GB0118077D0 - A gas turbine engine - Google Patents

A gas turbine engine

Info

Publication number
GB0118077D0
GB0118077D0 GB0118077A GB0118077A GB0118077D0 GB 0118077 D0 GB0118077 D0 GB 0118077D0 GB 0118077 A GB0118077 A GB 0118077A GB 0118077 A GB0118077 A GB 0118077A GB 0118077 D0 GB0118077 D0 GB 0118077D0
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
engine
gas
turbine
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.)
Withdrawn
Application number
GB0118077A
Other versions
GB2377973A (en
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 GB0118077A priority Critical patent/GB2377973A/en
Publication of GB0118077D0 publication Critical patent/GB0118077D0/en
Publication of GB2377973A publication Critical patent/GB2377973A/en
Withdrawn legal-status Critical Current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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/13—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having variable working fluid interconnections between turbines or compressors or stages of different rotors

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
GB0118077A 2001-07-25 2001-07-25 Gas bleed system for a gas turbine Withdrawn GB2377973A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0118077A GB2377973A (en) 2001-07-25 2001-07-25 Gas bleed system for a gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0118077A GB2377973A (en) 2001-07-25 2001-07-25 Gas bleed system for a gas turbine

Publications (2)

Publication Number Publication Date
GB0118077D0 true GB0118077D0 (en) 2001-09-19
GB2377973A GB2377973A (en) 2003-01-29

Family

ID=9919122

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0118077A Withdrawn GB2377973A (en) 2001-07-25 2001-07-25 Gas bleed system for a gas turbine

Country Status (1)

Country Link
GB (1) GB2377973A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112627989A (en) * 2021-01-08 2021-04-09 大连欧谱纳透平动力科技有限公司 System and method for controlling exhaust temperature and nitrogen oxide concentration of small gas turbine

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7353647B2 (en) 2004-05-13 2008-04-08 General Electric Company Methods and apparatus for assembling gas turbine engines
GB0504272D0 (en) 2005-03-02 2005-04-06 Rolls Royce Plc A turbine engine and a method of operating a turbine engine
EP1967717A1 (en) * 2007-03-07 2008-09-10 Siemens Aktiengesellschaft Gas turbine with a bypass conduit system
US8015826B2 (en) * 2007-04-05 2011-09-13 Siemens Energy, Inc. Engine brake for part load CO reduction
FR2981686B1 (en) * 2011-10-21 2016-05-20 Snecma TURBOMACHINE COMPRISING A CONTRAROTATIVE PROPELLER RECEIVER SUPPORTED BY A STRUCTURAL ENVELOPE FIXED TO THE INTERMEDIATE CASE
US11143407B2 (en) 2013-06-11 2021-10-12 Raytheon Technologies Corporation Combustor with axial staging for a gas turbine engine
DE102013224982A1 (en) 2013-12-05 2015-06-11 Rolls-Royce Deutschland Ltd & Co Kg Aircraft gas turbine with a core engine housing with cooling air tubes
US10696417B2 (en) * 2015-06-25 2020-06-30 Pratt & Whitney Canada Corp. Auxiliary power unit with excess air recovery
US10711702B2 (en) * 2015-08-18 2020-07-14 General Electric Company Mixed flow turbocore
US10578028B2 (en) 2015-08-18 2020-03-03 General Electric Company Compressor bleed auxiliary turbine
IT201600107332A1 (en) * 2016-10-25 2018-04-25 Nuovo Pignone Tecnologie Srl GAS TURBINE SYSTEM WITH ARRANGEMENT TO CONVEY THE PURGE / GAS TURBINE SYSTEM WITH BLEED ROUTING ARRANGEMENT
CN107061020A (en) * 2016-12-23 2017-08-18 中国人民解放军海军工程大学 A kind of deflation reutilization system of the low operating mode of gas turbine

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4157010A (en) * 1977-06-03 1979-06-05 General Electric Company Gas turbine engine with power modulation capability
US4631914A (en) * 1985-02-25 1986-12-30 General Electric Company Gas turbine engine of improved thermal efficiency
US5174105A (en) * 1990-11-09 1992-12-29 General Electric Company Hot day m & i gas turbine engine and method of operation
GB2288640B (en) * 1994-04-16 1998-08-12 Rolls Royce Plc A gas turbine engine
EP0978635B1 (en) * 1998-08-05 2003-05-28 ALSTOM (Switzerland) Ltd Process for cooling the thermally stressed structures of a power plant

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112627989A (en) * 2021-01-08 2021-04-09 大连欧谱纳透平动力科技有限公司 System and method for controlling exhaust temperature and nitrogen oxide concentration of small gas turbine

Also Published As

Publication number Publication date
GB2377973A (en) 2003-01-29

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)