JPH0454048B2 - - Google Patents

Info

Publication number
JPH0454048B2
JPH0454048B2 JP58118606A JP11860683A JPH0454048B2 JP H0454048 B2 JPH0454048 B2 JP H0454048B2 JP 58118606 A JP58118606 A JP 58118606A JP 11860683 A JP11860683 A JP 11860683A JP H0454048 B2 JPH0454048 B2 JP H0454048B2
Authority
JP
Japan
Prior art keywords
compressor
turbine
pressure
gas
inlet
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.)
Expired - Lifetime
Application number
JP58118606A
Other languages
English (en)
Japanese (ja)
Other versions
JPS6011635A (ja
Inventor
Hisashi Mitani
Toshiichi Suefuji
Hidefumi Saito
Munehiro Hayashi
Masanao Ando
Hiroshi Isaka
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shimadzu Corp
Original Assignee
Shimadzu Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Shimadzu Corp filed Critical Shimadzu Corp
Priority to JP58118606A priority Critical patent/JPS6011635A/ja
Publication of JPS6011635A publication Critical patent/JPS6011635A/ja
Publication of JPH0454048B2 publication Critical patent/JPH0454048B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26Starting; Ignition

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel Cell (AREA)
JP58118606A 1983-06-29 1983-06-29 タ−ボ・コンプレツサシステム Granted JPS6011635A (ja)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58118606A JPS6011635A (ja) 1983-06-29 1983-06-29 タ−ボ・コンプレツサシステム

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58118606A JPS6011635A (ja) 1983-06-29 1983-06-29 タ−ボ・コンプレツサシステム

Publications (2)

Publication Number Publication Date
JPS6011635A JPS6011635A (ja) 1985-01-21
JPH0454048B2 true JPH0454048B2 (enrdf_load_stackoverflow) 1992-08-28

Family

ID=14740720

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58118606A Granted JPS6011635A (ja) 1983-06-29 1983-06-29 タ−ボ・コンプレツサシステム

Country Status (1)

Country Link
JP (1) JPS6011635A (enrdf_load_stackoverflow)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6179856A (ja) * 1984-09-26 1986-04-23 Mitsubishi Electric Corp タ−ボ圧縮機システムの起動方法
JP6087591B2 (ja) * 2012-11-12 2017-03-01 三菱日立パワーシステムズ株式会社 発電システム及び発電システムにおける燃料電池の起動方法
WO2014069413A1 (ja) * 2012-10-31 2014-05-08 三菱重工業株式会社 発電システム及び発電システムにおける燃料電池の起動方法
JP2018152181A (ja) * 2017-03-10 2018-09-27 株式会社豊田自動織機 燃料電池システム

Also Published As

Publication number Publication date
JPS6011635A (ja) 1985-01-21

Similar Documents

Publication Publication Date Title
EP3623604B1 (en) Hybrid expander cycle with pre-compression cooling and turbo-generator
EP0083109B1 (en) Combined plant having steam turbine and gas turbine connected by single shaft
US2951340A (en) Gas turbine with control mechanism for turbine cooling air
US4459802A (en) Bleedoff of gas diffusers in fluid flow machines
US7690188B2 (en) Combination engines for aircraft
US6427448B1 (en) Gas turbine and method of cooling a turbine stage
US5832714A (en) Gas turbine engine having flat rated horsepower
US4819423A (en) Integrated power unit
US5224337A (en) Operating method for gas turbine with variable inlet vanes
US20200386408A1 (en) Aircraft engine and method of operation thereof
JPS59173527A (ja) ガスタ−ビン排気フレ−ム冷却空気系統
JPH0454048B2 (enrdf_load_stackoverflow)
US3984784A (en) Expander open cycle gas dynamic laser
US3717994A (en) Gas turbine system with regenerator bypass only during starting
US11970970B2 (en) Adjustable primary and supplemental power units
JPS5941012B2 (ja) ガスタ−ビンエンジンの燃料制御方法及び装置
US3444686A (en) Gas turbine smog control for internal combustion engine
GB1257072A (enrdf_load_stackoverflow)
US1255924A (en) Gas-turbine.
JPS60160579A (ja) 燃料電池発電システムの起動方式
GB716145A (en) Improvements in aircraft jet propulsion engines including a ducted fan
GB1162939A (en) Improvements relating to Gas-Turbine Engines for Driving Vehicles
GB749263A (en) Improvements in or relating to a gas-turbine installation with an auxiliary or after-burning chamber
JPH11229963A (ja) 液体ロケットエンジンにおけるエキスパンダサイクル構造
JPH11336510A (ja) 一軸コンバインドプラント起動システム