JPS5947323U - gas turbine starting device - Google Patents
gas turbine starting deviceInfo
- Publication number
- JPS5947323U JPS5947323U JP11344283U JP11344283U JPS5947323U JP S5947323 U JPS5947323 U JP S5947323U JP 11344283 U JP11344283 U JP 11344283U JP 11344283 U JP11344283 U JP 11344283U JP S5947323 U JPS5947323 U JP S5947323U
- Authority
- JP
- Japan
- Prior art keywords
- gas turbine
- starter
- turbine engine
- fuel supply
- starting device
- 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
- Combined Controls Of Internal Combustion Engines (AREA)
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図は本考案になるガスタービン始動装置の一実施例
を示す電気結線図、第２図は本考案装置の作動説明に供
する各部波形図である。
Ｓｏ・・・回転センサ、Ｓｌ・・・スタータスイッチ、
Ｓ２・・・フリーランスイッチ、３・・・タイマー、−
４・・・停止制御回路をなすＮＡＮＤゲート、７・・・
スタータリレー回路、８・・・スタータモータ、９．１
０・・・比較器、１７・・・燃料遮断弁、２２・・・イ
グナイタ、２３゜２４．２５・・・表示手段をなす表示
ランプ。FIG. 1 is an electrical wiring diagram showing an embodiment of the gas turbine starting device according to the present invention, and FIG. 2 is a waveform diagram of each part to explain the operation of the device according to the present invention. So... Rotation sensor, Sl... Starter switch,
S2...Free run switch, 3...Timer, -
4... NAND gate forming a stop control circuit, 7...
Starter relay circuit, 8...Starter motor, 9.1
0... Comparator, 17... Fuel cutoff valve, 22... Igniter, 23°24.25... Display lamp serving as display means.
Claims (1)
タと、前記ガスタービン機関の回転数が連続燃焼可能回
転数に達すると燃料遮断を解除して燃料供給を開始する
燃料制御手段と、この燃料制御手段による燃料供給開始
に同期して点火火花を発生する点火手段と、前記ガスタ
ービン機関の回転数が自立運転可能回転数に達するまで
前記スタータ及び前記点火手段の作動を持続させる制御
手段と、フリーラン操作に連動して前記燃料供給及び前
記点火火花の発生を停止して前記スタータのみ作動させ
るフリーラン手段とを具備することを特徴とするガスタ
ービン始動装置。a starter that starts a gas turbine engine in conjunction with a starting operation; a fuel control means that releases fuel cutoff and starts fuel supply when the rotational speed of the gas turbine engine reaches a rotational speed that allows continuous combustion; an ignition means that generates an ignition spark in synchronization with the start of fuel supply by the means; a control means that continues the operation of the starter and the ignition means until the rotation speed of the gas turbine engine reaches a rotation speed that allows self-sustaining operation; A gas turbine starting device characterized by comprising: a free run means that stops the fuel supply and the generation of the ignition spark in conjunction with a run operation, and operates only the starter.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11344283U JPS5947323U (en) | 1983-07-20 | 1983-07-20 | gas turbine starting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11344283U JPS5947323U (en) | 1983-07-20 | 1983-07-20 | gas turbine starting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS5947323U true JPS5947323U (en) | 1984-03-29 |
Family
ID=30262608
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP11344283U Pending JPS5947323U (en) | 1983-07-20 | 1983-07-20 | gas turbine starting device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5947323U (en) |
-
1983
- 1983-07-20 JP JP11344283U patent/JPS5947323U/en active Pending
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