可鎖緊一方之軸座3A的二支螺栓34,藉此,基底部113係可固定於一方之軸座3A的軸固定孔31內。 The base portion 113 is inserted into the shaft of one of the shaft seats 3A. In the fixing hole 31, the other end portion 1132 is protruded from the shaft fixing hole 31 of one of the shaft seats 3A toward the other shaft seat 3B side (see Fig. 2). In this state, the two bolts 34 of one of the shaft seats 3A can be locked, whereby the base portion 113 can be fixed in the shaft fixing hole 31 of one of the shaft seats 3A.

徑向軸承部114,係一體地形成於基底部113 之另一方的端面(作為軸向軸承面之段差面發揮作用)1132,且在該徑向軸承部114之外周面1142的全區域,形成有具有通氣性的多孔質燒結層112。在徑向軸承部114之外周面1142,係於圓周方向形成有位於與多孔質燒結層112間之境界部的複數個環狀槽1143,且在各環狀槽1143之槽底,係分別形成有連繫於通氣路116的孔1144。藉此,當來自連結於供氣口117的泵浦之供氣管41的供氣開始時,從泵浦送來的壓縮空氣,就會經由通氣路116及孔1144,供應至位於徑向軸承部114之外周面1142的圓周方向之各環狀槽1143,且通過多孔質燒結層112內之細孔,從發揮作為徑向軸承面的多孔質燒結層112之外周面1121噴出。 The radial bearing portion 114 is integrally formed on the base portion 113 The other end surface (acting as a step surface of the axial bearing surface) 1132, and a porous sintered layer 112 having air permeability is formed over the entire outer peripheral surface 1142 of the radial bearing portion 114. In the outer peripheral surface 1142 of the radial bearing portion 114, a plurality of annular grooves 1143 formed in a boundary portion between the porous sintered layer 112 and the bottom portion of the annular groove 1143 are formed in the circumferential direction. There is a hole 1144 that is connected to the air passage 116. Thereby, when the supply of air from the pump supply pipe 41 connected to the air supply port 117 is started, the compressed air sent from the pump is supplied to the radial bearing portion via the air passage 116 and the hole 1144. Each of the annular grooves 1143 in the circumferential direction of the outer peripheral surface 1142 is ejected from the outer peripheral surface 1121 of the porous sintered layer 112 which is a radial bearing surface through the pores in the porous sintered layer 112.

另外,位於徑向軸承部114之外周面1142的 環狀槽1143之條數及佈置,只要是以壓縮空氣能從多孔質燒結層112之外周面1121全區域均一地噴出的方式適當地決定即可。例如,亦可將與徑向軸承部114之長度(多孔質燒結層112之寬度)t4等相應之條數的環狀槽1143,以大致等間隔配置於多孔質燒結層112之軸心O方向。 又,亦可在從徑向軸承部114之中央位置(從徑向軸承部114之一方的端起算僅位在t4/2內側的位置)朝基底部113側及桿部115側分離的位置等、能夠維持較高的徑向軸承間隙60整體之壓力的位置形成環狀槽1143。 In addition, it is located on the outer peripheral surface 1142 of the radial bearing portion 114. The number and arrangement of the annular grooves 1143 may be appropriately determined so that compressed air can be uniformly ejected from the entire outer peripheral surface 1121 of the porous sintered layer 112. For example, the number of annular grooves 1143 corresponding to the length of the radial bearing portion 114 (the width of the porous sintered layer 112) t4 or the like may be arranged at substantially equal intervals in the direction of the axis O of the porous sintered layer 112. . In addition, the position from the center position of the radial bearing portion 114 (the position which is located only inside the t4/2 from one end of the radial bearing portion 114) to the base portion 113 side and the rod portion 115 side may be used. The annular groove 1143 is formed at a position capable of maintaining a high pressure of the entire radial bearing gap 60.

形成有多孔質燒結層112的徑向軸承部114, 係插入於滑輪2之氣壓軸插入用孔22內。包含多孔質燒 結層112的徑向軸承部114之外徑R1,係設計得比滑輪2的氣壓軸插入用孔22之內徑r1(參照第3圖)還更小預定尺寸。因此,當徑向軸承部114插入於滑輪2之氣壓軸插入用孔22內時,就會在該氣壓軸插入用孔22之內周面221與形成於徑向軸承部114之外周面1142的多孔質燒結層112之外周面(徑向軸承面)1121之間形成有徑向軸承間隙60(參照第7圖)。然後,在從泵浦對氣壓軸11開始供氣之後,藉由從多孔質燒結層112之外周面(徑向軸承面)1121噴出的壓縮空氣,在該徑向軸承間隙60形成有高壓的空氣膜。能藉由該空氣膜之壓力來支撐徑向荷重。 A radial bearing portion 114 having a porous sintered layer 112 formed thereon, It is inserted into the air shaft insertion hole 22 of the pulley 2. Contains porous burning The outer diameter R1 of the radial bearing portion 114 of the knot layer 112 is designed to be smaller than the inner diameter r1 (see FIG. 3) of the air shaft insertion hole 22 of the pulley 2 by a predetermined size. Therefore, when the radial bearing portion 114 is inserted into the air shaft insertion hole 22 of the pulley 2, the inner circumferential surface 221 of the air shaft insertion hole 22 and the outer circumferential surface 1142 of the radial bearing portion 114 are formed. A radial bearing gap 60 is formed between the outer peripheral surface (radial bearing surface) 1121 of the porous sintered layer 112 (see Fig. 7). Then, after the supply of air from the pump to the pneumatic shaft 11, the high-pressure air is formed in the radial bearing gap 60 by the compressed air ejected from the outer peripheral surface (radial bearing surface) 1121 of the porous sintered layer 112. membrane. The radial load can be supported by the pressure of the air film.

