JPS59142402U - Turbomachinery impeller structure - Google Patents

Turbomachinery impeller structure

Info

Publication number
JPS59142402U
JPS59142402U JP3663683U JP3663683U JPS59142402U JP S59142402 U JPS59142402 U JP S59142402U JP 3663683 U JP3663683 U JP 3663683U JP 3663683 U JP3663683 U JP 3663683U JP S59142402 U JPS59142402 U JP S59142402U
Authority
JP
Japan
Prior art keywords
back plate
blade wheel
ring
boss portion
attached
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.)
Granted
Application number
JP3663683U
Other languages
Japanese (ja)
Other versions
JPS6311282Y2 (en
Inventor
嶋北 正俊
Original Assignee
三菱重工業株式会社
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 三菱重工業株式会社 filed Critical 三菱重工業株式会社
Priority to JP3663683U priority Critical patent/JPS59142402U/en
Publication of JPS59142402U publication Critical patent/JPS59142402U/en
Application granted granted Critical
Publication of JPS6311282Y2 publication Critical patent/JPS6311282Y2/ja
Granted legal-status Critical Current

Links

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) [Abstract] 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 the drawing]

第1.2図は従来のターボ機械の翼車構造を示すもので
、第1図はその上半部の縦断面図、第2図はその背板の
変形を示す部分断面図であり、第3〜5図はいずれも本
考案の実施例としてのターボ機械の翼車取付構造であっ
て第3.4図は本考案の第1実施例としてのターボ機械
の翼車構造を示すもので、第3図はその横断面図、第4
図は第゛3図のIV−IV矢視断面図であり、第5図は
第4図に対応させて本考案の第2実施例としてのターボ
機械の翼車構造の要部を示す縦断面図である。 1・・・・・・主軸、2・・・・・・翼車、2a・・・
・・・翼車のリング状支持部、2b・・・・・・翼車の
ピン孔、6・・・・・・背板、6a・・・・・・背板の
リング状ボス部、6b・・・・・・背板のピン孔、27
・・・・・・ラジアルピン、28・・・・・・抜は止め
ピン、29・・・・・・0リング、31・・・・・・接
合面。
Figure 1.2 shows the blade wheel structure of a conventional turbomachine. Figure 1 is a vertical sectional view of its upper half, Figure 2 is a partial sectional view showing the deformation of its back plate, and Figures 3 to 5 all show the blade wheel mounting structure of a turbo machine as an embodiment of the present invention, and Figures 3 and 4 show the blade wheel structure of a turbo machine as a first embodiment of the present invention. Figure 3 is its cross-sectional view, Figure 4
The figure is a sectional view taken along the line IV-IV in FIG. 3, and FIG. It is a diagram. 1... main shaft, 2... impeller, 2a...
...Ring-shaped support part of the impeller, 2b... Pin hole of the impeller, 6... Back plate, 6a... Ring-shaped boss part of the back plate, 6b・・・・・・Pin hole on back plate, 27
... Radial pin, 28 ... Removal stop pin, 29 ... 0 ring, 31 ... Joint surface.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] ターボ機械の主軸に固着された翼車ボス部と、同翼車ボ
ス部に装着された背板と、同背板に取付けられた翼とを
そなえ、上記背板に形成されたリング状ボス部の内周が
、上記翼車ボス部の円周部の外周に支持されて、上記の
翼車ボス部と背板とを一体に回転させるようにしながら
、上記背板のリング状ボス部の拡径方向への変形を許容
すべく、上記翼車ボス部の円周部に装着された半径方向
のピンが、上記背板のリング状ボス部に形成されたピン
孔に挿通されていることを特徴とする、ターボ機械の翼
車構造。
A ring-shaped boss portion formed on the back plate, comprising a blade wheel boss portion fixed to the main shaft of the turbomachine, a back plate attached to the blade wheel boss portion, and a blade attached to the back plate. The inner periphery of the ring-shaped boss of the back plate is supported by the outer periphery of the circumferential part of the blade wheel boss, and the ring-shaped boss of the back plate is expanded while rotating the blade wheel boss and the back plate together. In order to allow deformation in the radial direction, a radial pin attached to the circumferential portion of the blade wheel boss portion is inserted into a pin hole formed in the ring-shaped boss portion of the back plate. Features a turbomachinery blade wheel structure.
JP3663683U 1983-03-14 1983-03-14 Turbomachinery impeller structure Granted JPS59142402U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3663683U JPS59142402U (en) 1983-03-14 1983-03-14 Turbomachinery impeller structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3663683U JPS59142402U (en) 1983-03-14 1983-03-14 Turbomachinery impeller structure

Publications (2)

Publication Number Publication Date
JPS59142402U true JPS59142402U (en) 1984-09-22
JPS6311282Y2 JPS6311282Y2 (en) 1988-04-02

Family

ID=30167301

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3663683U Granted JPS59142402U (en) 1983-03-14 1983-03-14 Turbomachinery impeller structure

Country Status (1)

Country Link
JP (1) JPS59142402U (en)

Also Published As

Publication number Publication date
JPS6311282Y2 (en) 1988-04-02

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