JPS6247796U - - Google Patents

Info

Publication number
JPS6247796U
JPS6247796U JP13868185U JP13868185U JPS6247796U JP S6247796 U JPS6247796 U JP S6247796U JP 13868185 U JP13868185 U JP 13868185U JP 13868185 U JP13868185 U JP 13868185U JP S6247796 U JPS6247796 U JP S6247796U
Authority
JP
Japan
Prior art keywords
multiple stages
rotor
utility
integrally formed
scope
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
JP13868185U
Other languages
English (en)
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 JP13868185U priority Critical patent/JPS6247796U/ja
Publication of JPS6247796U publication Critical patent/JPS6247796U/ja
Pending legal-status Critical Current

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Description

【図面の簡単な説明】
第1図aは本考案の一実施例にかかるタービン
動翼の部分の断面図、第1図bはその側面図、第
2図は従来のターボ分子ポンプの一例の縦断面図
、第3図はその動翼の部分の断面図、第4図は同
じくそのロータ回転中の作用説明図、第5図は本
考案の一実施例のロータ回転中の作用説明図であ
る。 図面中、24は動翼、25はボス、26は羽根
、27はロータ、θは羽根角度である。

Claims (1)

    【実用新案登録請求の範囲】
  1. 同軸上に複数段配列されるタービン動翼におい
    て、同一の羽根角度を有する前記動翼を複数段ま
    とめて一体に成形してなることを特徴とするター
    ビン動翼。
JP13868185U 1985-09-12 1985-09-12 Pending JPS6247796U (ja)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13868185U JPS6247796U (ja) 1985-09-12 1985-09-12

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13868185U JPS6247796U (ja) 1985-09-12 1985-09-12

Publications (1)

Publication Number Publication Date
JPS6247796U true JPS6247796U (ja) 1987-03-24

Family

ID=31043881

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13868185U Pending JPS6247796U (ja) 1985-09-12 1985-09-12

Country Status (1)

Country Link
JP (1) JPS6247796U (ja)

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