JPS63150040U - - Google Patents
Info
- Publication number
- JPS63150040U JPS63150040U JP4201187U JP4201187U JPS63150040U JP S63150040 U JPS63150040 U JP S63150040U JP 4201187 U JP4201187 U JP 4201187U JP 4201187 U JP4201187 U JP 4201187U JP S63150040 U JPS63150040 U JP S63150040U
- Authority
- JP
- Japan
- Prior art keywords
- air
- compressor
- gas turbine
- gaseous fuel
- combustion chamber
- 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
- 238000002485 combustion reaction Methods 0.000 claims description 5
- 239000000446 fuel Substances 0.000 claims description 5
- 238000010586 diagram Methods 0.000 description 1
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
添付図面は、一部断面を示す本考案の気体燃料
供給装置の系統図である。
１…ガスタービン本体、２…燃焼室、３…抽気
室、４…空気膨張タービン、５…ターボ圧縮機。
The accompanying drawing is a partial cross-sectional diagram of the gaseous fuel supply device of the present invention. DESCRIPTION OF SYMBOLS 1... Gas turbine main body, 2... Combustion chamber, 3... Bleed chamber, 4... Air expansion turbine, 5... Turbo compressor.
Claims (1)
燃焼室に燃料を噴入し連続燃焼させるガスタービ
ンにおいて、前記圧縮機の圧縮途中または最終位
置に圧縮空気を抽気する抽気室を設け、同抽気室
からの抽気を膨張させて回転動力を得る空気膨張
タービンを設け、同空気膨張タービンと直結し、
低圧の気体燃料を圧縮するターボ圧縮機を設け、
前記気体燃料を同ターボ圧縮機によつてガスター
ビン本体の燃焼室より高い圧力まで昇圧して燃焼
室に噴入させるようにしたガスタービン用気体燃
料供給装置。 Inhale air at atmospheric pressure and compress it with a compressor.
In a gas turbine that injects fuel into a combustion chamber for continuous combustion, an air bleed chamber for extracting compressed air is provided during or at the final position of the compressor, and the air extracted from the air bleed chamber is expanded to obtain rotational power. An expansion turbine is provided, which is directly connected to the air expansion turbine.
A turbo compressor is installed to compress low-pressure gaseous fuel.
A gaseous fuel supply device for a gas turbine, wherein the gaseous fuel is pressurized by the turbo compressor to a pressure higher than that in the combustion chamber of the gas turbine main body, and then injected into the combustion chamber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4201187U JPS63150040U (en) | 1987-03-24 | 1987-03-24 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4201187U JPS63150040U (en) | 1987-03-24 | 1987-03-24 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS63150040U true JPS63150040U (en) | 1988-10-03 |
Family
ID=30857532
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4201187U Pending JPS63150040U (en) | 1987-03-24 | 1987-03-24 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS63150040U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2014047657A (en) * | 2012-08-30 | 2014-03-17 | Hitachi Ltd | Moisture utilizing gas turbine system |
-
1987
- 1987-03-24 JP JP4201187U patent/JPS63150040U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2014047657A (en) * | 2012-08-30 | 2014-03-17 | Hitachi Ltd | Moisture utilizing gas turbine system |
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