徑向軸承部114之長度(段差面1132、1141 間之距離)t4,係設計得比滑輪2的兩端面25A、25B之輪轂24A、24B的端面241A、241B間之距離(滑輪2之長度)t3還更大預定尺寸。因此,在從泵浦對氣壓軸11開始供氣之後,在插入於徑向軸承部114的滑輪2之一方的輪轂24A之端面241A、與基底部113之另一方的端面(藉由徑向軸承部114及基底部113之外徑差所形成,且發揮作為軸向軸承面之功能的段差面)1132之間,係形成有與徑向軸承間隙60連繫的軸向軸承間隙61a。同樣,在滑輪2之另一方的輪轂24B之端面241B、與接觸到徑向軸承部114的端面(藉由徑向軸承部114及桿部115之外徑差所形成的段差面)1141、且發揮作為軸向軸承面之功能之後述的軸向板12之一方的端面121之間,亦形成有與徑向軸承間隙60連繫的軸向軸承間隙61b(參照第7圖)。另外, 為了防止自激振動發生,較佳是以徑向軸承部114之端面1141的邊緣部11411不塌邊之方式進行精加工,藉此提高軸向板12之組裝精度。 The length of the radial bearing portion 114 (segment surface 1132, 1141) The distance t4 is designed to be larger than the distance (the length of the pulley 2) t3 of the end faces 241A, 241B of the hubs 24A, 24B of the both end faces 25A, 25B of the pulley 2 by a predetermined size. Therefore, after the air supply to the air pressure shaft 11 is started from the pump, the end surface 241A of the hub 24A inserted into one of the pulleys 2 of the radial bearing portion 114 and the other end surface of the base portion 113 (by the radial bearing) An axial bearing gap 61a that is formed in contact with the radial bearing gap 60 is formed between the step 114 and the base portion 113 which are formed by the difference in outer diameter between the portion 114 and the base portion 113. Similarly, the end surface 241B of the other hub 2B of the pulley 2 and the end surface (the step surface formed by the difference in outer diameter between the radial bearing portion 114 and the rod portion 115) contacting the radial bearing portion 114 are 1141, and An axial bearing gap 61b (see FIG. 7) that is connected to the radial bearing gap 60 is also formed between the end faces 121 which are one of the axial plates 12 which will function as the axial bearing faces. In addition, In order to prevent self-excited vibration from occurring, it is preferable to perform finishing by the edge portion 11411 of the end surface 1141 of the radial bearing portion 114 without collapsing, thereby improving the assembly precision of the axial plate 12.

桿部115,係連續形成於徑向軸承部114之端 面1141,且插入於後述的軸向板12之軸插入用孔123內。又,在該桿部115之前端,係形成有與螺帽13螺合的螺紋部1151。 The rod portion 115 is continuously formed at the end of the radial bearing portion 114 The surface 1141 is inserted into the shaft insertion hole 123 of the axial plate 12 to be described later. Further, a screw portion 1151 that is screwed to the nut 13 is formed at the front end of the rod portion 115.

第6圖(A)係軸向板12之前視圖;第6圖(B) 係第6圖(A)之C-C剖視圖。 Figure 6 (A) is a front view of the axial plate 12; Figure 6 (B) Figure 6 is a cross-sectional view taken along line C-C of Figure 6 (A).

如圖示般,軸向板12,係為外徑與氣壓軸11 的基底部113之外徑大致相同的圓筒形狀,且在軸心O通過的位置,形成有從一方之端面121貫通至另一方之面122的軸插入用孔123。在該軸插入用孔123,係插入有氣壓軸11之桿部115。 As shown, the axial plate 12 is the outer diameter and the air pressure shaft 11 The base portion 113 has a cylindrical shape having substantially the same outer diameter, and a shaft insertion hole 123 penetrating from one end surface 121 to the other surface 122 is formed at a position where the axis O passes. The shaft insertion hole 123 is inserted into the rod portion 115 of the pneumatic shaft 11.

