EP2497537A2 - Installation d'exercice anti-incendie mobile sous forme de fuselage d'avion - Google Patents

Installation d'exercice anti-incendie mobile sous forme de fuselage d'avion Download PDF

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Publication number
EP2497537A2
EP2497537A2 EP12156496A EP12156496A EP2497537A2 EP 2497537 A2 EP2497537 A2 EP 2497537A2 EP 12156496 A EP12156496 A EP 12156496A EP 12156496 A EP12156496 A EP 12156496A EP 2497537 A2 EP2497537 A2 EP 2497537A2
Authority
EP
European Patent Office
Prior art keywords
module
fuselage
seats
fire
module base
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.)
Granted
Application number
EP12156496A
Other languages
German (de)
English (en)
Other versions
EP2497537B1 (fr
EP2497537A3 (fr
Inventor
Jörg WINKLER
Hans Weber
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.)
KFT Fire Trainer GmbH
Original Assignee
Kidde Fire Trainers 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 Kidde Fire Trainers GmbH filed Critical Kidde Fire Trainers GmbH
Publication of EP2497537A2 publication Critical patent/EP2497537A2/fr
Publication of EP2497537A3 publication Critical patent/EP2497537A3/fr
Application granted granted Critical
Publication of EP2497537B1 publication Critical patent/EP2497537B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • A62C99/0081—Training methods or equipment for fire-fighting
    • 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

Definitions

  • the invention relates to a mobile fire-fighting training system in the form of at least one fuselage, which is composed of a plurality of fuselage modules, each having a module bottom and at least one module wall and which are arranged in an exercise position in the direction of a longitudinal axis of the fuselage one behind the other and connected to each other and by releasing Of connections in each case in a separating position can be brought, in which each individual fuselage module by means of a road transport vehicle is transportable.
  • the invention relates to a method for disassembling and transporting a mobile fire training system in the form of an aircraft fuselage, which is composed of a plurality of fuselage modules, wherein the fuselage modules, starting from an exercise position in which they are arranged in the direction of a longitudinal axis of the fuselage successively and interconnected are brought by releasing connections in each case in a singulating position and then each individual trunk module is transported by means of a road transport vehicle.
  • Fire-fighting training systems are generally of particular importance for the training and advanced training of firefighters or fire fighters - collectively referred to as firefighters in the following.
  • Realistic fire conditions and concomitantly realistic environments and spatial conditions are essential in order to prepare (prospective) firefighters as comprehensively as possible for real fires.
  • an exercise facility in the form of a building is known, which is composed of individual prefabricated modules, wherein the individual modules can be designed differently.
  • different training systems can be set up in this way.
  • Fire-fighting exercises in the form of an aircraft fuselage serve in accordance with the training and training of firefighters in the event of a fire of an aircraft.
  • stationary systems that are fixed locally fixed to a specific practice site.
  • Such permanently installed fire-extinguishing equipment is usually provided at airports. The fact that they only need to be set up once and are not intended for a relocation in the following, they offer the advantage that they are not bound to any size specifications.
  • the disadvantage of existing mobile fire-extinguishing equipment lies in the limitation of the external dimensions, primarily the width.
  • the permissible width of a vehicle or a good transported on it in the road for example, within the European Union to a maximum value of 2.55 m set. This value should not be exceeded by the respective road transport vehicle or by the mobile fire-fighting equipment, as the latter would otherwise only be transportable with the help of special vehicles and, on the other hand, a separate approval from the supervisory authorities would have to be obtained before transport via public transport is likely to take place.
  • mobile fire-extinguishing equipment - and thus also those in the form of an aircraft fuselage - are usually chosen so that they have the permissible dimensions for road traffic comply.
  • it also conforms to the width according to the 2.468m (8ft) bulk container standardized worldwide in ISO 668. If this is the case, the individual fuselage modules can be equipped with container corners made of cast steel according to ISO standard 1161 and can be transported in this way without costly adjustments, for example by means of a truck.
  • this strategy is applied in the field of container construction.
  • the container is divided into individual parts, both in the longitudinal and in the transverse direction. Due to the high regularity of the geometry of a container, a re-assembly of the individual modules to a complete container from the point of view of the necessary Workloads justifiable. Nevertheless, such approaches are avoided wherever possible, as they always require a high work input and are correspondingly time consuming and costly.
  • the object of the invention is to further develop a mobile fire-fighting training system in the form of at least one fuselage in such a way that it can exceed a width of 2.55 m in an exercise position, but in a transport position the standard values for normal road traffic, preferably the latitude according to ISO 668 , corresponds.
