JPS6317839U - - Google Patents
Info
- Publication number
- JPS6317839U JPS6317839U JP10867386U JP10867386U JPS6317839U JP S6317839 U JPS6317839 U JP S6317839U JP 10867386 U JP10867386 U JP 10867386U JP 10867386 U JP10867386 U JP 10867386U JP S6317839 U JPS6317839 U JP S6317839U
- Authority
- JP
- Japan
- Prior art keywords
- fuel
- pressurized
- gas turbine
- supply device
- accumulator
- 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
- 239000000446 fuel Substances 0.000 claims description 13
- 238000010586 diagram Methods 0.000 description 3
- 239000002828 fuel tank Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
Description
第１図は本考案ガスタービンの燃料供給装置の
構成の一例を示す模式図、第２図は本考案の他の
実施例の構成を示す模式図、第３図は従来のガス
タービンの燃料供給装置の構成の一例を示す模式
図である。
１……タービン、２……コンプレツサ、４……
始動モータ、６……燃料ポンプ、８……燃料タン
ク、１０，３５……しや断弁、１１……燃焼器、
１２……燃料噴射弁、２１……アキユムレータ、
２２……レベライザ弁、２３……燃料送出管、２
３Ａ……分岐管、２４，２７，３２，３３……逆
止弁、２５……三方弁、２６……アクチユエータ
。
Fig. 1 is a schematic diagram showing an example of the configuration of a fuel supply system for a gas turbine of the present invention, Fig. 2 is a schematic diagram showing a configuration of another embodiment of the present invention, and Fig. 3 is a conventional fuel supply system for a gas turbine. FIG. 1 is a schematic diagram showing an example of the configuration of an apparatus. 1... Turbine, 2... Compressor, 4...
Starting motor, 6... fuel pump, 8... fuel tank, 10, 35... bottom valve, 11... combustor,
12... Fuel injection valve, 21... Accumulator,
22...Levelizer valve, 23...Fuel delivery pipe, 2
3A... Branch pipe, 24, 27, 32, 33... Check valve, 25... Three-way valve, 26... Actuator.
Claims (1)
プレツサから送出された加圧空気を燃焼器に導く
ようにしたガスタービンの燃料供給装置において
、 前記加圧燃料および前記加圧空気の貯留が可能
なアキユムレータと、 前記ガスタービンの運転中に前記加圧燃料およ
び前記加圧空気を前記アキユムレータに導く手段
と、 前記ガスタービンの始動時に前記アキユムレー
タから前記加圧燃料を前記燃焼器に供給する手段
とを設けたことを特徴とするガスタービンの燃料
供給装置。[Claims for Utility Model Registration] A fuel supply device for a gas turbine configured to guide pressurized fuel sent from a fuel pump and pressurized air sent from a compressor to a combustor, the pressurized fuel and the pressurized an accumulator capable of storing air; means for guiding the pressurized fuel and the pressurized air to the accumulator during operation of the gas turbine; and means for introducing the pressurized fuel from the accumulator to the combustor when the gas turbine is started. 1. A fuel supply device for a gas turbine, characterized in that a fuel supply device for a gas turbine is provided.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10867386U JPS6317839U (en) | 1986-07-17 | 1986-07-17 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10867386U JPS6317839U (en) | 1986-07-17 | 1986-07-17 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6317839U true JPS6317839U (en) | 1988-02-05 |
Family
ID=30986086
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP10867386U Pending JPS6317839U (en) | 1986-07-17 | 1986-07-17 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6317839U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103237971A (en) * | 2010-11-30 | 2013-08-07 | 西门子公司 | Method for operating a fixed gas turbine, device for regulating the operation of a gas turbine and power plant |
| CN105065123A (en) * | 2015-07-15 | 2015-11-18 | 中国航空工业集团公司沈阳发动机设计研究所 | Auxiliary oil-sealing method and device for combustion gas turbine |
-
1986
- 1986-07-17 JP JP10867386U patent/JPS6317839U/ja active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103237971A (en) * | 2010-11-30 | 2013-08-07 | 西门子公司 | Method for operating a fixed gas turbine, device for regulating the operation of a gas turbine and power plant |
| JP2013545022A (en) * | 2010-11-30 | 2013-12-19 | シーメンス アクティエンゲゼルシャフト | Operation method of stationary gas turbine, operation adjusting device for gas turbine, and power plant |
| CN105065123A (en) * | 2015-07-15 | 2015-11-18 | 中国航空工业集团公司沈阳发动机设计研究所 | Auxiliary oil-sealing method and device for combustion gas turbine |