而且,具有上述構成的氣壓軸單元1,係組裝 如下。 Further, the pneumatic shaft unit 1 having the above configuration is assembled as follows.

首先,在氣壓軸單元1組裝有滑輪2。具體而言,以形成有多孔質燒結層112的徑向軸承部114位於滑輪2之氣壓軸插入用孔22內的方式,將氣壓軸11插入於滑輪2之氣壓軸插入用孔22,接著,以桿部115位於軸向板12之軸插入用孔123內的方式,將插入有滑輪2的氣壓軸11更進一步插入於軸向板12之軸插入用孔123。在此狀態下,當在形成於桿部115之前端的螺紋部1151鎖緊連結有螺帽13時,軸向板12,其一方之端面121, 就會以接觸到藉由徑向軸承部114及桿部115之外徑差所形成的段差面(徑向軸承部114之端面)1141的位置來固定。 First, the pulley 2 is assembled in the pneumatic shaft unit 1. Specifically, the pneumatic bearing shaft 114 is inserted into the air shaft insertion hole 22 of the pulley 2 so that the radial bearing portion 114 in which the porous sintered layer 112 is formed is placed in the air shaft insertion hole 22 of the pulley 2, and then, The air shaft 11 into which the pulley 2 is inserted is further inserted into the shaft insertion hole 123 of the axial plate 12 so that the rod portion 115 is positioned in the shaft insertion hole 123 of the axial plate 12. In this state, when the threaded portion 1151 formed at the front end of the rod portion 115 is locked and coupled with the nut 13, the axial plate 12, one end surface 121 thereof, The position of the step surface (the end surface of the radial bearing portion 114) 1141 formed by the difference in outer diameter between the radial bearing portion 114 and the rod portion 115 is fixed.

之後,在如上述地組裝有滑輪2的氣壓軸單 元1之軸心O大致平行地朝向台座的狀態下,使得其兩端(軸向板12、氣壓軸11之基底部113),固定於以預定間隔對向配置的二台軸座3A、3B(參照第2圖)。具體而言,能以氣壓軸11的基底部113之另一方的端面(發揮作為軸向軸承面之功能的段差面)1132從一方之軸座3A的軸固定孔31朝向另一方之軸座3B側突出的方式,使氣壓軸11之基底部113插入於一方之軸座3A的軸固定孔31內,並且能以軸向板12之一方的端面(發揮作為軸向軸承面之功能的端面)121從另一方之軸座3B的軸固定孔31朝向一方之軸座3A側突出的方式,使軸向板12插入於另一方之軸座3B的軸固定孔31內。在此狀態下能藉由各軸座3A、3B之二支螺栓34的緊固,使氣壓板11之基底部113及軸向板12固定於各軸座3A、3B之軸固定孔31內。 Thereafter, the air pressure shaft of the pulley 2 is assembled as described above. In a state in which the axis O of the element 1 is substantially parallel to the pedestal, the both ends (the axial plate 12 and the base portion 113 of the pneumatic shaft 11) are fixed to the two shaft seats 3A, 3B which are disposed opposite each other at a predetermined interval. (Refer to Figure 2). Specifically, the other end surface of the base portion 113 of the pneumatic shaft 11 (the step surface that functions as the axial bearing surface) 1132 can be moved from the shaft fixing hole 31 of the one shaft seat 3A toward the other shaft seat 3B. In a side protruding manner, the base portion 113 of the pneumatic shaft 11 is inserted into the shaft fixing hole 31 of one of the shaft seats 3A, and one end surface of the axial plate 12 can be used (the end surface functioning as an axial bearing surface) The axial plate 12 is inserted into the shaft fixing hole 31 of the other shaft seat 3B so that the shaft fixing hole 31 of the other shaft seat 3B protrudes toward the one shaft seat 3A side. In this state, the base portion 113 and the axial plate 12 of the air pressure plate 11 can be fixed in the shaft fixing holes 31 of the respective shaft seats 3A and 3B by fastening the two bolts 34 of the respective shaft seats 3A and 3B.

如上述般,因徑向軸承部114之長度t4,係 比滑輪2之長度t3還更多出預定尺寸,故而在滑輪2的一方之輪轂24A的端面241A與基底部113之另一方的端面(軸向軸承面)1132之間形成有軸向軸承間隙61a,且在滑輪2的另一方之輪轂24B的端面241B與軸向板12之一方的端面(軸向軸承面)121之間形成有軸向軸承間隙61b。在上述的軸向軸承間隙61a、61b內,係流入有從徑向軸承間隙60排出的壓縮空氣,且形成有高壓的空氣膜 。能藉由該空氣膜之壓力來支撐軸向荷重。 As described above, due to the length t4 of the radial bearing portion 114, Since the predetermined length is larger than the length t3 of the pulley 2, an axial bearing gap 61a is formed between the end surface 241A of one of the hubs 24A of the pulley 2 and the other end surface (axial bearing surface) 1132 of the base portion 113. An axial bearing gap 61b is formed between the end surface 241B of the other hub 24B of the pulley 2 and one end surface (axial bearing surface) 121 of the axial plate 12. In the above-described axial bearing gaps 61a, 61b, compressed air discharged from the radial bearing gap 60 flows therein, and a high-pressure air film is formed. . The axial load can be supported by the pressure of the air film.

