GB651070A - Improvements in or relating to fluid control valves and to fire-extinguishing installations for aircraft - Google Patents

Improvements in or relating to fluid control valves and to fire-extinguishing installations for aircraft

Info

Publication number
GB651070A
GB651070A GB2609048A GB2609048A GB651070A GB 651070 A GB651070 A GB 651070A GB 2609048 A GB2609048 A GB 2609048A GB 2609048 A GB2609048 A GB 2609048A GB 651070 A GB651070 A GB 651070A
Authority
GB
United Kingdom
Prior art keywords
flap
valve
outlet
fire
close
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
GB2609048A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB2609048A priority Critical patent/GB651070A/en
Publication of GB651070A publication Critical patent/GB651070A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K11/00—Multiple-way valves, e.g. mixing valves; Pipe fittings incorporating such valves
    • F16K11/02—Multiple-way valves, e.g. mixing valves; Pipe fittings incorporating such valves with all movable sealing faces moving as one unit
    • F16K11/04—Multiple-way valves, e.g. mixing valves; Pipe fittings incorporating such valves with all movable sealing faces moving as one unit comprising only lift valves
    • F16K11/052—Multiple-way valves, e.g. mixing valves; Pipe fittings incorporating such valves with all movable sealing faces moving as one unit comprising only lift valves with pivoted closure members, e.g. butterfly valves
    • A—HUMAN NECESSITIES
    • A62—LIFE-SAVING; FIRE-FIGHTING
    • A62C—FIRE-FIGHTING
    • A62C3/00—Fire prevention, containment or extinguishing specially adapted for particular objects or places
    • A62C3/07—Fire prevention, containment or extinguishing specially adapted for particular objects or places in vehicles, e.g. in road vehicles
    • A62C3/08—Fire prevention, containment or extinguishing specially adapted for particular objects or places in vehicles, e.g. in road vehicles in aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • Public Health (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Mechanical Engineering (AREA)
  • Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)

Abstract

651,070. Fire-extinguishing systems. MACDONALD, I. G. Oct. 6, 1948, No. 26090. [Class 47 (ii)] [Also in Group XXIX] In a fire-extinguishing system on an aircraft, two valves 43, 44, Fig. 7, are mounted in adjacent engine nacelles 38, 39 respectively, the outlets 6 being interconnected by a pipe 45, while the outlets 5 lead to the respective engines and the inlets 4 are connected to extinguisher bottles 36, 37 respectively. The valves each comprise a flap 7, Fig. 1, spring-urged to close the inlet and adapted to engage one of two hinges 14, 15 slidable by a lever 18 so that inlet pressure moves the flap to close either outlet depending on which hinge is used. The lever is fixed to one end of a pin 19 movable by a lever 26, Fig. 6, connected through a link 27 to an armature 29 spring- urged to the position shown, in which the hinge 14 is engaged by the flap to close the outlet 6. Energization of a coil 33 aligns the armature between poles 32, thus moving the hinge 15 into engagement with the flap. Should a fire break out in one engine nacelle, e.g. 38, the pilot opens the bottles 36 and the fluid moves the flap of the valve 43 to cover the outlet 6 and flows through the outlet 5 on to the engine. If the fire is not extinguished, the pilot may energize the coil 33 of the valve 44, and movement of the armature causes an extension 48 of the link 27 to close a switch 50 which opens the bottles 37. The fluid moves the flap to close the outlet 5 and passes along the pipe 45, through the outlets 6, 5 of the valve 43 to the engine in the nacelle 38. It is stated that the outlet of one valve may be connected to the inlet of the other valve, whereby fluid from the inlet of the first valve may be directed to any one of three outlets.
GB2609048A 1948-10-06 1948-10-06 Improvements in or relating to fluid control valves and to fire-extinguishing installations for aircraft Expired GB651070A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2609048A GB651070A (en) 1948-10-06 1948-10-06 Improvements in or relating to fluid control valves and to fire-extinguishing installations for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2609048A GB651070A (en) 1948-10-06 1948-10-06 Improvements in or relating to fluid control valves and to fire-extinguishing installations for aircraft

Publications (1)

