JPS6284629U - - Google Patents
Info
- Publication number
- JPS6284629U JPS6284629U JP17693285U JP17693285U JPS6284629U JP S6284629 U JPS6284629 U JP S6284629U JP 17693285 U JP17693285 U JP 17693285U JP 17693285 U JP17693285 U JP 17693285U JP S6284629 U JPS6284629 U JP S6284629U
- Authority
- JP
- Japan
- Prior art keywords
- turbine
- turbine mechanism
- driven
- turbocharger
- rotation speed
- 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
- 230000005540 biological transmission Effects 0.000 claims description 2
- 230000007423 decrease Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 2
Landscapes
- Supercharger (AREA)
Description
第1図はこの考案の第1の実施例に係わるター
ボチヤージヤの概略的全体構成図、第2図は第2
の実施例の概略的全体構成図、第3図は第3の実
施例の概略的全体構成図である。
3……コンプレツサ、7……第1タービン、2
7……第2タービン、31……ワンウエイクラツ
チ(回転力伝達手段)。
FIG. 1 is a schematic overall configuration diagram of a turbocharger according to a first embodiment of this invention, and FIG.
FIG. 3 is a schematic overall configuration diagram of the third embodiment. 3... Compressor, 7... First turbine, 2
7...Second turbine, 31...One-way clutch (rotational force transmission means).
Claims (1)
ービン機構と、この第1のタービン機構に連動す
るコンプレツサとを有するターボチヤージヤにお
いて、前記コンプレツサによる過給圧が所定圧を
越えたとき前記排気エネルギによつて駆動しかつ
前記第1のタービンより回転慣性力の大きい第2
のタービン機構と、前記第1のタービン機構の回
転数が前記第2のタービン機構の回転数に略等し
くなるまで低下したとき前記第2のタービン機構
の回転力を前記第1のタービン機構に伝達する回
転力伝達手段とを有することを特徴とするターボ
チヤージヤ。 In a turbocharger having a first turbine mechanism driven by engine exhaust energy and a compressor linked to the first turbine mechanism, when boost pressure by the compressor exceeds a predetermined pressure, the turbocharger is driven by the exhaust energy. a second turbine which is driven by the turbine and has a larger rotational inertia than the first turbine;
a turbine mechanism, and transmitting the rotational force of the second turbine mechanism to the first turbine mechanism when the rotation speed of the first turbine mechanism decreases to approximately equal to the rotation speed of the second turbine mechanism. A turbocharger characterized by having a rotational force transmission means.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP17693285U JPS6284629U (en) | 1985-11-19 | 1985-11-19 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP17693285U JPS6284629U (en) | 1985-11-19 | 1985-11-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6284629U true JPS6284629U (en) | 1987-05-29 |
Family
ID=31117653
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP17693285U Pending JPS6284629U (en) | 1985-11-19 | 1985-11-19 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6284629U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0411219U (en) * | 1990-05-17 | 1992-01-30 |
-
1985
- 1985-11-19 JP JP17693285U patent/JPS6284629U/ja active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0411219U (en) * | 1990-05-17 | 1992-01-30 |
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