CA1005241A - Relief arrangement for closed gas turbine installation - Google Patents

Relief arrangement for closed gas turbine installation

Info

Publication number
CA1005241A
CA1005241A CA200,989A CA200989A CA1005241A CA 1005241 A CA1005241 A CA 1005241A CA 200989 A CA200989 A CA 200989A CA 1005241 A CA1005241 A CA 1005241A
Authority
CA
Canada
Prior art keywords
gas turbine
turbine installation
closed gas
relief arrangement
relief
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
Application number
CA200,989A
Other languages
English (en)
Other versions
CA200989S (en
Inventor
Hansulrich Frutschi
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.)
Brown Boveri Sulzer Turbomaschinen AG
Original Assignee
Brown Boveri Sulzer Turbomaschinen AG
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 Brown Boveri Sulzer Turbomaschinen AG filed Critical Brown Boveri Sulzer Turbomaschinen AG
Application granted granted Critical
Publication of CA1005241A publication Critical patent/CA1005241A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/24—Control of the pressure level in closed cycles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
CA200,989A 1973-06-08 1974-05-28 Relief arrangement for closed gas turbine installation Expired CA1005241A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH834473A CH558879A (de) 1973-06-08 1973-06-08 Entlastungsvorrichtung fuer eine geschlossene gasturbinen anlage.

Publications (1)

Publication Number Publication Date
CA1005241A true CA1005241A (en) 1977-02-15

Family

ID=4338880

Family Applications (1)

Application Number Title Priority Date Filing Date
CA200,989A Expired CA1005241A (en) 1973-06-08 1974-05-28 Relief arrangement for closed gas turbine installation

Country Status (9)

Country Link
US (1) US3864919A (de)
JP (1) JPS5727296B2 (de)
BE (1) BE815796A (de)
CA (1) CA1005241A (de)
CH (1) CH558879A (de)
FR (1) FR2232678B1 (de)
GB (1) GB1446820A (de)
IT (1) IT1010226B (de)
SE (1) SE412436B (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4761957A (en) * 1983-03-01 1988-08-09 Solar Turbines Incorporated Indirectly heated gas turbine engine
RU2464436C2 (ru) * 2008-03-28 2012-10-20 Мицубиси Хеви Индастрис, Лтд. Способ управления турбинной установкой и турбинная установка
EP2334912B1 (de) * 2008-03-28 2016-06-22 Mitsubishi Heavy Industries, Ltd. Verfahren zur steuerung einer turbinenanlage und turbinenanlage
US7805942B2 (en) * 2008-06-02 2010-10-05 Thomas Durso Thermodynamic cycle with power unit and venturi and a method of producing a useful effect therewith
US9706685B2 (en) 2011-12-28 2017-07-11 Liebert Corporation Cooling system for high density heat loads
US9494371B2 (en) * 2011-12-28 2016-11-15 Liebert Corporation Pumped refrigerant cooling system with 1+1 to N+1 and built-in redundancy
US11879385B2 (en) 2021-02-08 2024-01-23 Rolls-Royce North American Technologies Inc. Engine system with fuel-drive thermal support
US11776702B2 (en) 2021-02-08 2023-10-03 Rolls-Royce North American Technologies Inc. System for control of externally heated turbine engine
US11499474B2 (en) 2021-02-08 2022-11-15 Rolls-Royce North American Technologies Inc. System for startup support of externally heated turbine engine
US12503956B2 (en) 2023-11-03 2025-12-23 Rolls-Royce North American Technologies Inc. Closed Brayton cycle power generation system with compressor discharge fluid driven cooling flow for cooling electrical hardware
US12587067B1 (en) 2025-03-20 2026-03-24 Rolls-Royce North American Technologies Inc. Closed brayton cycle shutdown control with isolated fluid reservoir for cooling electrical components

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2642721A (en) * 1948-01-29 1953-06-23 Power Jets Res & Dev Ltd Closed cycle elastic fluid compressor-turbine plant and control thereof

Also Published As

Publication number Publication date
FR2232678A1 (de) 1975-01-03
IT1010226B (it) 1977-01-10
JPS5727296B2 (de) 1982-06-09
US3864919A (en) 1975-02-11
CH558879A (de) 1975-02-14
GB1446820A (en) 1976-08-18
JPS5022111A (de) 1975-03-10
SE412436B (sv) 1980-03-03
BE815796A (fr) 1974-09-16
SE7407548L (de) 1974-12-09
FR2232678B1 (de) 1980-08-01

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