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JPS63186932U - - Google Patents
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JPS63186932U - - Google Patents

Info

Publication number
JPS63186932U
JPS63186932U JP7685387U JP7685387U JPS63186932U JP S63186932 U JPS63186932 U JP S63186932U JP 7685387 U JP7685387 U JP 7685387U JP 7685387 U JP7685387 U JP 7685387U JP S63186932 U JPS63186932 U JP S63186932U
Authority
JP
Japan
Prior art keywords
turbine rotor
shaft
angle
rotational speed
variable
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
JP7685387U
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 JP7685387U priority Critical patent/JPS63186932U/ja
Publication of JPS63186932U publication Critical patent/JPS63186932U/ja
Pending legal-status Critical Current

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  • Supercharger (AREA)

Description

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

第1図は本考案の構成図、第2図、第3図は本
考案の実施例を示す構成断面図と側断面図、第4
図は制御内容を示すフローチヤート、第5図は作
動状態を示す説明図、第6図は本考案の他の実施
例を示すフローチヤート、第7図は従来例の断面
図である。 11……タービンロータ、12……コンプレツ
サ、13……シヤフト、15……軸受孔、16…
…回転センサ、18……可変案内翼、20……ア
クチユエータ、21……制御回路。
Fig. 1 is a block diagram of the present invention, Figs. 2 and 3 are a sectional view and a side sectional view of the embodiment of the present invention, and Fig. 4 is a block diagram of the structure of the present invention.
5 is a flowchart showing the control contents, FIG. 5 is an explanatory diagram showing the operating state, FIG. 6 is a flowchart showing another embodiment of the present invention, and FIG. 7 is a sectional view of the conventional example. 11... Turbine rotor, 12... Compressor, 13... Shaft, 15... Bearing hole, 16...
... Rotation sensor, 18 ... Variable guide vane, 20 ... Actuator, 21 ... Control circuit.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] タービンロータとコンプレツサとを連結するシ
ヤフトを動圧形空気軸受により支持するようにし
たターボチヤージヤにおいて、前記シヤフトの回
転数を検出する手段と、タービンロータへのガス
流入角を可変とする流入角可変手段と、シヤフト
の回転数が所定値よりも低いときにタービンロー
タの駆動トルクを増加する方向に流入角可変手段
を駆動する制御手段とを設けたことを特徴とする
ターボチヤージヤ。
In a turbocharger in which a shaft connecting a turbine rotor and a compressor is supported by a hydrodynamic air bearing, means for detecting the rotational speed of the shaft and variable inflow angle means for varying the angle of gas inflow into the turbine rotor. and a control means for driving the inlet angle variable means in a direction to increase the drive torque of the turbine rotor when the rotational speed of the shaft is lower than a predetermined value.
JP7685387U 1987-05-22 1987-05-22 Pending JPS63186932U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7685387U JPS63186932U (en) 1987-05-22 1987-05-22

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7685387U JPS63186932U (en) 1987-05-22 1987-05-22

Publications (1)

Publication Number Publication Date
JPS63186932U true JPS63186932U (en) 1988-11-30

Family

ID=30924315

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7685387U Pending JPS63186932U (en) 1987-05-22 1987-05-22

Country Status (1)

Country Link
JP (1) JPS63186932U (en)

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