JPS63191242U - - Google Patents

Info

Publication number
JPS63191242U
JPS63191242U JP11129987U JP11129987U JPS63191242U JP S63191242 U JPS63191242 U JP S63191242U JP 11129987 U JP11129987 U JP 11129987U JP 11129987 U JP11129987 U JP 11129987U JP S63191242 U JPS63191242 U JP S63191242U
Authority
JP
Japan
Prior art keywords
turbine wheel
inlet passage
exhaust gas
outer periphery
piece
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
JP11129987U
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 JP11129987U priority Critical patent/JPS63191242U/ja
Publication of JPS63191242U publication Critical patent/JPS63191242U/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図は本考案の第1実施例を示す断面図、第
2図は第1図の要部を拡大して示す側面図、第3
図は第2実施例の要部を拡大して示す側面図、第
4図は第3実施例の要部を拡大して示す側面図、
第5図は第4実施例の要部を拡大して示す側面図
、第6図は第5実施例を示す断面図である。 11……タービンホイル、12……タービンハ
ウジング、16……入口通路、18……内壁、2
1……外周縁部、22,32……脆弱片部。
Fig. 1 is a sectional view showing a first embodiment of the present invention, Fig. 2 is a side view showing an enlarged main part of Fig. 1, and Fig. 3 is a side view showing a main part of Fig.
The figure is a side view showing an enlarged main part of the second embodiment, FIG. 4 is a side view showing an enlarged main part of a third embodiment,
FIG. 5 is a side view showing an enlarged main part of the fourth embodiment, and FIG. 6 is a sectional view showing the fifth embodiment. DESCRIPTION OF SYMBOLS 11... Turbine foil, 12... Turbine housing, 16... Inlet passage, 18... Inner wall, 2
1...Outer peripheral edge portion, 22, 32...Fragile piece portion.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] タービンホイルの外周を渦巻状に囲繞する入口
通路が形成され、タービンホイルが、該入口通路
を流動する排気ガスにより回転駆動されるターボ
チヤージヤにおいて、上記タービンホイルの外周
縁部のうち上記入口通路内に臨む部分に脆弱片部
を設け、該脆弱片部は排気ガス中の異物の衝突に
よりタービンホイルとタービンハウジング内壁と
の間の最小間隙よりも小さい片部となつて欠落す
ることを特徴とするターボチヤージヤ。
In a turbocharger in which an inlet passage spirally surrounds the outer periphery of a turbine wheel, and the turbine wheel is rotationally driven by exhaust gas flowing through the inlet passage, a part of the outer periphery of the turbine wheel is located within the inlet passage. A turbocharger characterized in that a fragile piece is provided in a facing portion, and the fragile piece becomes a piece smaller than the minimum gap between the turbine wheel and the inner wall of the turbine housing and breaks off due to collision of foreign matter in exhaust gas. .
JP11129987U 1987-01-31 1987-07-22 Pending JPS63191242U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11129987U JPS63191242U (en) 1987-01-31 1987-07-22

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP1221287 1987-01-31
JP11129987U JPS63191242U (en) 1987-01-31 1987-07-22

Publications (1)

Publication Number Publication Date
JPS63191242U true JPS63191242U (en) 1988-12-09

Family

ID=33454769

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11129987U Pending JPS63191242U (en) 1987-01-31 1987-07-22

Country Status (1)

Country Link
JP (1) JPS63191242U (en)

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