GB2240858B - Engine controller for reheated turbofans - Google Patents

Engine controller for reheated turbofans

Info

Publication number
GB2240858B
GB2240858B GB9002945A GB9002945A GB2240858B GB 2240858 B GB2240858 B GB 2240858B GB 9002945 A GB9002945 A GB 9002945A GB 9002945 A GB9002945 A GB 9002945A GB 2240858 B GB2240858 B GB 2240858B
Authority
GB
United Kingdom
Prior art keywords
turbofans
reheated
engine controller
engine
controller
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
GB9002945A
Other versions
GB9002945D0 (en
GB2240858A (en
Inventor
Graham John Dadd
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.)
UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
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 UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Priority to GB9002945A priority Critical patent/GB2240858B/en
Publication of GB9002945D0 publication Critical patent/GB9002945D0/en
Publication of GB2240858A publication Critical patent/GB2240858A/en
Application granted granted Critical
Publication of GB2240858B publication Critical patent/GB2240858B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06Varying effective area of jet pipe or nozzle
    • F02K1/15Control or regulation
    • F02K1/16Control or regulation conjointly with another control
    • F02K1/17Control or regulation conjointly with another control with control of fuel supply

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feedback Control In General (AREA)
GB9002945A 1990-02-09 1990-02-09 Engine controller for reheated turbofans Expired - Fee Related GB2240858B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9002945A GB2240858B (en) 1990-02-09 1990-02-09 Engine controller for reheated turbofans

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9002945A GB2240858B (en) 1990-02-09 1990-02-09 Engine controller for reheated turbofans

Publications (3)

Publication Number Publication Date
GB9002945D0 GB9002945D0 (en) 1990-04-04
GB2240858A GB2240858A (en) 1991-08-14
GB2240858B true GB2240858B (en) 1993-08-04

Family

ID=10670712

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9002945A Expired - Fee Related GB2240858B (en) 1990-02-09 1990-02-09 Engine controller for reheated turbofans

Country Status (1)

Country Link
GB (1) GB2240858B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112328968B (en) * 2020-11-03 2024-05-17 中国航发沈阳发动机研究所 Engine inlet total pressure determining method

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1012941A (en) * 1961-03-10 1965-12-15 Plessey Co Ltd Improvements in or relating to fuel control devices for internal combustion engines
GB1071241A (en) * 1963-09-13 1967-06-07 Bendix Corp Fuel flow apparatus for combustion engines
GB1184369A (en) * 1966-12-22 1970-03-18 Gen Electric Improvements in control systems for axial flow compressors particularly adapted for use in gas turbine engines
GB1296986A (en) * 1969-03-27 1972-11-22
GB1322356A (en) * 1969-11-25 1973-07-04 Gen Electric Gas turbine engine augmentation control system

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1012941A (en) * 1961-03-10 1965-12-15 Plessey Co Ltd Improvements in or relating to fuel control devices for internal combustion engines
GB1071241A (en) * 1963-09-13 1967-06-07 Bendix Corp Fuel flow apparatus for combustion engines
GB1184369A (en) * 1966-12-22 1970-03-18 Gen Electric Improvements in control systems for axial flow compressors particularly adapted for use in gas turbine engines
GB1296986A (en) * 1969-03-27 1972-11-22
GB1322356A (en) * 1969-11-25 1973-07-04 Gen Electric Gas turbine engine augmentation control system

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
GB 680136 A *

Also Published As

Publication number Publication date
GB9002945D0 (en) 1990-04-04
GB2240858A (en) 1991-08-14

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Legal Events

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

Effective date: 19950209