在此,徑向軸承部114之長度t4,係以滑輪2兩側的軸向軸承間隙61a、61b之厚度s1(參照第7圖)比徑向軸承間隙60之厚度s2還更為大之方式所設定,以免發生自激振動。在此,所謂以免發生自激振動之厚度s1的軸向軸承間隙61a、61b,係指較寬的軸向軸承間隙61a、61b,其設計為以下的程度:即便因呈無負載狀態之滑輪2在軸向方向所發生之些微程度的移動,使得滑輪2些微靠近一方之軸向軸承面1132、121側,亦不會急劇地被回推至另一方之軸向軸承面121、1132側。例如,在滑輪2的輪轂24A、24B之外徑約22mm、徑向軸承間隙60之厚度約9μm至10μm的情況,以軸向軸承間隙61a、61b之厚度s1成為約22.5μm至37μm的方式設定徑向軸承部114之長度t4,且更進一步在開放流量520NL/hr以下之範圍內進行供氣壓0.5Mpa之壓縮空氣的流量調整,藉此能防止自激振動之發生。 Here, the length t4 of the radial bearing portion 114 is such that the thickness s1 (see FIG. 7) of the axial bearing gaps 61a, 61b on both sides of the pulley 2 is larger than the thickness s2 of the radial bearing gap 60. Set to avoid self-excited vibration. Here, the axial bearing gaps 61a and 61b for avoiding the self-excited vibration thickness s1 refer to the wide axial bearing gaps 61a and 61b, which are designed to the extent that the pulley 2 is in an unloaded state. The slight movement in the axial direction causes the pulley 2 to be slightly closer to the axial bearing surface 1132, 121 side of one side, and is not suddenly pushed back to the other axial bearing surface 121, 1132 side. For example, when the outer diameters of the hubs 24A and 24B of the pulley 2 are about 22 mm and the thickness of the radial bearing gap 60 is about 9 μm to 10 μm, the thickness s1 of the axial bearing gaps 61a and 61b is set to be about 22.5 μm to 37 μm. The length t4 of the radial bearing portion 114 and the flow rate of the compressed air at a pressure of 0.5 MPa are further adjusted within the range of the open flow rate of 520 NL/hr or less, whereby the occurrence of self-excited vibration can be prevented.

其次,就對氣壓軸11供氣中的滑輪2之支撐狀態加以說明。 Next, the state of support of the pulley 2 in the supply of air to the pneumatic shaft 11 will be described.

第7圖係顯示對氣壓軸11供氣中的滑輪2之支撐狀態的示意圖。 Fig. 7 is a view showing the state of support of the pulley 2 in the supply of air to the pneumatic shaft 11.

如圖示般,在組裝有滑輪2之狀態(第2圖之狀態)的空氣軸承單元4中,當將泵浦之供氣管(未圖示)連結於氣壓軸11之供氣口117,且開始來自泵浦之壓縮空氣f的供應時,該壓縮空氣f,係經由氣壓軸11之通氣路 116及孔1144,供應至位於徑向軸承部114之外周面1142的各環狀槽1143,且從多孔質燒結層112之外周面(徑向軸承面)1121噴出至徑向軸承間隙60內。因此,在徑向軸承間隙60內形成有高壓的空氣膜,能藉由該壓力來支撐徑向荷重。藉此,能拘束滑輪2朝向徑向方向之移動。 As shown in the figure, in the air bearing unit 4 in which the pulley 2 is assembled (the state of Fig. 2), a pumping air supply pipe (not shown) is coupled to the air supply port 117 of the air shaft 11, and When the supply of compressed air f from the pump is started, the compressed air f is an air passage through the pneumatic shaft 11 116 and the hole 1144 are supplied to the respective annular grooves 1143 located on the outer peripheral surface 1142 of the radial bearing portion 114, and are ejected from the outer peripheral surface (radial bearing surface) 1121 of the porous sintered layer 112 into the radial bearing gap 60. Therefore, a high-pressure air film is formed in the radial bearing gap 60, and the radial load can be supported by the pressure. Thereby, the movement of the pulley 2 in the radial direction can be restrained.

