CN205887251U - Main shaft device - Google Patents

Main shaft device Download PDF

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Publication number
CN205887251U
CN205887251U CN201620543026.5U CN201620543026U CN205887251U CN 205887251 U CN205887251 U CN 205887251U CN 201620543026 U CN201620543026 U CN 201620543026U CN 205887251 U CN205887251 U CN 205887251U
Authority
CN
China
Prior art keywords
mentioned
rotary shaft
gas bearing
main shaft
rotation axis
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.)
Expired - Fee Related
Application number
CN201620543026.5U
Other languages
Chinese (zh)
Inventor
高桥淳
小林直也
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.)
NSK Ltd
Original Assignee
NSK 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 NSK Ltd filed Critical NSK Ltd
Priority to CN201620543026.5U priority Critical patent/CN205887251U/en
Application granted granted Critical
Publication of CN205887251U publication Critical patent/CN205887251U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides a main shaft device, it becomes the flat constitution that axial length is short, can realize miniaturizedly and the lightweight. This main shaft device has: the rotation axis, its within range at the circumferencial direction is equipped with a plurality of turbine blade, the casing, it accomodates this rotation axis, and gas bearing, it is installed on this casing, the supply of passing through gases and for above -mentioned casing with the mode of non -contact with above -mentioned rotation axis floating bearing, above -mentioned a plurality of turbine blade are for above -mentioned gas bearing and dispose in radial inboard, and overlap in the axial with this gas bearing, through making above -mentioned rotation axis rotary driving to a plurality of turbine blade jet gas of the aforesaid, above -mentioned main shaft device's characterized in that, when establishing above -mentioned casing into L in the ascending length of axle of above -mentioned rotation axis, and when establishing the length on the width direction of above -mentioned casing into D, < D's mode forms with L, and be equipped with the workpiece setting portion that supplies workpiece setting on above -mentioned rotation axis, above -mentioned workpiece setting portion overlaps in the axial with this gas bearing.

