CN202616914U - Bidirectional tapered roller thrust bearing device of direct drive type electrically excited wind generator - Google Patents
Bidirectional tapered roller thrust bearing device of direct drive type electrically excited wind generator Download PDFInfo
- Publication number
- CN202616914U CN202616914U CN 201220214207 CN201220214207U CN202616914U CN 202616914 U CN202616914 U CN 202616914U CN 201220214207 CN201220214207 CN 201220214207 CN 201220214207 U CN201220214207 U CN 201220214207U CN 202616914 U CN202616914 U CN 202616914U
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- tapered roller
- bearing device
- thrust bearing
- roller
- shaft seat
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Abstract
The utility model relates to a bidirectional tapered roller thrust bearing device of a direct drive type electrically excited wind generator. The bidirectional tapered roller thrust bearing device comprises a fixed shaft seat, a rotary shaft seat, a cylindrical roller, and a tapered roller, wherein the cylindrical roller is mounted in the fixed shaft seat, the tapered roller is mounted on the rotary shaft seat, and matched with the cylindrical roller, the rotary shaft seat is fixedly connected with a rotor, and the fixed shaft seat is fixedly connected with a stator. The fixed shaft seat is formed by fixedly connecting two same fixed shaft seat blocks. Compared with the prior art, the bidirectional tapered roller thrust bearing device has the following advantages and effects: the structure of the bidirectional tapered roller thrust bearing device is simple and reasonable, the bearing can be assembled and disassembled, the tapered roller is in the tapered shape, the cylindrical roller is in the cylindrical shape, the bidirectional tapered roller thrust bearing structure is formed in the rotation process of the rotor, and the service life of the bearing is prolonged.
Description
Technical field
The utility model relates to a kind of direct-driving electric excitation wind-driven generator bidirectional thrust tapered roller bearing device.
Background technology
Design and installation has stator and rotor in the wind-driven generator; Be to rely on the energy of wind to make the rotor rotation realize the conversion of wind-powered electricity generation energy, in long rotor rotation process, the blast rotation of rotor will inevitably have pressure to bearing; Can produce bearing heating, influence bearing useful life.The prior art wind-driven generator does not design tapered roller bearing device, and its defective is general bearing in rotor rotation process for a long time, and the bear rotor rotational pressure is big, bearing heating, and what influence bearing influences bearing useful life.
The utility model content
The technical problem of the required solution of the utility model is to overcome existing above-mentioned deficiency in the prior art, and provides a kind of simple for structure, the direct-driving electric excitation wind-driven generator bidirectional thrust tapered roller bearing device of long service life.
The utility model solves the problems of the technologies described above and the technical scheme that adopts: a kind of direct-driving electric excitation wind-driven generator bidirectional thrust tapered roller bearing device; It is characterized in that being provided with fixedly axle bed, rotating shaft base, cylindrical roller, taper roller; Cylindrical roller fixedly is installed in the axle bed, taper roller is installed on the rotating shaft base, cylindrical roller and taper roller are complementary; Rotating shaft base is fixedly connected with rotor, and fixedly axle bed is fixedly connected with stator.
The said fixedly axle bed of the utility model is formed by fixedly connecting two identical fixed axis saddles.
The utility model compared with prior art has the following advantages and effect: simple for structure rationally, bearing body can installing/dismounting; Taper roller is cone; Cylindrical roller is cylinder, in rotor rotation process, forms the two-direction thrust bearing structure, prolongs bearing useful life.
Description of drawings
Fig. 1 is the scheme of installation of the utility model embodiment.
Embodiment
Referring to Fig. 1; The utility model embodiment direct-driving electric excitation wind-driven generator bidirectional thrust tapered roller bearing device is provided with fixedly axle bed 5, rotating shaft base 6, cylindrical roller 7, taper roller 8; Fixedly in the axle bed 5 (clamping) cylindrical roller 7 is installed, taper roller 8 is installed on the rotating shaft base 6, cylindrical roller 7 fits like a glove in bearing body with taper roller 8 and is complementary; Form tapered roller bearing device; Tapered roller bearing device snaps between rotor 2 and the stator 3, and rotating shaft base 6 usefulness bolts and rotor 2 are tightened fixing, and two fixedly axle bed 5 usefulness bolts and stator 3 are tightened fixing.
The described bearing body of present embodiment can installing/dismounting, and said fixedly axle bed 5 is formed by fixedly connecting two identical fixed axis saddles, is easy for installation and removal.
The described taper roller 8 of present embodiment is cone, and cylindrical roller 7 is cylinder, in rotor 2 rotary courses, forms the two-direction thrust bearing structure; Cylindrical roller 7 fits like a glove in bearing body with taper roller 8 and is complementary, under the effect of cylindrical roller 7, taper roller 8, and the blast rotational pressure of ability bear rotor 2; Because taper roller 8 has pyramidal structure with bearing body; Make that the linear velocity of roller end face is consistent, avoided the friction of roller and bearing body, prolonged bearing useful life.
The direct-driving electric excitation wind-driven generator is a prior art, can comprise main frame 1, rotor 2, stator 3, and rotor 2 is installed in the main frame 1 with stator 3.
Simple deformation of every the utility model or equivalent transformation should be thought the protection range that falls into the utility model.
Claims (2)
1. direct-driving electric excitation wind-driven generator bidirectional thrust tapered roller bearing device; It is characterized in that: be provided with fixedly axle bed, rotating shaft base, cylindrical roller, taper roller; Cylindrical roller fixedly is installed in the axle bed, taper roller is installed on the rotating shaft base, cylindrical roller and taper roller are complementary; Rotating shaft base is fixedly connected with rotor, and fixedly axle bed is fixedly connected with stator.
2. direct-driving electric excitation wind-driven generator bidirectional thrust tapered roller bearing device according to claim 1 is characterized in that: said fixedly axle bed is formed by fixedly connecting two identical fixed axis saddles.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220214207 CN202616914U (en) | 2012-05-14 | 2012-05-14 | Bidirectional tapered roller thrust bearing device of direct drive type electrically excited wind generator |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220214207 CN202616914U (en) | 2012-05-14 | 2012-05-14 | Bidirectional tapered roller thrust bearing device of direct drive type electrically excited wind generator |
Publications (1)
Publication Number | Publication Date |
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CN202616914U true CN202616914U (en) | 2012-12-19 |
Family
ID=47350584
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN 201220214207 Expired - Fee Related CN202616914U (en) | 2012-05-14 | 2012-05-14 | Bidirectional tapered roller thrust bearing device of direct drive type electrically excited wind generator |
Country Status (1)
Country | Link |
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CN (1) | CN202616914U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105784245A (en) * | 2014-12-17 | 2016-07-20 | 中国航空工业集团公司沈阳发动机设计研究所 | Thermal deformation-discordant single-rotor double-thrust bearing axial force testing method |
-
2012
- 2012-05-14 CN CN 201220214207 patent/CN202616914U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105784245A (en) * | 2014-12-17 | 2016-07-20 | 中国航空工业集团公司沈阳发动机设计研究所 | Thermal deformation-discordant single-rotor double-thrust bearing axial force testing method |
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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 |
Granted publication date: 20121219 Termination date: 20190514 |
|
CF01 | Termination of patent right due to non-payment of annual fee |