再者,徑向軸承間隙60內之壓縮空氣f,係 沿著多孔質燒結層112之外周面(徑向軸承面)1121,朝向軸向板12之一方的端面(軸向軸承面)121側及基底部113之另一方的端面(軸向軸承面)1132側流動,且流入於滑輪2的一方之輪轂24A的端面241A與基底部113之軸向軸承面1132之間的軸向軸承間隙61a、及滑輪2的另一方之輪轂24B的端面241B與軸向板12之一方的端面(軸向軸承面)121之間的軸向軸承間隙61b。 Furthermore, the compressed air f in the radial bearing gap 60 is The outer peripheral surface (radial bearing surface) 1121 of the porous sintered layer 112 faces the one end surface (axial bearing surface) 121 side of the axial plate 12 and the other end surface (axial bearing surface) of the base portion 113. The axial bearing gap 61a flowing between the end surface 241A of one of the hubs 24A of the pulley 2 and the axial bearing surface 1132 of the base portion 113, and the end surface 241B and the shaft of the other hub 24B of the pulley 2 An axial bearing gap 61b between the end faces (axial bearing faces) 121 of one of the plates 12.

流入於軸向軸承間隙61a、61b的壓縮空氣f1 ,係以輻射狀朝向各輪轂24A、24B之外周流動,最終朝向外部(大氣壓)釋放出。各軸向軸承間隙61a、61b內之壓力,係在從徑向軸承間隙60排出的壓縮氣體f1所流入的滑輪2之內周側變高,而隨著朝向輪轂24A、24B之外周逐漸地減少。因此,在軸向軸承間隙61a、61b內係形成有平均壓力較高的空氣膜,能藉由該壓力來支撐軸向荷重。藉此,能拘束滑輪2朝向軸向方向之移動。 Compressed air f1 flowing into the axial bearing gaps 61a, 61b The radiation flows toward the outer circumference of each of the hubs 24A and 24B, and is finally released toward the outside (atmospheric pressure). The pressure in each of the axial bearing gaps 61a, 61b becomes higher on the inner peripheral side of the pulley 2 into which the compressed gas f1 discharged from the radial bearing gap 60 flows, and gradually decreases toward the outer circumference of the hubs 24A, 24B. . Therefore, an air film having a relatively high average pressure is formed in the axial bearing gaps 61a and 61b, and the axial load can be supported by the pressure. Thereby, the movement of the pulley 2 in the axial direction can be restrained.

在此,在軸向軸承間隙61a、61b之厚度s1較小的情況,當滑輪2沿著軸心O些微移動時,因一方之 軸向軸承間隙61a、61b會變狹窄,而另一方之軸向軸承間隙61a、61b變寬厚,故而軸向軸承間隙61a、61b內之壓力分佈會變化,而有發生自激振動的可能性。具體而言,因在變窄的軸向軸承間隙61a、61b內,壓力會依阻抗之增加而上升,而在變寬的軸向軸承間隙61a、61b內,壓力會依阻抗之減少而減少,故而滑輪2,係以只要些微地靠近一方之軸向軸承面1132、121就會被回推至另一方之軸向軸承面121、1132側的方式沿著軸心O移動。這情形將反覆發生。 Here, in the case where the thickness s1 of the axial bearing gaps 61a, 61b is small, when the pulley 2 moves slightly along the axis O, The axial bearing gaps 61a, 61b become narrower, and the other axial bearing gaps 61a, 61b become wider and thicker, so that the pressure distribution in the axial bearing gaps 61a, 61b changes, and there is a possibility that self-excited vibration occurs. Specifically, since the pressure increases in accordance with an increase in impedance in the narrowed axial bearing gaps 61a, 61b, the pressure decreases in the widened axial bearing gaps 61a, 61b depending on the impedance. Therefore, the pulley 2 is moved along the axis O so as to be pushed back to the other axial bearing surfaces 121 and 1132 as long as the axial bearing surfaces 1132 and 121 are slightly pushed closer to each other. This situation will happen again and again.

在本實施形態中,因是以即便滑輪2朝向一 方之軸向軸承面1132、121些微地移動,亦不急劇地被回推至另一方之軸向軸承面121、1132側的程度設置具有餘裕之厚度s1的軸向軸承間隙61a、61b,故而可以抑止自激振動之發生。 In this embodiment, even if the pulley 2 is oriented toward one The axial bearing surfaces 1132, 61 of the square are slightly moved, and the axial bearing gaps 61a, 61b having the margin s1 of the margin are provided without being sharply pushed back to the other axial bearing faces 121, 1132. It can suppress the occurrence of self-excited vibration.

