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GB2378224B - Gas turbine engine fuel delivery system - Google Patents

Gas turbine engine fuel delivery system

Info

Publication number
GB2378224B
GB2378224B GB0210014A GB0210014A GB2378224B GB 2378224 B GB2378224 B GB 2378224B GB 0210014 A GB0210014 A GB 0210014A GB 0210014 A GB0210014 A GB 0210014A GB 2378224 B GB2378224 B GB 2378224B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
delivery system
turbine engine
fuel delivery
engine fuel
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 - Fee Related
Application number
GB0210014A
Other versions
GB2378224A (en
GB0210014D0 (en
Inventor
Leslie Roy Summerfield
Jonathan Mark Gregoy
James Leonard Boston
Peter John Harding
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
Priority claimed from GB0117554A external-priority patent/GB0117554D0/en
Priority claimed from GB0209295A external-priority patent/GB0209295D0/en
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of GB0210014D0 publication Critical patent/GB0210014D0/en
Priority to DE60217768T priority Critical patent/DE60217768T2/en
Priority to EP02254367A priority patent/EP1278014B1/en
Priority to US10/183,391 priority patent/US6857272B2/en
Publication of GB2378224A publication Critical patent/GB2378224A/en
Application granted granted Critical
Publication of GB2378224B publication Critical patent/GB2378224B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding And Controlling Fuel (AREA)
GB0210014A 2001-07-18 2002-05-02 Gas turbine engine fuel delivery system Expired - Fee Related GB2378224B (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
DE60217768T DE60217768T2 (en) 2001-07-18 2002-06-24 Fuel delivery device
EP02254367A EP1278014B1 (en) 2001-07-18 2002-06-24 Fuel delivery system
US10/183,391 US6857272B2 (en) 2001-07-18 2002-06-28 Fuel delivery system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB0117554A GB0117554D0 (en) 2001-07-18 2001-07-18 Fluid delivery system
GB0209295A GB0209295D0 (en) 2002-04-24 2002-04-24 Fuel delivery system

Publications (3)

Publication Number Publication Date
GB0210014D0 GB0210014D0 (en) 2002-06-12
GB2378224A GB2378224A (en) 2003-02-05
GB2378224B true GB2378224B (en) 2005-10-12

Family

ID=26246324

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0210014A Expired - Fee Related GB2378224B (en) 2001-07-18 2002-05-02 Gas turbine engine fuel delivery system

Country Status (1)

Country Link
GB (1) GB2378224B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2480773B1 (en) * 2009-09-24 2014-12-31 Siemens Aktiengesellschaft Fuel line system, method for operating a gas turbine, and method for purging the fuel line system of a gas turbine
GB201604379D0 (en) 2016-03-15 2016-04-27 Rolls Royce Plc A combustion chamber system and a method of operating a combustion chamber system
CN115030824B (en) * 2022-08-11 2022-11-22 成都凯天电子股份有限公司 Self-adaptive oil supply system and method under full flight profile of helicopter

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB654122A (en) * 1948-06-11 1951-06-06 Rolls Royce Improvements in or relating to combustion equipment for gas-turbine engines
US4417439A (en) * 1981-07-29 1983-11-29 United Technologies Corporation Starting means for a gas turbine engine
US4817389A (en) * 1987-09-24 1989-04-04 United Technologies Corporation Fuel injection system
EP0802310A2 (en) * 1996-04-18 1997-10-22 ROLLS-ROYCE plc Fuel system for a gas turbine engine
US5680753A (en) * 1994-08-19 1997-10-28 Asea Brown Boveri Ag Method of regulating the rotational speed of a gas turbine during load disconnection
GB2320063A (en) * 1993-12-09 1998-06-10 United Technologies Corp Fuel staging system for gas turbine engine
EP1182401A1 (en) * 2000-08-16 2002-02-27 General Electric Company Method and apparatus for decreasing combustor emissions

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB654122A (en) * 1948-06-11 1951-06-06 Rolls Royce Improvements in or relating to combustion equipment for gas-turbine engines
US4417439A (en) * 1981-07-29 1983-11-29 United Technologies Corporation Starting means for a gas turbine engine
US4817389A (en) * 1987-09-24 1989-04-04 United Technologies Corporation Fuel injection system
GB2320063A (en) * 1993-12-09 1998-06-10 United Technologies Corp Fuel staging system for gas turbine engine
US5680753A (en) * 1994-08-19 1997-10-28 Asea Brown Boveri Ag Method of regulating the rotational speed of a gas turbine during load disconnection
EP0802310A2 (en) * 1996-04-18 1997-10-22 ROLLS-ROYCE plc Fuel system for a gas turbine engine
EP1182401A1 (en) * 2000-08-16 2002-02-27 General Electric Company Method and apparatus for decreasing combustor emissions

Also Published As

Publication number Publication date
GB2378224A (en) 2003-02-05
GB0210014D0 (en) 2002-06-12

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20200502