JPS5364112A - Gas turbine compressor - Google Patents
Gas turbine compressorInfo
- Publication number
- JPS5364112A JPS5364112A JP13839876A JP13839876A JPS5364112A JP S5364112 A JPS5364112 A JP S5364112A JP 13839876 A JP13839876 A JP 13839876A JP 13839876 A JP13839876 A JP 13839876A JP S5364112 A JPS5364112 A JP S5364112A
- Authority
- JP
- Japan
- Prior art keywords
- gas turbine
- turbine compressor
- compressor
- durability
- casing
- 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
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
PURPOSE: To improve the durability of a compressor by setting up a cut groove on the inner surface of casing and extracting dust with air, then discharging outside with the compressor.
COPYRIGHT: (C)1978,JPO&Japio
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP13839876A JPS5364112A (en) | 1976-11-19 | 1976-11-19 | Gas turbine compressor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP13839876A JPS5364112A (en) | 1976-11-19 | 1976-11-19 | Gas turbine compressor |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5364112A true JPS5364112A (en) | 1978-06-08 |
Family
ID=15221009
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP13839876A Pending JPS5364112A (en) | 1976-11-19 | 1976-11-19 | Gas turbine compressor |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5364112A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04232337A (en) * | 1990-07-30 | 1992-08-20 | General Electric Co <Ge> | Back flow in cooling device and method for airplane engine |
JPH04284136A (en) * | 1990-11-19 | 1992-10-08 | General Electric Co <Ge> | High pressure compressor flow passage bleeding valve extraction slot |
JP2003533631A (en) * | 2000-05-15 | 2003-11-11 | ヌオーヴォ ピニォーネ ホールディング ソシエタ ペル アチオニ | Apparatus for controlling cooling flow rate of gas turbine |
JP2012255440A (en) * | 2011-06-08 | 2012-12-27 | Siemens Ag | Axial turbo compressor |
WO2016143103A1 (en) * | 2015-03-11 | 2016-09-15 | 株式会社 東芝 | Turbine |
-
1976
- 1976-11-19 JP JP13839876A patent/JPS5364112A/en active Pending
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04232337A (en) * | 1990-07-30 | 1992-08-20 | General Electric Co <Ge> | Back flow in cooling device and method for airplane engine |
JPH04284136A (en) * | 1990-11-19 | 1992-10-08 | General Electric Co <Ge> | High pressure compressor flow passage bleeding valve extraction slot |
JP2003533631A (en) * | 2000-05-15 | 2003-11-11 | ヌオーヴォ ピニォーネ ホールディング ソシエタ ペル アチオニ | Apparatus for controlling cooling flow rate of gas turbine |
JP2012255440A (en) * | 2011-06-08 | 2012-12-27 | Siemens Ag | Axial turbo compressor |
WO2016143103A1 (en) * | 2015-03-11 | 2016-09-15 | 株式会社 東芝 | Turbine |
US10550698B2 (en) | 2015-03-11 | 2020-02-04 | Toshiba Energy Systems & Solutions Corporation | Turbine |
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