JPS6319093U - - Google Patents
Info
- Publication number
- JPS6319093U JPS6319093U JP11217986U JP11217986U JPS6319093U JP S6319093 U JPS6319093 U JP S6319093U JP 11217986 U JP11217986 U JP 11217986U JP 11217986 U JP11217986 U JP 11217986U JP S6319093 U JPS6319093 U JP S6319093U
- Authority
- JP
- Japan
- Prior art keywords
- rotor
- seal
- housing
- pressure
- rotating machine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Landscapes
- Control Of Positive-Displacement Air Blowers (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
Description
第1図は、本考案の一実施例であるスラスト力
調整機構をターボ・コンプレツサに利用したもの
の概略断面図を示す。第2図は、同図のスラスト
方向に作用する圧力の関係を概略図示したもので
ある。
1……ターボ・コンプレツサ(気体回転機械)
、4……ロータ、5……ハウジング、10……ラ
ビリンス・シール、12……圧力導入経路、A…
…受圧面。
FIG. 1 shows a schematic cross-sectional view of a turbo compressor using a thrust force adjustment mechanism according to an embodiment of the present invention. FIG. 2 schematically shows the relationship of pressure acting in the thrust direction in the same figure. 1...Turbo compressor (gas rotating machine)
, 4... Rotor, 5... Housing, 10... Labyrinth seal, 12... Pressure introduction path, A...
...Pressure receiving surface.
Claims (1)
とともにこのロータにハウジングとの間の隙間を
気密にするシールを設けてなる気体回転機械にお
いて、前記シールを設けたロータの途中にスラス
ト方向の受圧面をなす段差を形成するとともに、
該シールに臨む前記ハウジング内壁に圧力源から
前記ロータに掛るスラスト力に対抗する圧力を導
入するための圧力導入経路を設けたことを特徴と
する気体回転機械のスラスト力調整機構。 In a gas rotating machine in which a rotor is supported in a housing by a hydrodynamic gas bearing and a seal is provided on the rotor to make the gap between the rotor and the housing airtight, a pressure receiving surface in the thrust direction is provided in the middle of the rotor provided with the seal. In addition to forming a step,
A thrust force adjustment mechanism for a gas rotating machine, characterized in that a pressure introduction path for introducing pressure counteracting the thrust force applied to the rotor from a pressure source is provided on the inner wall of the housing facing the seal.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11217986U JPH0720399Y2 (en) | 1986-07-21 | 1986-07-21 | Turbo compressor thrust force adjustment mechanism |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11217986U JPH0720399Y2 (en) | 1986-07-21 | 1986-07-21 | Turbo compressor thrust force adjustment mechanism |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS6319093U true JPS6319093U (en) | 1988-02-08 |
JPH0720399Y2 JPH0720399Y2 (en) | 1995-05-15 |
Family
ID=30992807
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP11217986U Expired - Lifetime JPH0720399Y2 (en) | 1986-07-21 | 1986-07-21 | Turbo compressor thrust force adjustment mechanism |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0720399Y2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2003509633A (en) * | 1999-09-14 | 2003-03-11 | アトラス コプコ エアーパワー,ナームローゼ フェンノートシャップ | Radial-axial composite sliding bearing |
-
1986
- 1986-07-21 JP JP11217986U patent/JPH0720399Y2/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2003509633A (en) * | 1999-09-14 | 2003-03-11 | アトラス コプコ エアーパワー,ナームローゼ フェンノートシャップ | Radial-axial composite sliding bearing |
Also Published As
Publication number | Publication date |
---|---|
JPH0720399Y2 (en) | 1995-05-15 |
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