  • the object is achieved in that at least one fuselage module is convertible from the singulation position into a transport position in which a measured width of the fuselage module transversely to the longitudinal axis of the fuselage smaller than in the singulation position, wherein the module bottom consists of at least two parts which are collapsible in a direction transverse to the longitudinal axis of the fuselage.
  • a trained in this way fire training system has the possibility of reducing the width of the fuselage a desired flexibility in terms of transportability in public roads by means of a road transport vehicle. Even with hull widths greater than 2.55 m, a width of the hull module during transport of at most 2.55 m, preferably 2.438 m, can be achieved after pushing together.
  • the width of the fuselage modules measured transversely to the longitudinal axis of the fuselage is reduced relative to the singling position to such an extent that transport by means of a road transport vehicle is readily possible.
  • a subdivision of the module floor located in the fuselage modules along the longitudinal direction of the fuselage is provided in two parts. These can be subsequently pushed together transversely to the longitudinal axis of the fuselage, whereby the width of each individual fuselage module can be reduced so that a value of 2.55 m is not exceeded, optimally even reaches a value of 2.438 m.
  • An advantageous embodiment of the mobile fire extinguishing training system provides that at least one fuselage module has two module walls, which are each preferably rigidly connected to an associated part of the module base, wherein a measured from the module bottom height of a free end of the first module wall of the one part of Module bottom is smaller than a likewise measured from the bottom of the module height of an aligned perpendicular to the module bottom opening cross section below a free end of the second module wall of the other part of the module bottom.
  • the collapsibility of the two-part module base is made possible.
  • the collapsibility is ensured, as a collision of the free ends the two Modulwandept is prevented. Rather, the Modulwandung with the lower free end under in the course of a transfer of the fuselage module from its separation into its transport position into a free cross section of the fuselage module.
  • the increase in a difference between the height of the free end of the first module wall and the height of the free end may second Modulwandung above the module bottom can be additionally achieved that the two modulus walls are zususchiebbar by an increased degree to each other and, accordingly, a larger difference between the widths of the separating position and the transport position of the fuselage module can be realized.
  • each one of the one part of the module base facing seat is removable, so that in the transport position in each row of seats four seats are available, two of which are connected to one part of the module base and two with the other part of the module base.
  • the total width of the interior of a mobile fire-fighting training system of this type according to the invention is in its exercise or its singling position thus from the sum of the widths of the rows of seats with two seats on one part of the module base and the rows of seats with three seats and a transition between the Rows of seats on the other part of the module floor together.
  • a space gain created by the expanded seats in the interior of the fuselage module now allows insertion of the one, narrower part of the module floor in the other, wider part of the module floor so far that the rows of seats with two seats to middle seats of rows of seats, each with three seats bump.
  • the total width of a hull module in its transport position of a mobile fire-fighting training system according to the invention is therefore composed of the width of the two remaining seats of rows of seats with three seats on one part of the module base and the width of rows of seats with two seats on the other part of the module base.
  • the arrangement should be designed in such a way that the rows of seats with two seats are approximately so wide that as the sum of the width of the developed seat plus the width of the corridor between the rows of seats.
  • horizontally aligned rows of seats are preferably arranged with two seats, with another part of the module base - viewed in a plane perpendicular to the longitudinal axis of the fuselage - opposite a horizontal inclined at an angle between 5 ° and 65 °, wherein the arranged on this other part of the module base seats are also arranged inclined, the horizontally aligned rows of seats are removable, so that in the transport position connected to the other part of the module base inclined seat rows remain in a relation to the practice position unchanged arrangement.
  • Tilting a portion of the module floor in the manner described enables a simulation of a firefighting situation for a case where an aircraft is inclined transverse to the longitudinal axis of the fuselage.
  • a complete inclination of the fire-fighting equipment is conceivable.
  • this is associated with a great effort and is therefore not applied.
  • an inclination of an aircraft fuselage could occur, for example, in the event of damage to the landing gear of the aircraft.
  • the inclination of a part of the module base also includes that, together with this part, the rows of seats mounted thereon are tilted with the respective seats.
  • the other part of the module base retains its original horizontal orientation.
  • the inclined part is preferably the wider part of the module base.
  • At least one fuselage module has two module walls, each of which is preferably rigidly connected to an associated part of the module base wherein a height of a free end of the first module wall measured from the module bottom corresponds to a part of the module bottom of a height of a free end of the second module wall of another part of the module bottom, also measured from the module bottom.
