JPS62200134U - - Google Patents
Info
- Publication number
- JPS62200134U JPS62200134U JP8819786U JP8819786U JPS62200134U JP S62200134 U JPS62200134 U JP S62200134U JP 8819786 U JP8819786 U JP 8819786U JP 8819786 U JP8819786 U JP 8819786U JP S62200134 U JPS62200134 U JP S62200134U
- Authority
- JP
- Japan
- Prior art keywords
- pressure stage
- turbine chamber
- turbine
- stage compression
- chamber
- 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
- 230000006835 compression Effects 0.000 claims description 12
- 238000007906 compression Methods 0.000 claims description 12
- 238000010586 diagram Methods 0.000 description 1
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
第１図は本考案の一実施例を示す断面図、第２
図は従来の２軸２段圧縮２段膨張型のターボコン
プレツサを概略的に示す構成図である。
図中、１はケーシング、２は駆動タービン室、
５は低圧段圧縮タービン室、６は高圧段圧縮ター
ビン室、７は駆動タービン、８は低圧段圧縮ター
ビン、９は高圧段圧縮タービン、１０は共通軸、
２３はラジシル軸受である。
Fig. 1 is a sectional view showing one embodiment of the present invention;
The figure is a schematic configuration diagram of a conventional two-shaft, two-stage compression, two-stage expansion type turbo compressor. In the figure, 1 is a casing, 2 is a drive turbine chamber,
5 is a low pressure stage compression turbine chamber, 6 is a high pressure stage compression turbine chamber, 7 is a drive turbine, 8 is a low pressure stage compression turbine, 9 is a high pressure stage compression turbine, 10 is a common shaft,
23 is a radisil bearing.
Claims (1)
の一側部に低圧段圧縮タービン室を、その他側部
に高圧段圧縮タービン室を同軸心状に形成し、低
圧段圧縮タービン室に収納した低圧段圧縮タービ
ン、駆動タービン室に収納した駆動タービン、及
び高圧段圧縮タービン室に収納した高圧段圧縮タ
ービンを共通軸で連結し、この共通軸とケーシン
グとの間に介在させたラジアル軸受が、低圧段圧
縮タービンと駆動タービン室との間、及び駆動タ
ービン室と高圧段圧縮タービン室との間に配置さ
れていることを特徴とするターボコンプレツサ。 A drive turbine chamber is formed in the center of the casing, a low-pressure stage compression turbine chamber is formed on one side of the casing, and a high-pressure stage compression turbine chamber is formed coaxially on the other side. The compression turbine, the drive turbine housed in the drive turbine chamber, and the high-pressure stage compression turbine housed in the high-pressure stage compression turbine chamber are connected by a common shaft, and a radial bearing interposed between the common shaft and the casing connects the low-pressure stage compressor turbine. A turbo compressor characterized in that it is disposed between a compression turbine and a drive turbine chamber, and between a drive turbine chamber and a high-pressure stage compression turbine chamber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8819786U JPH0437232Y2 (en) | 1986-06-10 | 1986-06-10 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8819786U JPH0437232Y2 (en) | 1986-06-10 | 1986-06-10 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS62200134U true JPS62200134U (en) | 1987-12-19 |
| JPH0437232Y2 JPH0437232Y2 (en) | 1992-09-02 |
Family
ID=30946092
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP8819786U Expired JPH0437232Y2 (en) | 1986-06-10 | 1986-06-10 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0437232Y2 (en) |
-
1986
- 1986-06-10 JP JP8819786U patent/JPH0437232Y2/ja not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0437232Y2 (en) | 1992-09-02 |
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