Description

Main shaft device
Technical field
This utility model is related to main shaft device, relates more specifically to preferably use the main shaft dress in electrostatic sprayer Put.
Background technology
In the past, knew such main shaft as Patent Document 1 as the main shaft device being used in electrostatic sprayer Device.This main shaft device has: rotary shaft, and it is provided with cup on axial one end, and sets on axial the other end There are multiple turbo blades;The housing interting for rotary shaft;With the crust of the device of storage case, by multiple turbo blades injection Gas and make rotary shaft rotate.In addition, electrostatic sprayer is equipped on to use on multi-joint mechanical arm mostly.In addition, this rotation Axle is radially rotatably supported by by the gas bearing being arranged on housing.And, rotary shaft passes through following magnetic Balance between power and counter-force and be supported by along thrust direction, wherein, magnetic force be to be attracted by the Magnet installed on housing convex The power of edge, this counter-force is to power during flange part gas injection by gas bearing.But, in main shaft as patent documentation 1 In device, the axial one end being provided with the rotary shaft of cup extends very long from flange part in the axial direction.Thus, work as rotation During axle high-speed rotation, the whirling of rotary shaft becomes big, and, the resonant frequency of rotary shaft low it is therefore desirable to for dangerous speed Spend and take some countermeasures.
Patent documentation
Patent documentation 1: Japanese Unexamined Patent Publication 2006-77797 Japanese Laid Open Patent
Utility model content
In order to solve above-mentioned problem, this utility model provides a kind of main shaft device, has: rotary shaft, it is in circumferencial direction In the range of be provided with multiple turbo blades;Housing, it receives this rotary shaft;And gas bearing, it is installed on the housing, passes through The supply of gas and with respect to above-mentioned housing in a non-contact manner by above-mentioned rotary shaft floating support, above-mentioned multiple turbo blades Configure in radially inner side with respect to above-mentioned gas bearing, and overlapping in the axial direction with this gas bearing, by above-mentioned multiple Turbo blade gas injection and make above-mentioned rotary shaft rotation driving, above-mentioned main shaft device is characterised by, when above-mentioned housing exists Length in the axial direction of above-mentioned rotary shaft is set to l, and when the length on the width of above-mentioned housing is set to d, with l < d's Mode is formed, and is provided with the workpiece installation portion installed for workpiece, above-mentioned workpiece installation portion and this gas in above-mentioned rotary shaft Bearing is overlapping in the axial direction.
The effect of utility model
According to main shaft device of the present utility model, workpiece installation portion is overlapping in the axial direction with this gas bearing, thus, it is possible to Shorten the axial length of rotary shaft.Thereby, it is possible to reduce the whirling of rotary shaft, in addition, it is possible to increase the resonance of rotary shaft Frequency.In addition, multiple turbo blades configure with respect to gas bearing in radially inner side, therefore the rotation of rotary shaft when inertia Moment diminishes, and can reduce time when carrying out acceleration and deceleration.
Brief description
Fig. 1 is the sectional view representing main shaft device of the present utility model.
Specific embodiment
The main shaft device 10 of present embodiment has: rotary shaft 12, it is provided with multiple turbines in the range of circumferencial direction Blade 11;Housing 20, it receives this rotary shaft 12;Gas bearing 40, it is arranged on this housing 20, and by the supply of gas And with respect to above-mentioned housing in a non-contact manner by above-mentioned rotary shaft 12 floating support, above-mentioned multiple turbo blades 11 with respect to Above-mentioned gas bearing 40 and configure in radially inner side and overlapping in the axial direction with this gas bearing 40, by above-mentioned multiple whirlpools Impeller blade 11 gas injection and make the rotation driving of above-mentioned rotary shaft 12, this main shaft device is characterised by, when by above-mentioned housing 20 Length in the axial direction of above-mentioned rotary shaft 12 is set to l, and when the length on the width of above-mentioned housing 20 is set to d, with l The mode of < d is formed, and is provided with the workpiece installation portion 15 installed for workpiece, above-mentioned workpiece installation portion in above-mentioned rotary shaft 12 15 is overlapping in the axial direction with this gas bearing 40.
According to main shaft device of the present utility model, workpiece installation portion is overlapping in the axial direction with this gas bearing, thus, it is possible to Shorten the axial length of rotary shaft.Thereby, it is possible to reduce the whirling of rotary shaft, in addition, it is possible to increase the resonance of rotary shaft Frequency.In addition, multiple turbo blades configure being used in the rotation of radially inner side, therefore rotary shaft with respect to gas bearing 40 Property moment diminishes, and can reduce time when carrying out acceleration and deceleration.

Claims (1)

1. a kind of main shaft device, has:
Rotary shaft, it is provided with multiple turbo blades in the range of circumferencial direction;
Housing, it receives this rotary shaft;With
Gas bearing, it is installed on the housing, in a non-contact manner will with respect to described housing by the supply of gas Described rotary shaft floating support,
The plurality of turbo blade configures in radially inner side with respect to described gas bearing, and with this gas bearing in the axial direction Overlap, by making described rotary shaft rotation driving to the plurality of turbo blade gas injection, the feature of described main shaft device It is,
When by described housing, the length in the axial direction of described rotary shaft is set to l, and by the length on the width of described housing When degree is set to d, formed in the way of l < d, and the workpiece installation portion installed for workpiece is provided with described rotary shaft, described Workpiece installation portion is overlapping in the axial direction with this gas bearing.
CN201620543026.5U 2016-06-06 2016-06-06 Main shaft device Expired - Fee Related CN205887251U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620543026.5U CN205887251U (en) 2016-06-06 2016-06-06 Main shaft device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620543026.5U CN205887251U (en) 2016-06-06 2016-06-06 Main shaft device

Publications (1)

Publication Number Publication Date
CN205887251U true CN205887251U (en) 2017-01-18

Family

ID=57767554

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620543026.5U Expired - Fee Related CN205887251U (en) 2016-06-06 2016-06-06 Main shaft device

Country Status (1)

Country Link
CN (1) CN205887251U (en)

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20170118

Termination date: 20200606