如此,依據本實施形態的空氣軸承單元4,因 能從與滑輪2之內周面221對向的多孔質燒結層112對徑向軸承間隙60供應壓縮空氣,而從該徑向軸承間隙60排出的壓縮空氣,能在保持其壓力之狀態下,導入於滑輪2的兩面側之軸向軸承間隙61a、61b,故而可以藉由徑向軸承間隙60內的空氣膜之壓力及軸向軸承間隙61a、61b內的空氣膜之壓力,以非接觸方式支撐滑輪2之徑向荷重及軸向荷重。因此,因幾乎不會發生動力損失,故而可以使滑輪2高速地旋轉。又,因將從徑向軸承間隙60排出的壓縮空氣利用於軸向軸承間隙61a、61b內的空氣膜之 形成,故而沒有必要將用以排出來自徑向軸承間隙60之壓縮空氣的排氣用槽和排氣孔,形成於氣壓軸單元1及滑輪2中之任一個。因而,可以簡化保持高速旋轉的滑輪2之空氣軸承單元4的構造。 Thus, according to the air bearing unit 4 of the present embodiment, The compressed air can be supplied to the radial bearing gap 60 from the porous sintered layer 112 opposed to the inner peripheral surface 221 of the pulley 2, and the compressed air discharged from the radial bearing gap 60 can maintain its pressure. The axial bearing gaps 61a, 61b are introduced on both sides of the pulley 2, so that the pressure of the air film in the radial bearing gap 60 and the pressure of the air film in the axial bearing gaps 61a, 61b can be used in a non-contact manner. The radial load and axial load of the support pulley 2 are supported. Therefore, since the power loss hardly occurs, the pulley 2 can be rotated at a high speed. Further, the compressed air discharged from the radial bearing gap 60 is utilized for the air film in the axial bearing gaps 61a, 61b. Since it is formed, it is not necessary to form the exhaust groove and the exhaust hole for discharging the compressed air from the radial bearing gap 60, and it is formed in either one of the pneumatic shaft unit 1 and the pulley 2. Thus, the configuration of the air bearing unit 4 of the pulley 2 that maintains the high speed rotation can be simplified.

再者,因亦沒有必要將對軸向軸承間隙61a、 61b噴出壓縮空氣的多孔質燒結層另外設置於氣壓軸11,故而可以更加簡化空氣軸承單元4之構造,並且可以謀求空氣軸承單元4之製造成本的減低。 Furthermore, since it is not necessary to apply the axial bearing clearance 61a, Since the porous sintered layer in which compressed air is blown off 61b is additionally provided to the pneumatic shaft 11, the structure of the air bearing unit 4 can be further simplified, and the manufacturing cost of the air bearing unit 4 can be reduced.

又,氣壓軸單元1係以其兩端部來保持,故 而即便為了保持長條狀之滑輪2而使氣壓軸11長條化,亦可以抑制氣壓軸11因自重所引起的撓曲。因此,隔出些微之徑向軸承間隙60可防止相對向的滑輪2之氣壓軸插入用孔22之內周面221與多孔質燒結層112之外周面(徑向軸承面)1121的接觸。因此,即便將支撐對象之滑輪2在軸心O方向加長,亦可以穩定地非接觸支撐該滑輪2。 Moreover, the pneumatic shaft unit 1 is held at both ends thereof, so Further, even if the air shaft 11 is elongated in order to hold the long pulley 2, the deflection of the air shaft 11 due to its own weight can be suppressed. Therefore, the slight radial bearing gap 60 is separated to prevent the inner circumferential surface 221 of the air-pressure shaft insertion hole 22 of the opposing pulley 2 from coming into contact with the outer circumferential surface (radial bearing surface) 1121 of the porous sintered layer 112. Therefore, even if the pulley 2 of the support object is lengthened in the direction of the axis O, the pulley 2 can be stably and non-contactly supported.

又,由於沒有必要將順沿軸心O方向的排氣 孔形成於滑輪2,所以能夠將滑輪2之厚度形成得更為薄。因此,即便將滑輪2在軸心O方向加長,亦可以藉由滑輪2的薄化,來謀求滑輪2之輕量化。藉此,因能夠使長條狀之滑輪2更高速地旋轉,並且能減低施加於氣壓軸11的荷重,故而能更進一步抑制氣壓軸11之撓曲。因此,可以更穩定地非接觸支撐高速旋轉的滑輪2。 Also, since there is no need to exhaust the direction along the axis O Since the hole is formed in the pulley 2, the thickness of the pulley 2 can be made thinner. Therefore, even if the pulley 2 is lengthened in the direction of the axis O, the weight of the pulley 2 can be reduced by thinning the pulley 2. Thereby, since the long pulley 2 can be rotated at a higher speed and the load applied to the pneumatic shaft 11 can be reduced, the deflection of the pneumatic shaft 11 can be further suppressed. Therefore, the pulley 2 that supports the high-speed rotation can be supported more stably in a non-contact manner.

又,在本實施形態的空氣軸承單元4中,只 要能從徑向軸承面1121對徑向軸承間隙60噴出壓縮空氣即可,沒有必要安裝從軸向軸承面1132、121及徑向軸承面1121之各個噴出壓縮氣體之較厚的多孔質體。因而,只要厚度數毫米(例如約2.5mm)左右的多孔質燒結層112一體地形成於背墊金屬111即可。因此,可以實現空氣軸承單元4之小型化。 Further, in the air bearing unit 4 of the present embodiment, only It is sufficient to discharge the compressed air from the radial bearing surface 1121 to the radial bearing gap 60. It is not necessary to install a thick porous body that discharges compressed gas from each of the axial bearing surfaces 1132, 121 and the radial bearing surface 1121. Therefore, the porous sintered layer 112 having a thickness of several millimeters (for example, about 2.5 mm) may be integrally formed on the backing metal 111. Therefore, miniaturization of the air bearing unit 4 can be achieved.