  • Pushing together the two parts of the module bottom of a fuselage module designed in this way is only possible if there is a free space in the form of a distance between the free ends of the module walls. Since the free ends of both Modulwandungen are arranged at an equal height, they collide against each other during the pushing together. A "retraction" according to the explanation of the principle of operation of the previously described embodiment is no longer possible. Instead, a collapse is therefore possible only on such a level that corresponds to the distance between the free ends of the module walls.
  • a positionability of the rows of seats with the three seats in a rotated position makes it possible to reduce a width occupied by said rows of seats width and thus to allow a pushing together of the two parts of the module base.
  • a rotated position may, for example, be such that the rows of seats with the three seats, after being detached from the module bottom, are rotated about an axis parallel to the longitudinal axis of the fuselage module and, as it were, positioned in an "upright" position on the module floor.
  • a rotation of the rows of seats about an axis perpendicular to the module bottom axis or another axis is also conceivable.
  • such an embodiment of the mobile fire extinguishing system according to the invention is advantageous, which has a free space in the exercise position between the free ends of the respective parts of the module bottom associated module walls, which can be covered by means of a removable cover.
  • a fire-fighting training system should preferably be designed so that one of a part of the module base is transverse to the longitudinal axis of the fuselage measured width between 0.50 m and 2.00 m, preferably between 1.00 m and 1.50 m, and another part of the module base has a width measured transversely to the longitudinal axis of the fuselage of approximately 2.50 m, preferably approximately 2,438 m.
  • the approximately 2.50 m wide part of the module floor thus fills almost the full width allowed in road traffic.
  • the other between 0.50 m and 2.00 m, preferably between 1.00 m and 1.50 m wide part of the fuselage module should disappear accordingly in the course of pushing together completely in the first part.
  • a hull module in its transport position thus has a total width of approximately 2.50 m, with a bottom of such a module consisting entirely of the wider part of the module bottom. Disruptions in the footprint of the fuselage module in its transport position can thus be avoided, whereby the transport on a road transport vehicle is simplified.
  • a fire-fighting training system should be designed so that in the training position of the fuselage module, the two module walls together describe an arc in the form of a parabola.
  • Such a form of the module walls corresponds to the generally customary geometry of a passenger aircraft and, correspondingly, allows a maximum degree of realism in the simulation of a real fire.
  • an embodiment of the fire fighting exercise system according to the invention is advantageous in which the two parts of the module base by means of a linear drive, preferably by means of at least one hydraulically or pneumatically actuated fluid cylinder, relative to each other in the direction transverse to the longitudinal axis of the fuselage are displaced.
  • a purely mechanical spindle drive is possible.
  • the transfer of a fuselage module from its separation position into its exercise position is particularly easy to carry out by means of a fire extinguishing equipment designed in this way.
  • the object is achieved in that at least one trunk module is transferred, starting from the singulation position in a transport position in which a transverse to the longitudinal axis of the Aircraft fuselage measured width of the fuselage module is smaller than in the singulation position, wherein the module bottom consists of at least two parts which are pushed together in a direction transverse to the longitudinal axis of the fuselage, and that at least one fuselage module is transported in the transport position.
  • Such a method is particularly simple to carry out using a fire-fighting training system according to the invention.
  • FIG. 1 shows a section through a trunk module 2 of an inventive, in FIG. 1 not shown in its entirety fire extinguishing equipment 1 in a singling position.
  • the fuselage module 2 is moved downwards through a module floor 3 and to the sides and behind bounded above each by a left Modulwandung 4 and a right Modulwandung 5.
  • the left module wall 4 is fixed rigidly on a rigid part 6 of the module base 3 while the right module wall 5 is fixed rigidly on a movable part 7 of the module base 3.
  • Both module walls 4 and 5 each have a free end 8 and 9 above the module base 3. In an exercise or singulation position, an opening between these free ends 8 and 9 can be covered by means of a removable cover 13.
  • both walls 4 and 5 form the shape of a parabola, as is customary in passenger aircraft.
  • the free end 9 of the right module wall 5 is arranged so that a height H2 of the free end 9 above the module bottom 3 by such a measure is smaller than a height H1 of the free end 8 of the left module wall 4.
  • the movement of the part 7 can be effected for example via hydraulically or pneumatically driven fluid cylinder, but is also possible for example via a spindle drive.
  • a left row of seats 10 with three seats and a right row of seats 11 with two seats are fixedly connected to the rigid part 6 of the module base 3.
  • the right-hand seat 12 of the left-hand row of seats 10 must be removed so that there is sufficient space for the movable part 7 of the module base 3 including the module wall 5 and the row of seats 11 according to the double-headed arrow in FIG. 1 to move in the direction of the rigid part 6 of the module bottom 3.
