EP1306108A1 - Système d'extinction pour éteindre un incendie à l'intérieur d'une enceinte - Google Patents

Système d'extinction pour éteindre un incendie à l'intérieur d'une enceinte Download PDF

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Publication number
EP1306108A1
EP1306108A1 EP02020947A EP02020947A EP1306108A1 EP 1306108 A1 EP1306108 A1 EP 1306108A1 EP 02020947 A EP02020947 A EP 02020947A EP 02020947 A EP02020947 A EP 02020947A EP 1306108 A1 EP1306108 A1 EP 1306108A1
Authority
EP
European Patent Office
Prior art keywords
extinguishing
fire
air
separation module
nozzles
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.)
Withdrawn
Application number
EP02020947A
Other languages
German (de)
English (en)
Inventor
Thomas Dipl.-Ing. Grabow
Alexander Dipl.-Ing. Scheidt
Konstantin Dipl.-Ing. Kallergis
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.)
Airbus Operations GmbH
Original Assignee
Airbus Operations GmbH
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 Airbus Operations GmbH filed Critical Airbus Operations GmbH
Publication of EP1306108A1 publication Critical patent/EP1306108A1/fr
Withdrawn legal-status Critical Current

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Classifications

    • A—HUMAN NECESSITIES
    • A62—LIFE-SAVING; FIRE-FIGHTING
    • A62C—FIRE-FIGHTING
    • A62C99/00—Subject matter not provided for in other groups of this subclass
    • A62C99/0009—Methods of extinguishing or preventing the spread of fire by cooling down or suffocating the flames
    • 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
    • A—HUMAN NECESSITIES
    • A62—LIFE-SAVING; FIRE-FIGHTING
    • A62C—FIRE-FIGHTING
    • A62C99/00—Subject matter not provided for in other groups of this subclass
    • A62C99/0009—Methods of extinguishing or preventing the spread of fire by cooling down or suffocating the flames
    • A62C99/0018—Methods of extinguishing or preventing the spread of fire by cooling down or suffocating the flames using gases or vapours that do not support combustion, e.g. steam, carbon dioxide

Definitions

  • the invention relates to an extinguishing system for deleting an fire that has broken out inside a closed room, preferably inside the cabin or a cargo hold of a passenger aircraft, a device for nitrogen generation via a piping system with inside the extinguishing nozzles arranged in a closed space is in the closed for the purpose of supplying nitrogen Space, giving the fire what it needs to maintain it Withdrawn oxygen and extinguished the fire becomes.
  • the invention is based on the object of an extinguishing system for deleting an inside a closed space to create a fire that breaks out Extinguishing media are used.
  • a Storage container for storing pressure-liquefied halon it is provided that the reservoir over the piping system is connected to the extinguishing nozzles that the Halon first, the extinguishing concentration in short Extinguishing agent that builds up time via the extinguishing nozzles closed space is supplied, and that through the extinguishing nozzles and the piping system as a second extinguishing agent nitrogen-rich air, which provides long-term fire suppression ensures brought into the enclosed space becomes.
  • Embodiments of the invention are in the subclaims 2 to 11 described.
  • halon or an adequate, tested and approved substitute e.g. FM200 / FE36
  • the extinguishing concentration set up in no time.
  • This concentration is compared to that of extinguishing agents such as carbon dioxide, argon or nitrogen very low. Therefore - during or after the extinguishing agent is evenly in the closed Distributed or distributed space - with the nitrogen discharge started in the closed space and thus advantageously long-term fire suppression ensured.
  • the mixture in the cargo hold, consisting of halon / halon substitute and nitrogen-rich air must go to everyone Time of the suppression phase above a certain minimum concentration lie, whereby the extinguishing system at predetermined Room size to this required mixture concentration must be interpreted.
  • the drawing is an embodiment according to the invention shown.
  • the only figure shows an extinguishing system to delete an inside a closed room 1 outbreak of fire.
  • the system has a storage container 2 for storing pressure-liquefied halons or one Substitute on, the reservoir 2 over a Pipe system 3 arranged within the room 1 Extinguishing nozzles 4 is connected.
  • the halon is the first thing building up the effective concentration in a short time Extinguishing agent 5 via the extinguishing nozzles 4 in the closed space 1 fed.
  • the design concentration required to extinguish the fire is by massive introduction of the halon or one Substitute built up suddenly.
  • the extinguishing agents grip now depending on their predominant quenching effect in the combustion reaction on.
  • the main deletion effect of the halon 1301 is the inhibition in homogeneous phase (withdrawal of free Radicals from the chain reaction of combustion).
  • the Halon substitutes generally tend to displace oxygen and cooling on the combustion reaction.
  • An air separation module is also located above the piping system 3 7, which is nitrogen-rich air second Extinguishing agent 6 from supplied via an input line 11 generated atmospheric air, connected to the extinguishing nozzles 4, preferably via a check valve 9 the air separation module 7 can be designed as a molecular sieve, its sieving function over a membrane layer that is on porous Hollow fibers is applied is achieved.
  • the air separation module 7 can its input line 11th for example the turbine bleed air of aircraft engines fed and under a predetermined pressure in the air separation module 7 can be initiated.
  • the Input line 11 of the air separation module 7 to a blower an aircraft air conditioning system for providing compressed air be connected for the air separation module 7. in the Operation generates the air separation module 7 next to the extinguishing agent 2, long-term fire suppression in the room 1 ensures oxygen-rich air as a waste product is removed via the discharge line 8.
  • the first and second extinguishing agents 5 and 6 can either simultaneously or one after the other in a predetermined time interval via the extinguishing nozzles 4 into the closed space 1 be introduced.
  • the danger of the room 1 bursting from one Avoiding unwanted pressure build-up is in the walls of the closed space 1 at least one valve 10 as Pressure compensation device arranged.
  • the application of the fire extinguishing system according to the invention is not limited to airplanes. Rather, there are possible uses in loading and engine rooms of ships, in industrial production areas, in test rooms and Laboratories, companies, archives, libraries, galleries or also given museums as well as in the military field.

