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JPS60162223U - Variable nozzle mechanism in exhaust turbine - Google Patents

Variable nozzle mechanism in exhaust turbine

Info

Publication number
JPS60162223U
JPS60162223U JP4987784U JP4987784U JPS60162223U JP S60162223 U JPS60162223 U JP S60162223U JP 4987784 U JP4987784 U JP 4987784U JP 4987784 U JP4987784 U JP 4987784U JP S60162223 U JPS60162223 U JP S60162223U
Authority
JP
Japan
Prior art keywords
nozzle
turbine
partition plate
exhaust turbine
nozzle mechanism
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
Application number
JP4987784U
Other languages
Japanese (ja)
Other versions
JPH0121146Y2 (en
Inventor
榊田 勝
正三 清水
暢宏 近藤
Original Assignee
石川島播磨重工業株式会社
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 石川島播磨重工業株式会社 filed Critical 石川島播磨重工業株式会社
Priority to JP4987784U priority Critical patent/JPS60162223U/en
Publication of JPS60162223U publication Critical patent/JPS60162223U/en
Application granted granted Critical
Publication of JPH0121146Y2 publication Critical patent/JPH0121146Y2/ja
Granted legal-status Critical Current

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Landscapes

  • Supercharger (AREA)
  • Control Of Turbines (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【図面の簡単な説明】[Brief explanation of drawings]

第1図は排気ガスタービン過給機のタービンをその回転
軸に直角な面で切断した断面図、第2図は排気ガスター
ビン過給機のタービンをその回転軸を通る面で切断した
断面図で、aは1つ口形タービン渦巻室を有するもの、
bは2つ口形タービン渦巻室を有するもの、第3図はこ
の考案の一実施例を示す図で、回転軸に直角な面で切断
した断面図、第4図は第3図の排気ガスタービン過給機
を回転軸を通る平面で切断した断面図、第5図はノズル
14の動作を説明するための第3図の一部拡大図、第6
図はこの考案の他の実施例を示すノズル14の拡大図で
ある。 10・・・・・・タービン車室(渦巻室)、11・・・
・・・隔壁、12−−−−−−タービンインペラ、14
・・・・・・ノズル、16・・・・・・シールリング、
18・・・・・・ノズル仕切板、19,22,28・・
・・・・ピン、20,30・・・・・・摺動孔、26・
・・・・・ロッド。
Figure 1 is a cross-sectional view of the turbine of an exhaust gas turbine supercharger taken along a plane perpendicular to its rotation axis, and Figure 2 is a cross-sectional view of the exhaust gas turbine supercharger turbine taken along a plane passing through its rotation axis. , a has a single-mouthed turbine volute chamber,
b is a two-necked turbine with a spiral chamber; FIG. 3 is a cross-sectional view taken along a plane perpendicular to the rotational axis; FIG. 4 is the exhaust gas turbine of FIG. 3; 5 is a cross-sectional view of the supercharger taken along a plane passing through the rotation axis; FIG. 5 is a partially enlarged view of FIG. 3 for explaining the operation of the nozzle 14; and FIG.
The figure is an enlarged view of a nozzle 14 showing another embodiment of this invention. 10...Turbine casing (vortex chamber), 11...
... Bulkhead, 12---Turbine impeller, 14
...Nozzle, 16...Seal ring,
18... Nozzle partition plate, 19, 22, 28...
...Pin, 20, 30...Sliding hole, 26.
·····rod.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 2つ口形タービン車室を有し、ノズル仕切板を挾んでそ
の両側にノズルを配したタービン過給機において、前記
ノズル仕切板をタービンインペラの周りに回転可能に支
持すると共に、前記ノズルを前記ノズル仕切板とタービ
ン車室の固定部分の相互にずらした位置でそれぞれ支持
し、前記ノズル仕切板を回転させることにより、前記ノ
ズルの角度を可変するようにしたことを特徴とする排気
タービンにおける可変ノズル機構。
In a turbine supercharger having a two-necked turbine casing and having nozzles arranged on both sides of a nozzle partition plate, the nozzle partition plate is rotatably supported around a turbine impeller, and the nozzle is arranged in the A variable exhaust turbine characterized in that a nozzle partition plate and a fixed part of a turbine casing are respectively supported at mutually shifted positions, and the angle of the nozzle is varied by rotating the nozzle partition plate. Nozzle mechanism.
JP4987784U 1984-04-05 1984-04-05 Variable nozzle mechanism in exhaust turbine Granted JPS60162223U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4987784U JPS60162223U (en) 1984-04-05 1984-04-05 Variable nozzle mechanism in exhaust turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4987784U JPS60162223U (en) 1984-04-05 1984-04-05 Variable nozzle mechanism in exhaust turbine

Publications (2)

Publication Number Publication Date
JPS60162223U true JPS60162223U (en) 1985-10-28
JPH0121146Y2 JPH0121146Y2 (en) 1989-06-23

Family

ID=30567471

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4987784U Granted JPS60162223U (en) 1984-04-05 1984-04-05 Variable nozzle mechanism in exhaust turbine

Country Status (1)

Country Link
JP (1) JPS60162223U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62141636U (en) * 1986-02-28 1987-09-07
KR101070907B1 (en) * 2004-10-09 2011-10-06 삼성테크윈 주식회사 Turbine having variable vane

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62141636U (en) * 1986-02-28 1987-09-07
KR101070907B1 (en) * 2004-10-09 2011-10-06 삼성테크윈 주식회사 Turbine having variable vane

Also Published As

Publication number Publication date
JPH0121146Y2 (en) 1989-06-23

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