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JPS6010835U - axial turbine turbocharger - Google Patents

axial turbine turbocharger

Info

Publication number
JPS6010835U
JPS6010835U JP10189583U JP10189583U JPS6010835U JP S6010835 U JPS6010835 U JP S6010835U JP 10189583 U JP10189583 U JP 10189583U JP 10189583 U JP10189583 U JP 10189583U JP S6010835 U JPS6010835 U JP S6010835U
Authority
JP
Japan
Prior art keywords
flow path
axial turbine
nozzle
compressor
valve
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
Application number
JP10189583U
Other languages
Japanese (ja)
Inventor
健 三堀
倉沢 稔
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 JP10189583U priority Critical patent/JPS6010835U/en
Publication of JPS6010835U publication Critical patent/JPS6010835U/en
Pending legal-status Critical Current

Links

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 the drawing]

第1図は従来のディーゼル機関用過給機の一例を示す軸
流タービン部の切断正面図、第2図は本考案の一実施例
を示す切断側面図、第3図は第2図のm−m矢視図であ
る。 1はディーゼルエンジン、3は軸流タービン、4はター
ビン翼車、5は軸、6はブロワ扇車、7はコンプレッサ
、9は仕切板、10は主ノズル、11は副ノズル、12
は仕切板、13は主流入路、14は副流入路、15はタ
ービンケーシング、18は仕切弁、20はエアーシリン
ダ、21は空気流路、22は作動流路、23はパイロッ
ト弁を  ・示す。
Fig. 1 is a cutaway front view of an axial flow turbine section showing an example of a conventional turbocharger for a diesel engine, Fig. 2 is a cutaway side view showing an embodiment of the present invention, and Fig. 3 is a -m arrow view. 1 is a diesel engine, 3 is an axial flow turbine, 4 is a turbine wheel, 5 is a shaft, 6 is a blower fan, 7 is a compressor, 9 is a partition plate, 10 is a main nozzle, 11 is a sub nozzle, 12
1 is a partition plate, 13 is a main inflow path, 14 is a sub-inflow path, 15 is a turbine casing, 18 is a gate valve, 20 is an air cylinder, 21 is an air flow path, 22 is an operating flow path, and 23 is a pilot valve. .

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 同心円状に内外側に区画したノズルと、該各区内したノ
ズルに別々に連通ずる流路を区画し且つその一方の流路
の開閉を行う開閉弁を内蔵したタービンケーシングと、
前記開閉弁の開閉作動を行うエアーシリンダと、該エア
ーシリンダとコンプレッサの出側空気流路とを接続する
作動流路と、該作動流路に設置したパイロット弁とを備
えたことを特徴とする軸流タービン過給機。
A turbine casing that includes a nozzle that is concentrically divided into inner and outer parts, and a built-in on-off valve that divides a flow path that communicates with each nozzle and opens and closes one of the flow paths;
The compressor is characterized by comprising an air cylinder that opens and closes the on-off valve, an operating flow path that connects the air cylinder and the outlet air flow path of the compressor, and a pilot valve installed in the operating flow path. Axial flow turbine supercharger.
JP10189583U 1983-06-30 1983-06-30 axial turbine turbocharger Pending JPS6010835U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10189583U JPS6010835U (en) 1983-06-30 1983-06-30 axial turbine turbocharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10189583U JPS6010835U (en) 1983-06-30 1983-06-30 axial turbine turbocharger

Publications (1)

Publication Number Publication Date
JPS6010835U true JPS6010835U (en) 1985-01-25

Family

ID=30240417

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10189583U Pending JPS6010835U (en) 1983-06-30 1983-06-30 axial turbine turbocharger

Country Status (1)

Country Link
JP (1) JPS6010835U (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5543289A (en) * 1978-09-15 1980-03-27 Maschf Augsburg Nuernberg Ag Device for altering cross section of turbine inlet passage of exhaust turbosupercharger
JPS5593923A (en) * 1979-01-10 1980-07-16 Hitachi Ltd Exhaust bypass type turbo-charger

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5543289A (en) * 1978-09-15 1980-03-27 Maschf Augsburg Nuernberg Ag Device for altering cross section of turbine inlet passage of exhaust turbosupercharger
JPS5593923A (en) * 1979-01-10 1980-07-16 Hitachi Ltd Exhaust bypass type turbo-charger

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