JPH0191043U - - Google Patents
Info
- Publication number
- JPH0191043U JPH0191043U JP18626587U JP18626587U JPH0191043U JP H0191043 U JPH0191043 U JP H0191043U JP 18626587 U JP18626587 U JP 18626587U JP 18626587 U JP18626587 U JP 18626587U JP H0191043 U JPH0191043 U JP H0191043U
- Authority
- JP
- Japan
- Prior art keywords
- auxiliary
- turbine
- compressor
- turbo
- engine
- 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.)
- Pending
Links
- 230000008878 coupling Effects 0.000 claims 2
- 238000010168 coupling process Methods 0.000 claims 2
- 238000005859 coupling reaction Methods 0.000 claims 2
Landscapes
- Supercharger (AREA)
Description
第１図は本考案の一実施例としての複段式ター
ボ装置を示す模式的断面図であり、第２図は従来
のターボ装置を示す模式的断面図である。
１……タービン、２……連結軸、３……コンプ
レツサ、４……補助タービン、５……内部連結軸
、６……補助コンプレツサ、７……ベアリング、
８……タービンケーシング、９……コンプレツサ
ケーシング。
FIG. 1 is a schematic sectional view showing a multi-stage turbo device as an embodiment of the present invention, and FIG. 2 is a schematic sectional view showing a conventional turbo device. DESCRIPTION OF SYMBOLS 1... Turbine, 2... Connection shaft, 3... Compressor, 4... Auxiliary turbine, 5... Internal connection shaft, 6... Auxiliary compressor, 7... Bearing,
8... Turbine casing, 9... Compressor casing.
Claims (1)
作動するタービンと、同タービンに連結軸を介し
直結されて上記エンジンの給気系に介装されたコ
ンプレツサとをそなえたターボ装置において、上
記連結軸内に回転可能に配設された内部連結軸と
、同内部連結軸の一端に固着されて上記排気系に
介装された補助タービンと、上記内部連結軸の他
端に固着されて上記給気系に介装された補助コン
プレツサとからなる補助ターボ機構が設けられ、
上記の補助タービンおよび補助コンプレツサが、
それぞれ上記のタービンおよびコンプレツサより
も小さい回転慣性を有していることを特徴とする
、複段式ターボ装置。 In a turbo device comprising a turbine installed in an exhaust system of an engine and operated by exhaust gas, and a compressor directly connected to the turbine via a connecting shaft and installed in an air supply system of the engine, the connecting shaft an auxiliary turbine fixed to one end of the internal coupling shaft and interposed in the exhaust system; and an auxiliary turbine fixed to the other end of the internal coupling shaft and connected to the air supply system. An auxiliary turbo mechanism consisting of an auxiliary compressor installed in the system is provided,
The above auxiliary turbine and auxiliary compressor are
Multi-stage turbo arrangement, characterized in that it has a rotational inertia smaller than each of the above-mentioned turbines and compressors.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP18626587U JPH0191043U (en) | 1987-12-07 | 1987-12-07 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP18626587U JPH0191043U (en) | 1987-12-07 | 1987-12-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0191043U true JPH0191043U (en) | 1989-06-15 |
Family
ID=31477497
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP18626587U Pending JPH0191043U (en) | 1987-12-07 | 1987-12-07 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0191043U (en) |
-
1987
- 1987-12-07 JP JP18626587U patent/JPH0191043U/ja active Pending
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