GB1293672A - Improvements in fuel supply systems for aircraft gas turbine jet engines - Google Patents

Improvements in fuel supply systems for aircraft gas turbine jet engines

Info

Publication number
GB1293672A
GB1293672A GB00647/70A GB1064770A GB1293672A GB 1293672 A GB1293672 A GB 1293672A GB 00647/70 A GB00647/70 A GB 00647/70A GB 1064770 A GB1064770 A GB 1064770A GB 1293672 A GB1293672 A GB 1293672A
Authority
GB
United Kingdom
Prior art keywords
line
fuel
valve
pressure
controlled
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
GB00647/70A
Other languages
English (en)
Inventor
Stanley George Glaze
Donald Craven
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.)
Hobson Ltd H M
HM Hobson Ltd
Original Assignee
Hobson Ltd H M
HM Hobson Ltd
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 Hobson Ltd H M, HM Hobson Ltd filed Critical Hobson Ltd H M
Priority to GB00647/70A priority Critical patent/GB1293672A/en
Priority to FR7107690A priority patent/FR2081729B1/fr
Priority to DE19712110538 priority patent/DE2110538A1/de
Publication of GB1293672A publication Critical patent/GB1293672A/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
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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)
  • Control Of The Air-Fuel Ratio Of Carburetors (AREA)
GB00647/70A 1970-03-05 1970-03-05 Improvements in fuel supply systems for aircraft gas turbine jet engines Expired GB1293672A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB00647/70A GB1293672A (en) 1970-03-05 1970-03-05 Improvements in fuel supply systems for aircraft gas turbine jet engines
FR7107690A FR2081729B1 (enrdf_load_stackoverflow) 1970-03-05 1971-03-05
DE19712110538 DE2110538A1 (de) 1970-03-05 1971-03-05 Brennstoffsteuervorrichtung fuer einen Nachbrenner fuer Strahltriebwerke von Flugzeugen

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB00647/70A GB1293672A (en) 1970-03-05 1970-03-05 Improvements in fuel supply systems for aircraft gas turbine jet engines

Publications (1)

Publication Number Publication Date
GB1293672A true GB1293672A (en) 1972-10-18

Family

ID=9971700

Family Applications (1)

Application Number Title Priority Date Filing Date
GB00647/70A Expired GB1293672A (en) 1970-03-05 1970-03-05 Improvements in fuel supply systems for aircraft gas turbine jet engines

Country Status (3)

Country Link
DE (1) DE2110538A1 (enrdf_load_stackoverflow)
FR (1) FR2081729B1 (enrdf_load_stackoverflow)
GB (1) GB1293672A (enrdf_load_stackoverflow)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2432886A (en) * 1990-03-16 2007-06-06 Lucas Ind Plc Gas turbine engine reheat fuel control system and control valves therefor
US7413141B1 (en) 1989-05-10 2008-08-19 Goodrich Control Systems Limited Gas turbine engine fuel control system and regulating valves therefor

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1381100A (en) * 1971-04-13 1975-01-22 Lucas Industries Ltd Fuel control apparatus for gas turbine engine
GB1423363A (en) * 1972-06-21 1976-02-04 Lucas Industries Ltd Fuel control apparatus for gas turbine engine reheat systems
GB1423364A (en) * 1972-06-21 1976-02-04 Lucas Industries Ltd Fuel control apparatus for gas turbine engine reheat system
DE3629551A1 (de) * 1986-08-30 1988-03-10 Telefonbau & Normalzeit Gmbh Anordnung fuer hauptverteiler

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7413141B1 (en) 1989-05-10 2008-08-19 Goodrich Control Systems Limited Gas turbine engine fuel control system and regulating valves therefor
GB2432886A (en) * 1990-03-16 2007-06-06 Lucas Ind Plc Gas turbine engine reheat fuel control system and control valves therefor
GB2432886B (en) * 1990-03-16 2007-12-05 Lucas Ind Plc Gas turbine engine fuel control system and regulating valve therefor

Also Published As

Publication number Publication date
DE2110538A1 (de) 1971-09-16
FR2081729A1 (enrdf_load_stackoverflow) 1971-12-10
FR2081729B1 (enrdf_load_stackoverflow) 1975-07-04

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Legal Events

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