JPH0437807U - - Google Patents
Info
- Publication number
- JPH0437807U JPH0437807U JP7811990U JP7811990U JPH0437807U JP H0437807 U JPH0437807 U JP H0437807U JP 7811990 U JP7811990 U JP 7811990U JP 7811990 U JP7811990 U JP 7811990U JP H0437807 U JPH0437807 U JP H0437807U
- Authority
- JP
- Japan
- Prior art keywords
- side ring
- stationary side
- gas turbine
- steam introduction
- introduction section
- 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
Links
- 238000002347 injection Methods 0.000 claims description 2
- 239000007924 injection Substances 0.000 claims description 2
- 238000001816 cooling Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Description
第1図は、本考案の実施例に係るエンジンの断
面図、第2図aは従来の静止側を分割構造とした
チツプクリアランス調整方法を示す断面図、第2
図bは第2図A−A方向の矢視図、第3図は従来
の冷却抽気空気構造としたチツプクリアランス調
整方法を示す断面図である。
1……動翼、2……静止側リング、3……噴射
孔、4……流量調節弁、8……通路部、10……
水蒸気導入部。
FIG. 1 is a sectional view of an engine according to an embodiment of the present invention, FIG.
Fig. b is a view taken along the line A--A in Fig. 2, and Fig. 3 is a sectional view showing a method of adjusting chip clearance using a conventional cooling bleed air structure. DESCRIPTION OF SYMBOLS 1... Moving blade, 2... Stationary side ring, 3... Injection hole, 4... Flow rate control valve, 8... Passage part, 10...
Water vapor introduction section.
Claims (1)
させるガスタービンにおいて、静止側リング外側
に設けられた水蒸気導入部と前記水蒸気導入部に
前記静止側リングに向けて穿設された噴射孔と、
前記水蒸気導入部が位置する前記静止側リング外
周空間部と前記燃焼器とを連通する通路部とを備
えたことを特徴とするガスタービン。 In a gas turbine that operates a turbine with high-temperature gas burned in a combustor, a steam introduction section provided outside a stationary side ring, and an injection hole bored in the steam introduction section toward the stationary side ring;
A gas turbine characterized in that the gas turbine includes a passage section that communicates the stationary side ring outer circumferential space where the steam introduction section is located and the combustor.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1990078119U JP2588415Y2 (en) | 1990-07-23 | 1990-07-23 | gas turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1990078119U JP2588415Y2 (en) | 1990-07-23 | 1990-07-23 | gas turbine |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH0437807U true JPH0437807U (en) | 1992-03-31 |
JP2588415Y2 JP2588415Y2 (en) | 1999-01-13 |
Family
ID=31621109
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1990078119U Expired - Lifetime JP2588415Y2 (en) | 1990-07-23 | 1990-07-23 | gas turbine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2588415Y2 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2014058979A (en) * | 2013-11-27 | 2014-04-03 | Mitsubishi Heavy Ind Ltd | Gas turbine and its rated operational method |
US9255490B2 (en) | 2008-10-08 | 2016-02-09 | Mitsubishi Heavy Industries, Ltd. | Gas turbine and operating method thereof |
JP2017025908A (en) * | 2015-07-20 | 2017-02-02 | ゼネラル・エレクトリック・カンパニイ | Cooling system for turbine engine |
US11702958B2 (en) | 2021-09-23 | 2023-07-18 | General Electric Company | System and method of regulating thermal transport bus pressure |
US11788470B2 (en) | 2021-03-01 | 2023-10-17 | General Electric Company | Gas turbine engine thermal management |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6479386B2 (en) * | 2014-09-26 | 2019-03-06 | 株式会社東芝 | Steam turbine |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4910763A (en) * | 1972-05-26 | 1974-01-30 | ||
JPS6267239A (en) * | 1985-09-20 | 1987-03-26 | Toyo Eng Corp | Power generating method for gas turbine |
JPS6297239A (en) * | 1985-10-22 | 1987-05-06 | Toshiba Corp | X-ray image pickup tube |
JPS63154806A (en) * | 1986-12-19 | 1988-06-28 | Mitsubishi Heavy Ind Ltd | Blade tip clearance adjuster for rotary machine |
JPS6438214A (en) * | 1987-08-03 | 1989-02-08 | Kyoto Kasei Kogyo Kk | Method for molding product having closure film |
-
1990
- 1990-07-23 JP JP1990078119U patent/JP2588415Y2/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4910763A (en) * | 1972-05-26 | 1974-01-30 | ||
JPS6267239A (en) * | 1985-09-20 | 1987-03-26 | Toyo Eng Corp | Power generating method for gas turbine |
JPS6297239A (en) * | 1985-10-22 | 1987-05-06 | Toshiba Corp | X-ray image pickup tube |
JPS63154806A (en) * | 1986-12-19 | 1988-06-28 | Mitsubishi Heavy Ind Ltd | Blade tip clearance adjuster for rotary machine |
JPS6438214A (en) * | 1987-08-03 | 1989-02-08 | Kyoto Kasei Kogyo Kk | Method for molding product having closure film |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9255490B2 (en) | 2008-10-08 | 2016-02-09 | Mitsubishi Heavy Industries, Ltd. | Gas turbine and operating method thereof |
US9951644B2 (en) | 2008-10-08 | 2018-04-24 | Mitsubishi Heavy Industries, Ltd. | Gas turbine and operating method thereof |
US10247030B2 (en) | 2008-10-08 | 2019-04-02 | Mitsubishi Heavy Industries, Ltd. | Gas turbine and operating method thereof |
US10309245B2 (en) | 2008-10-08 | 2019-06-04 | Mitsubishi Heavy Industries, Ltd. | Gas turbine and operating method thereof |
JP2014058979A (en) * | 2013-11-27 | 2014-04-03 | Mitsubishi Heavy Ind Ltd | Gas turbine and its rated operational method |
JP2017025908A (en) * | 2015-07-20 | 2017-02-02 | ゼネラル・エレクトリック・カンパニイ | Cooling system for turbine engine |
US10487739B2 (en) | 2015-07-20 | 2019-11-26 | General Electric Company | Cooling system for a turbine engine |
US11788470B2 (en) | 2021-03-01 | 2023-10-17 | General Electric Company | Gas turbine engine thermal management |
US11702958B2 (en) | 2021-09-23 | 2023-07-18 | General Electric Company | System and method of regulating thermal transport bus pressure |
Also Published As
Publication number | Publication date |
---|---|
JP2588415Y2 (en) | 1999-01-13 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
EXPY | Cancellation because of completion of term |