JPS5932104U - axial turbine - Google Patents
axial turbineInfo
- Publication number
- JPS5932104U JPS5932104U JP12797882U JP12797882U JPS5932104U JP S5932104 U JPS5932104 U JP S5932104U JP 12797882 U JP12797882 U JP 12797882U JP 12797882 U JP12797882 U JP 12797882U JP S5932104 U JPS5932104 U JP S5932104U
- Authority
- JP
- Japan
- Prior art keywords
- stator
- annular row
- blades
- rotating shaft
- stator vanes
- 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図は従来技術における軸流タービンの断面図、第2
図は入口室内部の圧力分布を説明する線 、図、第3図
は本考案に係る軸流タービンの要部を示す断面図、第4
図は本考案に係る入口室内における圧力分布を説明する
線図である。
10・・・回転軸、11・・・入口管路、12・・・入
口室、13・・・静翼、14・・・動翼、15・・・ケ
ーシング、16・・・ダイヤフラム外輪、17・・・ダ
イヤフラム内輪、18・・・ガイド部。Figure 1 is a cross-sectional view of an axial flow turbine in the prior art;
3 is a sectional view showing the main parts of the axial flow turbine according to the present invention, and 4 is a sectional view showing the main parts of the axial flow turbine according to the present invention.
The figure is a diagram illustrating the pressure distribution in the inlet chamber according to the present invention. DESCRIPTION OF SYMBOLS 10... Rotating shaft, 11... Inlet pipe line, 12... Inlet chamber, 13... Stationary blade, 14... Moving blade, 15... Casing, 16... Diaphragm outer ring, 17 ...Diaphragm inner ring, 18...Guide part.
Claims (1)
の環状列と、回転軸に植設された動翼の環状列とを備え
、これらの静翼、および動翼の環状列は互いに回転軸の
軸線方向に一定の間隙を保持して配置され、また前記静
翼の環状列の上流側には入口管路を通して送られる作動
流体を各静翼に案内せしめる入口室を設けてなる軸流タ
ービンにおいて、前記入口室の前方に前記入口管路中心
点よりその反対側まで周方向に除々に減少する山形のガ
イド部をケーシングと一体に設けたことを特徴とする軸
流タービン。The diaphragm includes an annular row of stator vanes held between an outer ring and an inner ring, and an annular row of rotor blades installed on a rotating shaft, and these stator vanes and the annular row of rotor blades are arranged in the axial direction of the rotating shaft. In the axial flow turbine, the stator blades are arranged with a constant gap between the stator vanes, and an inlet chamber is provided upstream of the annular row of the stator blades for guiding the working fluid sent through the inlet pipe to each stator blade. An axial flow turbine characterized in that a chevron-shaped guide portion that gradually decreases in the circumferential direction from the center point of the inlet pipe to the opposite side thereof is provided integrally with the casing in front of the inlet chamber.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP12797882U JPS5932104U (en) | 1982-08-26 | 1982-08-26 | axial turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP12797882U JPS5932104U (en) | 1982-08-26 | 1982-08-26 | axial turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5932104U true JPS5932104U (en) | 1984-02-28 |
Family
ID=30290479
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP12797882U Pending JPS5932104U (en) | 1982-08-26 | 1982-08-26 | axial turbine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5932104U (en) |
-
1982
- 1982-08-26 JP JP12797882U patent/JPS5932104U/en active Pending
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