GB1335974A - Gas turbine engine fuel system - Google Patents

Gas turbine engine fuel system

Info

Publication number
GB1335974A
GB1335974A GB1335974DA GB1335974A GB 1335974 A GB1335974 A GB 1335974A GB 1335974D A GB1335974D A GB 1335974DA GB 1335974 A GB1335974 A GB 1335974A
Authority
GB
United Kingdom
Prior art keywords
parts
gas turbine
turbine engine
fuel system
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
Application number
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
Publication of GB1335974A publication Critical patent/GB1335974A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/16Sealings between relatively-moving surfaces
    • F16J15/32Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings
    • F16J15/3284Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings characterised by their structure; Selection of materials
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22Fuel supply systems
    • F02C7/222Fuel flow conduits, e.g. manifolds
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L41/00Branching pipes; Joining pipes to walls
    • F16L41/08Joining pipes to walls or pipes, the joined pipe axis being perpendicular to the plane of the wall or to the axis of another pipe
    • F16L41/088Joining pipes to walls or pipes, the joined pipe axis being perpendicular to the plane of the wall or to the axis of another pipe fixed using an elastic grommet between the extremity of the tube and the wall

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Compositions Of Macromolecular Compounds (AREA)

Abstract

1335974 Butyl rubber compositions DEFENCE SECRETARY OF STATE FOR 19 April 1971 [12 Feb 1970] 6782/70 Heading C3P [Also in Division F2] A butyl rubber fuel seal may be made by curing in a mould the following mixture: a copolymer of isobutylene and isoprene (100 parts by wt.), dimethylol phenolic resin (6 to 15 parts by wt.), zinc oxide (0 to 10 parts by wt.), stearic acid (1 to 5 parts by wt.), carbon black (50 to 100 parts by wt.), and chlorosulphonated polyethylene (3 to 8 parts by wt.)
GB1335974D 1971-04-19 1971-04-19 Gas turbine engine fuel system Expired GB1335974A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB678270 1971-04-19

Publications (1)

Publication Number Publication Date
GB1335974A true GB1335974A (en) 1973-10-31

Family

ID=9820651

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1335974D Expired GB1335974A (en) 1971-04-19 1971-04-19 Gas turbine engine fuel system

Country Status (1)

Country Link
GB (1) GB1335974A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2148912A (en) * 1982-09-06 1985-06-05 Aerosol Inventions Dev Gaskets for use in pressurised dispensers

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2148912A (en) * 1982-09-06 1985-06-05 Aerosol Inventions Dev Gaskets for use in pressurised dispensers

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Legal Events

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