又,依據本實施形態的空氣軸承單元4,因在 氣壓軸11側形成有多孔質燒結層112,故而只要在支撐對象之滑輪2,形成有用以插入氣壓軸11的氣壓軸插入用孔22就足夠,沒有必要形成特別的部位。因此,可以減低作為交換零件的滑輪2之製造成本,且可以削減運轉成本(running cost)。 Moreover, according to the air bearing unit 4 of the present embodiment, Since the porous sintered layer 112 is formed on the side of the pneumatic shaft 11, it is sufficient to form the pneumatic shaft insertion hole 22 for inserting the pneumatic shaft 11 in the pulley 2 to be supported, and it is not necessary to form a special portion. Therefore, the manufacturing cost of the pulley 2 as an exchange part can be reduced, and the running cost can be reduced.

又,因將軸向軸承間隙61a、61b之厚度s1, 加大至不發生自激振動的程度,故而可以防止自激振動之發生。因此,可以更穩定地非接觸支撐高速旋轉的滑輪2。 Moreover, since the thickness s1 of the axial bearing gaps 61a, 61b is Increase to the extent that self-excited vibration does not occur, so self-excited vibration can be prevented from occurring. Therefore, the pulley 2 that supports the high-speed rotation can be supported more stably in a non-contact manner.

另外,在本實施形態中,雖然是使用具有段 差的圓柱狀之背墊金屬111,但是亦可將該背墊金屬111形成為例如中空構造。 In addition, in the present embodiment, although the segment is used, The cylindrical back pad metal 111 is poor, but the back pad metal 111 may be formed, for example, in a hollow configuration.

以上,在本實施形態中,雖然是舉支撐長條 狀之滑輪2的空氣軸承單元4為例,但是亦可為支撐長條狀之滑輪2以外的旋轉體者。例如,亦可為支撐複數個一般的滑輪者。 As described above, in the present embodiment, although the support strip is The air bearing unit 4 of the pulley 2 is exemplified, but may be a rotating body other than the long pulley 2. For example, it is also possible to support a plurality of general pulleys.

1‧‧‧氣壓軸單元 1‧‧‧Pneumatic shaft unit

2‧‧‧滑輪 2‧‧‧ pulley

3A、3B‧‧‧軸座 3A, 3B‧‧‧ shaft seat

4‧‧‧空氣軸承單元 4‧‧‧Air bearing unit

12‧‧‧軸向板 12‧‧‧Axial plate

13‧‧‧螺帽 13‧‧‧ Nuts

21‧‧‧凸緣部 21‧‧‧Flange

23‧‧‧輪轂之外周面 23‧‧·The outer circumference of the hub

24A、24B‧‧‧輪轂 24A, 24B‧‧ wheels

31‧‧‧軸固定孔 31‧‧‧Axis fixing hole

32‧‧‧上側塊體材料 32‧‧‧Upper block material

33‧‧‧下側塊體材料 33‧‧‧Lower block material

34‧‧‧螺栓 34‧‧‧Bolts

40‧‧‧聯結器 40‧‧‧Connector

41‧‧‧供氣管 41‧‧‧ gas supply pipe

113‧‧‧基底部 113‧‧‧ base

114‧‧‧徑向軸承部 114‧‧‧ Radial bearing department

121‧‧‧軸向板之端面(軸向軸承面) 121‧‧‧Axial plate end face (axial bearing surface)

1132‧‧‧基底部之端面(段差面、軸向軸承面) 1132‧‧‧End face of the base (segment surface, axial bearing surface)

t2‧‧‧厚度 T2‧‧‧ thickness

Claims (5)