Publication Number Publication Date
GB651070A true GB651070A (en) 1951-03-07

Family

ID=10238208

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2609048A Expired GB651070A (en) 1948-10-06 1948-10-06 Improvements in or relating to fluid control valves and to fire-extinguishing installations for aircraft

Country Status (1)

Country Link
GB (1) GB651070A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2516456A1 (en) * 1981-11-17 1983-05-20 Renault Distributor for car ventilating air - has equilateral triangular prism with single inner shutter blocking one of three outlets
EP0383368A2 (en) * 1984-07-24 1990-08-22 Kidde-Graviner Limited Fire protection systems
WO2004067931A1 (en) * 2003-01-31 2004-08-12 Honeywell International Inc. A three-way valve, in particular a valve for a turbocharger system
FR3022219A1 (en) * 2014-06-12 2015-12-18 Airbus Operations Sas AIRCRAFT COMPRISING A FIRE-FIGHTING SYSTEM
EP3909652A1 (en) * 2020-05-13 2021-11-17 Airbus Operations (S.A.S.) Aircraft including a propulsion assembly and a fire protection system for the propulsion assembly

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2516456A1 (en) * 1981-11-17 1983-05-20 Renault Distributor for car ventilating air - has equilateral triangular prism with single inner shutter blocking one of three outlets
EP0383368A2 (en) * 1984-07-24 1990-08-22 Kidde-Graviner Limited Fire protection systems
EP0383368A3 (en) * 1984-07-24 1991-07-03 Kidde-Graviner Limited Fire protection systems
WO2004067931A1 (en) * 2003-01-31 2004-08-12 Honeywell International Inc. A three-way valve, in particular a valve for a turbocharger system
FR3022219A1 (en) * 2014-06-12 2015-12-18 Airbus Operations Sas AIRCRAFT COMPRISING A FIRE-FIGHTING SYSTEM
EP3909652A1 (en) * 2020-05-13 2021-11-17 Airbus Operations (S.A.S.) Aircraft including a propulsion assembly and a fire protection system for the propulsion assembly
FR3110141A1 (en) * 2020-05-13 2021-11-19 Airbus Operations (S.A.S.) Aircraft comprising a propulsion unit and a propulsion unit fire-fighting system.
US11691039B2 (en) 2020-05-13 2023-07-04 Airbus Operations (S.A.S.) Aircraft comprising a propulsion assembly and a fire-fighting system for the propulsion assembly

Similar Documents

Publication Publication Date Title
US2818703A (en) Jet engine fuel, pressure ratio, and nozzle area control
GB651070A (en) Improvements in or relating to fluid control valves and to fire-extinguishing installations for aircraft
US2208689A (en) Automatic carburetor deicing system
GB1115968A (en) Device for controlling the bleed of air from a gas turbine engine compressor
US2395384A (en) Pilot control for primary and secondary fuels
US3621655A (en) Fuel control system for a gas turbine engine
GB925436A (en) Improvements in or relating to valves for controlling air flow
US2966210A (en) Fuel control for gas turbine power plants
GB673025A (en) Safety devices for internal combustion engines operating in a group
SU980733A1 (en) Powder fire extinguisher
US2812140A (en) Combustion control apparatus
GB1405666A (en) Electric control system for steam or gas turbines
GB705881A (en) Improvements in or relating to valves for controlling the flow of fluids
GB853706A (en) Valves for controlling re-heat fuel supply systems for an aircraft gas turbine engine
GB333996A (en) Improvements in or relating to the control of plunger valves
GB631600A (en) Valve, e.g. for use in fire extinguishing systems
GB733657A (en) Improvements in governing systems for prime movers, such as elastic fluid turbines
GB1120250A (en) Improvements in gas safety control valves
GB860848A (en) Improvements in or relating to control mechanisms and to uses thereof
IT1063032B (en) Blast furnace gas pressure control - at blast furnace mouth using a logic system to control gas turbines in parallel with the gas main throttling device (SW251076)
CN106247067A (en) A kind of explosion-proof valve of pipeline road
GB943303A (en) Fuel supply control mechanism for an engine
GB822443A (en) Fuel control systems for gas turbine engines
GB705897A (en) Automatic air relief device
GB657082A (en) Improvements in fuel supply systems for aircraft