JPS58144031U - turbocharged engine - Google Patents

turbocharged engine

Info

Publication number
JPS58144031U
JPS58144031U JP4092182U JP4092182U JPS58144031U JP S58144031 U JPS58144031 U JP S58144031U JP 4092182 U JP4092182 U JP 4092182U JP 4092182 U JP4092182 U JP 4092182U JP S58144031 U JPS58144031 U JP S58144031U
Authority
JP
Japan
Prior art keywords
engine
compressor
turbocharged engine
driven
turbo supercharger
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
JP4092182U
Other languages
Japanese (ja)
Inventor
博 杉戸
糟谷 保
利彦 西山
Original Assignee
株式会社小松製作所
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 株式会社小松製作所 filed Critical 株式会社小松製作所
Priority to JP4092182U priority Critical patent/JPS58144031U/en
Publication of JPS58144031U publication Critical patent/JPS58144031U/en
Pending legal-status Critical Current

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  • Supercharger (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図はこの考案の一実施例を示すブロック図、第2図
aないしeは性能曲線図である。 1はエンビン、2は高圧側ターボ過給機、2aはタービ
ン、3は低圧側ターボ過給機、3bはコンプレッサ、6
はニアコンプレッサ。
FIG. 1 is a block diagram showing an embodiment of this invention, and FIGS. 2a to 2e are performance curve diagrams. 1 is an engine, 2 is a high pressure side turbocharger, 2a is a turbine, 3 is a low pressure side turbocharger, 3b is a compressor, 6
is the near compressor.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] エンジン1の排気に゛より駆動される高圧側ターボ過給
機2及び低圧側ターボ過給機3によりエンジン1を2段
過給するものにおいて、適宜駆動源により駆動されるニ
アコンプレッサ6を設け、このニアコンプレッサ6で加
圧されたエアを高圧側ターボ過給機2のタービン2a(
[1及び低圧側ターボ過給機3のコンプレッサ3b側へ
供給してなる一ターボ過給エンジン。
In a system in which the engine 1 is supercharged in two stages by a high-pressure turbo supercharger 2 and a low-pressure turbo supercharger 3 driven by the exhaust gas of the engine 1, a near compressor 6 driven by an appropriate drive source is provided, The air pressurized by this near compressor 6 is transferred to the turbine 2a (
[1 and a turbocharged engine supplied to the compressor 3b side of the low pressure side turbocharger 3.
JP4092182U 1982-03-25 1982-03-25 turbocharged engine Pending JPS58144031U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4092182U JPS58144031U (en) 1982-03-25 1982-03-25 turbocharged engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4092182U JPS58144031U (en) 1982-03-25 1982-03-25 turbocharged engine

Publications (1)

Publication Number Publication Date
JPS58144031U true JPS58144031U (en) 1983-09-28

Family

ID=30052119

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4092182U Pending JPS58144031U (en) 1982-03-25 1982-03-25 turbocharged engine

Country Status (1)

Country Link
JP (1) JPS58144031U (en)

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