一種靜壓氣體軸承單元,係藉由夾介存在於徑向軸承間隙和第一及第二軸向軸承間隙的氣體膜以非接觸方式支撐朝向繞軸心之方向旋轉的旋轉體之靜壓氣體軸承單元,其特徵為,具備:軸單元,其係插入於貫通前述旋轉體之兩端面的軸插入孔內;以及軸保持手段,其係以前述旋轉體之軸插入孔的兩側之位置來保持前述軸單元,前述軸單元,係具有:徑向軸承面,其係對向於前述軸插入孔之內周面,並在與該內周面之間形成前述徑向軸承間隙,且對前述徑向軸承間隙噴出用以形成前述氣體膜的氣體;及第一軸向軸承面,其係與前述徑向軸承面相鄰,且對向於前述旋轉體之一方的端面,並在與該端面之間,形成與前述徑向軸承間隙之一方的端側連繫的前述第一軸向軸承間隙;以及第二軸向軸承面,其係與前述徑向軸承面相鄰,且對向於前述旋轉體之另一方的端面,並在與該端面之間,形成與前述徑向軸承間隙之另一方的端側連繫的前述第二軸向軸承間隙,前述氣體,係朝向前述第一軸向軸承間隙及前述第二軸向軸承間隙流動於前述徑向軸承間隙內,並從該徑向軸承間隙分別排出至前述第一軸向軸承間隙及前述第二軸向 軸承間隙,且在該第一軸向軸承間隙內及該第二軸向軸承間隙分別形成前述氣體膜。 A static pressure gas bearing unit for supporting a static gas of a rotating body rotating in a direction around an axis by a gas film interposed between a radial bearing gap and first and second axial bearing gaps in a non-contact manner The bearing unit is characterized in that: a shaft unit is inserted into a shaft insertion hole penetrating both end faces of the rotating body; and a shaft holding means is provided at a position of both sides of the shaft insertion hole of the rotating body Holding the shaft unit, the shaft unit has a radial bearing surface that faces the inner circumferential surface of the shaft insertion hole and forms the radial bearing gap between the inner circumferential surface and the aforesaid a radial bearing gap ejecting a gas for forming the gas film; and a first axial bearing surface adjacent to the radial bearing surface and facing an end surface of one of the rotating bodies, and at the end surface Between the first axial bearing gaps that are connected to one end side of the radial bearing gap; and a second axial bearing surface that is adjacent to the radial bearing surface and opposite to the foregoing Rotating body a second axial bearing gap formed between the end surface and the end surface, and the end of the radial bearing gap, wherein the gas is directed toward the first axial bearing gap and a second axial bearing gap flows in the radial bearing gap and is discharged from the radial bearing gap to the first axial bearing gap and the second axial direction The bearing gap, and the gas film is formed in the first axial bearing gap and the second axial bearing gap, respectively. 如申請專利範圍第1項所述的靜壓氣體軸承單元,其中,前述軸單元,係具備:軸,其係具有:附段差的圓柱狀之背墊金屬;以及形成於前述徑向軸承部之外周面的多孔質層,該背墊金屬係具有:基底部;以及形成於前述基底部之端面且直徑比前述基底部還更為小的徑向軸承部,前述軸係插入於前述旋轉體之軸插入孔,並以前述多孔質層之表面作為前述徑向軸承面而在與前述旋轉體之軸插入孔的內周面之間形成前述徑向軸承間隙,並且以前述基底部與前述徑向軸承部之間的段差面作為前述第一軸向軸承面而在與前述旋轉體之一方的端面之間形成前述第一軸向軸承間隙;以及軸向板,其係固定於前述徑向軸承部之端面,且以與前述旋轉體之另一方的端面相對向之面作為前述第二軸向軸承面而在與前述旋轉體之另一方的端面之間形成前述第二軸向軸承間隙,前述軸保持手段,係固定前述軸之基底部和前述軸向板。 The static pressure gas bearing unit according to claim 1, wherein the shaft unit includes: a shaft having a cylindrical backing pad metal with a stepped difference; and a radial bearing portion formed in the radial bearing portion a porous layer having an outer peripheral surface, the backing metal having a base portion; and a radial bearing portion formed on an end surface of the base portion and having a smaller diameter than the base portion, wherein the shaft is inserted into the rotating body The shaft is inserted into the hole, and the radial bearing gap is formed between the inner peripheral surface of the shaft insertion hole of the rotating body with the surface of the porous layer as the radial bearing surface, and the base portion and the radial direction are a stepped surface between the bearing portions as the first axial bearing surface forms a first axial bearing gap between one end surface of the rotating body; and an axial plate fixed to the radial bearing portion An end surface of the second axial bearing between the end surface facing the other end surface of the rotating body as the second axial bearing surface and the other end surface of the rotating body The gap holding means fixes the base portion of the shaft and the axial plate. 如申請專利範圍第1項所述的靜壓氣體軸承單元,其中,作為前述旋轉體,係具有前述軸向之尺寸比前述徑向之尺寸還更為長的滑輪。 The static pressure gas bearing unit according to claim 1, wherein the rotating body has a pulley having a size in the axial direction that is longer than a radial dimension. 如申請專利範圍第2項所述的靜壓氣體軸承單元,其中,作為前述旋轉體,係具有前述軸向之尺寸比前述徑 向之尺寸還更為長的滑輪。 The static pressure gas bearing unit according to claim 2, wherein the rotating body has the axial dimension as compared with the diameter A pulley that is longer in size. 一種軸單元,其特徵為:作為申請專利範圍第1至3項中任一項所述的靜壓氣體軸承單元之構成要素而用於該靜壓氣體軸承單元。 A shaft unit for use in the static pressure gas bearing unit as a component of the static pressure gas bearing unit according to any one of claims 1 to 3.
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