GB1275754A - Improvements in or relating to gas turbine engine power plants - Google Patents

Improvements in or relating to gas turbine engine power plants

Info

Publication number
GB1275754A
GB1275754A GB03927/69A GB1392769A GB1275754A GB 1275754 A GB1275754 A GB 1275754A GB 03927/69 A GB03927/69 A GB 03927/69A GB 1392769 A GB1392769 A GB 1392769A GB 1275754 A GB1275754 A GB 1275754A
Authority
GB
United Kingdom
Prior art keywords
valve
members
gas turbine
pass
duct
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
GB03927/69A
Inventor
Albert Jubb
Robert George Ward
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to FR6931135A priority Critical patent/FR2022168A1/en
Priority to CH1376669A priority patent/CH505283A/en
Priority to DE19691946676 priority patent/DE1946676A1/en
Publication of GB1275754A publication Critical patent/GB1275754A/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
    • G—PHYSICS
    • G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21D—NUCLEAR POWER PLANT
    • G21D5/00—Arrangements of reactor and engine in which reactor-produced heat is converted into mechanical energy
    • G21D5/04—Reactor and engine not structurally combined
    • G21D5/06—Reactor and engine not structurally combined with engine working medium circulating through reactor core
    • G—PHYSICS
    • G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21D—NUCLEAR POWER PLANT
    • G21D5/00—Arrangements of reactor and engine in which reactor-produced heat is converted into mechanical energy
    • G21D5/04—Reactor and engine not structurally combined
    • G21D5/08—Reactor and engine not structurally combined with engine working medium heated in a heat exchanger by the reactor coolant
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E30/00—Energy generation of nuclear origin

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Plasma & Fusion (AREA)
  • High Energy & Nuclear Physics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Control Of Turbines (AREA)

Abstract

1275754 Valves ROLLS-ROYCE Ltd 8 Sept 1969 [14 Sept 1968 17 March 1969] 43820/68 and 13927/69 Heading F2V [Also in Division F1] The invention relates to a gas turbine plant (see Division F1). In Fig. 2 the compressor drive turbine 24 and power turbine 32 are shown disposed in working fluid duct 35, a by-pass valve 36 controlling flow through by-pass duct 38 and a control valve 34 being shown. The by-pass duct is controlled by annular valve member 56 which moves ciroumferentially and axially by actuators 61 through linkage 62, 63, 59, the valve member 56 co-operating with an annular port 55 and being provided with sealing devices 57, 58. The control valve 34 comprises two series of arcuate members 66 which are formed with arms 70 which are pivotally mounted on tangential pins 72, the valve members being movable by actuators 80 which engage the valve members by a hook-shaped member 82, also by a roller 84. The valve members 66 are formed with openings 90 so as to permit a restricted flow of fluid when the valve members are in the closed positions.
GB03927/69A 1968-09-14 1968-09-14 Improvements in or relating to gas turbine engine power plants Expired GB1275754A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR6931135A FR2022168A1 (en) 1968-09-14 1969-09-12 Gas turbine for use with nuclear reactors
CH1376669A CH505283A (en) 1968-09-14 1969-09-12 Gas turbine power plant
DE19691946676 DE1946676A1 (en) 1968-09-14 1969-09-15 Gas turbine plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4382068 1968-09-14

Publications (1)

Publication Number Publication Date
GB1275754A true GB1275754A (en) 1972-05-24

Family

ID=10430436

Family Applications (1)

Application Number Title Priority Date Filing Date
GB03927/69A Expired GB1275754A (en) 1968-09-14 1968-09-14 Improvements in or relating to gas turbine engine power plants

Country Status (1)

Country Link
GB (1) GB1275754A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8499874B2 (en) 2009-05-12 2013-08-06 Icr Turbine Engine Corporation Gas turbine energy storage and conversion system
US8669670B2 (en) 2010-09-03 2014-03-11 Icr Turbine Engine Corporation Gas turbine engine configurations
US8866334B2 (en) 2010-03-02 2014-10-21 Icr Turbine Engine Corporation Dispatchable power from a renewable energy facility
US8984895B2 (en) 2010-07-09 2015-03-24 Icr Turbine Engine Corporation Metallic ceramic spool for a gas turbine engine
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
FR3060190A1 (en) * 2016-12-09 2018-06-15 Commissariat Energie Atomique CONVERTER, NUCLEAR POWER PLANT AND ASSOCIATED METHOD
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8499874B2 (en) 2009-05-12 2013-08-06 Icr Turbine Engine Corporation Gas turbine energy storage and conversion system
US8708083B2 (en) 2009-05-12 2014-04-29 Icr Turbine Engine Corporation Gas turbine energy storage and conversion system
US8866334B2 (en) 2010-03-02 2014-10-21 Icr Turbine Engine Corporation Dispatchable power from a renewable energy facility
US8984895B2 (en) 2010-07-09 2015-03-24 Icr Turbine Engine Corporation Metallic ceramic spool for a gas turbine engine
US8669670B2 (en) 2010-09-03 2014-03-11 Icr Turbine Engine Corporation Gas turbine engine configurations
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine
FR3060190A1 (en) * 2016-12-09 2018-06-15 Commissariat Energie Atomique CONVERTER, NUCLEAR POWER PLANT AND ASSOCIATED METHOD

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Legal Events

Date Code Title Description
PS Patent sealed
PLNP Patent lapsed through nonpayment of renewal fees