JPH01130034U - - Google Patents

Info

Publication number
JPH01130034U
JPH01130034U JP2502488U JP2502488U JPH01130034U JP H01130034 U JPH01130034 U JP H01130034U JP 2502488 U JP2502488 U JP 2502488U JP 2502488 U JP2502488 U JP 2502488U JP H01130034 U JPH01130034 U JP H01130034U
Authority
JP
Japan
Prior art keywords
air
line
bypass
supply
turbine
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
JP2502488U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP2502488U priority Critical patent/JPH01130034U/ja
Publication of JPH01130034U publication Critical patent/JPH01130034U/ja
Pending legal-status Critical Current

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  • Supercharger (AREA)

Description

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

第1図は本考案の過給機の給気バイパス装置の
一実施例を示す概要図、第2図はタービン側圧力
及びコンプレツサ側圧力とエンジン負荷との関係
を示す図、第3図は従来の過給機の給気バイパス
装置の概要図である。 1……過給機、2……タービン、3……コンプ
レツサ、4……エンジン、5……給気ライン、6
……排気ガスライン、7……バイパスライン、1
2……補助ブロワ、13……モータ。
Fig. 1 is a schematic diagram showing an example of an air supply bypass device for a supercharger according to the present invention, Fig. 2 is a diagram showing the relationship between turbine side pressure, compressor side pressure, and engine load, and Fig. 3 is a conventional FIG. 2 is a schematic diagram of an air supply bypass device for a supercharger. 1...Supercharger, 2...Turbine, 3...Compressor, 4...Engine, 5...Air supply line, 6
...Exhaust gas line, 7...Bypass line, 1
2...Auxiliary blower, 13...Motor.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] タービンとコンプレツサを備えた過給機を、排
気ガスライン及び給気ラインを介してエンジンに
接続し、且つ上記給気ラインの途中から取り出し
た給気の一部をバイパスラインでタービンの入口
側にバイパスさせるようにしてある過給機の給気
バイパス装置において、上記バイパスラインの途
中に、バイパスされる給気の圧力を上昇させるた
めの補助ブロワを組み込んでなることを特徴とす
る過給機の給気バイパス装置。
A supercharger equipped with a turbine and a compressor is connected to the engine via an exhaust gas line and an air supply line, and a portion of the air taken out from the middle of the air supply line is sent to the inlet side of the turbine through a bypass line. A supply air bypass device for a turbocharger configured to bypass the turbocharger, characterized in that an auxiliary blower is installed in the middle of the bypass line to increase the pressure of the supply air to be bypassed. Supply air bypass device.
JP2502488U 1988-02-29 1988-02-29 Pending JPH01130034U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2502488U JPH01130034U (en) 1988-02-29 1988-02-29

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2502488U JPH01130034U (en) 1988-02-29 1988-02-29

Publications (1)

Publication Number Publication Date
JPH01130034U true JPH01130034U (en) 1989-09-05

Family

ID=31245383

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2502488U Pending JPH01130034U (en) 1988-02-29 1988-02-29

Country Status (1)

Country Link
JP (1) JPH01130034U (en)

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