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  • Health & Medical Sciences (AREA)
  • Public Health (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
  • Fire-Extinguishing Compositions (AREA)
EP02020947A 2001-10-26 2002-09-19 Système d'extinction pour éteindre un incendie à l'intérieur d'une enceinte Withdrawn EP1306108A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10152964 2001-10-26
DE10152964A DE10152964C1 (de) 2001-10-26 2001-10-26 Löschsystem zur Löschung eines innerhalb der Kabine oder eines Frachtraumes eines Passagierflugzeuges ausgebrochenen Feuers

Publications (1)

Publication Number Publication Date
EP1306108A1 true EP1306108A1 (fr) 2003-05-02

Family

ID=7703850

Family Applications (1)

Application Number Title Priority Date Filing Date
EP02020947A Withdrawn EP1306108A1 (fr) 2001-10-26 2002-09-19 Système d'extinction pour éteindre un incendie à l'intérieur d'une enceinte

Country Status (5)

Country Link
US (1) US6676081B2 (fr)
EP (1) EP1306108A1 (fr)
JP (1) JP4190249B2 (fr)
CA (1) CA2409879C (fr)
DE (1) DE10152964C1 (fr)

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US7962991B2 (en) 2002-09-20 2011-06-21 Colgate-Palmolive Company Toothbrush
WO2011054683A3 (fr) * 2009-10-26 2011-08-25 Airbus Operations Gmbh Aéronef ou astronef et conteneur
DE202011102871U1 (de) * 2011-06-16 2011-09-09 Minimax Gmbh & Co. Kg Trockenrohrnetz für Feuerlöschanlagen mit chemischem Löschgas
WO2012099628A3 (fr) * 2011-01-23 2012-09-13 The Boeing Company Système de distribution d'agent d'extinction d'incendie à bord hybride

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US7962991B2 (en) 2002-09-20 2011-06-21 Colgate-Palmolive Company Toothbrush
WO2011054683A3 (fr) * 2009-10-26 2011-08-25 Airbus Operations Gmbh Aéronef ou astronef et conteneur
WO2012099628A3 (fr) * 2011-01-23 2012-09-13 The Boeing Company Système de distribution d'agent d'extinction d'incendie à bord hybride
US8733463B2 (en) 2011-01-23 2014-05-27 The Boeing Company Hybrid cargo fire-suppression agent distribution system
DE202011102871U1 (de) * 2011-06-16 2011-09-09 Minimax Gmbh & Co. Kg Trockenrohrnetz für Feuerlöschanlagen mit chemischem Löschgas

Also Published As

Publication number Publication date
JP2003144568A (ja) 2003-05-20
CA2409879A1 (fr) 2003-04-26
US20030136879A1 (en) 2003-07-24
JP4190249B2 (ja) 2008-12-03
CA2409879C (fr) 2008-05-20
US6676081B2 (en) 2004-01-13
DE10152964C1 (de) 2003-08-21

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