JPS6052301U - axial flow turbomachinery - Google Patents
axial flow turbomachineryInfo
- Publication number
- JPS6052301U JPS6052301U JP13358883U JP13358883U JPS6052301U JP S6052301 U JPS6052301 U JP S6052301U JP 13358883 U JP13358883 U JP 13358883U JP 13358883 U JP13358883 U JP 13358883U JP S6052301 U JPS6052301 U JP S6052301U
- Authority
- JP
- Japan
- Prior art keywords
- axial flow
- flow turbomachinery
- rotor disk
- cylinder
- turbomachinery
- 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
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) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第１図はタービン段落の縦断正面図、第２図は従来例の
ディスクの側面図、第３図は第２図の■−ｍ線断面図、
第４図は本考案のディスクの側面図、第５図は第４図の
■−■線断面図である。 ４・・・・・・ロータ
ディスク、５・・・・・↓バランスホール、１０・・・
・・・ひさし。Fig. 1 is a longitudinal sectional front view of the turbine stage, Fig. 2 is a side view of a conventional disk, Fig. 3 is a sectional view taken along the line ■-m in Fig. 2,
FIG. 4 is a side view of the disk of the present invention, and FIG. 5 is a cross-sectional view taken along the line ■--■ in FIG. 4...Rotor disk, 5...↓Balance hole, 10...
···eaves.
Claims (1)
スホールにおいて、蒸気流の上流側となる入口側に、円
筒を部分しロータディスクに直角に、かつ回転方向に対
して円筒の内側が向くようなひさしを突設してなる軸流
ターボ機械。In the balance hole provided in the rotor disk of the turbine stage, on the inlet side, which is the upstream side of the steam flow, a part of the cylinder is provided with an eave that is perpendicular to the rotor disk and with the inside of the cylinder facing the direction of rotation. A protruding axial flow turbomachine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13358883U JPS6052301U (en) | 1983-08-31 | 1983-08-31 | axial flow turbomachinery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13358883U JPS6052301U (en) | 1983-08-31 | 1983-08-31 | axial flow turbomachinery |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6052301U true JPS6052301U (en) | 1985-04-12 |
Family
ID=30301289
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP13358883U Pending JPS6052301U (en) | 1983-08-31 | 1983-08-31 | axial flow turbomachinery |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6052301U (en) |
-
1983
- 1983-08-31 JP JP13358883U patent/JPS6052301U/en active Pending
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JPS6052301U (en) | axial flow turbomachinery | |
| JPS6012630U (en) | Turbocharger with variable nozzle vane | |
| JPS60190942U (en) | Turbo gear | |
| JPS6070798U (en) | centrifugal fluid machine | |
| JPS6043180U (en) | cross flow water wheel | |
| JPS60143109U (en) | Turbine exhaust structure | |
| JPS59182636U (en) | Turbocharger with variable nozzle vane | |
| JPS58142302U (en) | axial flow turbomachinery | |
| JPS58114846U (en) | turbo supercharger | |
| JPS58114842U (en) | Gas leak prevention mechanism for variable vane supercharger | |
| JPS6143675U (en) | Gas turbine combustor transition piece | |
| JPS613979U (en) | water wheel | |
| JPS60124588U (en) | Once-through water turbine | |
| JPS6055797U (en) | Diffuser pump | |
| JPS60116001U (en) | axial flow rotating machine | |
| JPS6039738U (en) | exhaust turbo supercharger | |
| JPS6098701U (en) | axial flow turbomachinery | |
| JPS59157538U (en) | turbo supercharger | |
| JPS6072902U (en) | turbine | |
| JPS60143272U (en) | Gas turbine combustor transition piece | |
| JPS6143902U (en) | gas turbine | |
| JPS5919930U (en) | Turbine housing of turbocharger | |
| JPS6117102U (en) | Steam turbine leak prevention device | |
| JPS60141428U (en) | Turbo combustion device | |
| JPS6077702U (en) | fluid rotating machinery |