  • the remote seat 12 may be placed, for example, in an inverted orientation on one of the fixed seats of the left or the right seat row 10 or 11 for the purpose of temporary storage during transport of the fire fighting exercise 1 and the fuselage module 2.
  • FIG. 2 shows the same fuselage module 2 FIG. 1 in the transport position.
  • the seat 12 is removed and the movable part 7 of the module base 3 is inserted to the left into the rigid part 6 of the module base 3.
  • the module walls 4 and 5 are shifted accordingly relative to each other. From the drawing it is clear that a restriction of movement of the part 7 in the direction of the part 6 is caused by the fact that on the one hand the rows of seats 10 and 11 do not have enough space available and on the other hand, the module walls 4 and 5 at the height H2 above the module bottom 3 against each other.
  • the height H2 is correspondingly designed so that a juxtaposition of the module walls just does not take place when the two parts 6 and 7 of the module base 3 are pushed together. A present in the exercise position gear between the rows of seats 10 and 11 has almost completely disappeared in the transport position.
  • a width B2 in the transport position of the fuselage module 2 is considerably smaller than a width B1 in the exercise or the singulation position of the fuselage module 2.
  • the width B2 assumes a value of 2.438 m and thus corresponds to the width of one according to ISO standard 668 standardized container.
  • container corners 15 arranged in accordance with ISO standard 1161. With the help of these container corners 15, it is particularly easy to transport the fuselage module 2 by means of a road transport vehicle, since it is a standardized device in the container corners 15, thanks to which the fuselage module 2 can be fixed on a variety of common trucks.
  • FIG. 3 a further fuselage module 2 'of another fire-extinguishing equipment 1' is shown in the singling position.
  • a difference to the fuselage module 2 consists merely in that the row of seats 10 arranged on the rigid part 6 of the module base 3 is inclined by an angle ⁇ of approximately 30 ° against a surface of the module base 3.
  • hull modules 2 ' is the seat 12, as well as the remaining seats of the seat 10, not removable.
  • both seats of the seat row 11 are removably arranged, so that a movement of the movable part 7 of the module base 3 in the direction of the rigid part 6 can continue to be made possible.
  • a corresponding transport position of the fuselage module 2 ' is in FIG. 4 displayed.
  • the two remote seats of the seat row 11 must be stored separately during transport of the fuselage module 2 '.
  • One the desired final result of a width reduction of the fuselage module 2 ' is achieved in a similar manner to the fuselage module 2.
  • FIG. 5 is a plan view of a fire extinguishing equipment 1, 1 'shown, which consists of a plurality of fuselage modules 2, 2'.
  • the individual fuselage modules 2, 2 ' are arranged one behind the other in the direction of a longitudinal axis 16 of an aircraft fuselage of the fire-extinguishing equipment 1, 1' and connected to one another.
  • the fire-extinguishing equipment 1, 1 ' is thus in its exercise position.
  • a viewed in the direction of the longitudinal axis 16 front part of the fire-fighting exercise system consists of fuselage modules 2 "and 2"', which have a narrowing of the fuselage forward according to a real aircraft shape. This has an effect only on a geometry of the module walls 4 and 5 which, in addition to their sectional shape of a parabola, also have a curvature in plan view.
  • FIG. 6 is an alternative embodiment of a fuselage module 2 of a fire extinguishing system 1 according to the invention in comparison to the FIGS. 1 to 3 shown in a singling position.
  • the heights H 1, H 2 of the free ends 8, 9 of the two module walls 4, 5 are identical in the example shown. So that a collapsibility of the two parts 6, 7 of the module base 3 is ensured, the cover 13 'in the example shown opposite the cover 13 from FIG. 1 significantly larger, that is wider in the sense of a width measured transversely to the longitudinal axis 16 of the fuselage. By removing the cover 13 ', in FIG.
  • the fuselage module 2 After pushing together of the two parts 6, 7 of the module base 3, that is, by the transfer of the alternative fuselage module 2 from its separation into its transport position, the fuselage module 2 lies in a shape according to FIG FIG. 7 in front.
  • the free ends 8, 9 of the module walls 4, 5 are minimally spaced and coupled together by a connection 17, which serves primarily to absorb tensile forces that may occur during transport.
  • the rotated rows of seats 10 are moved almost to the still horizontally aligned rows of seats 11 zoom.
  • the part 7 of the module base 3 is approximately completely inserted into the part 6 of the module base 3, so that the width B2 of the hull module 2 located in the transport position reaches a value of 2.438 m and is readily suitable for transport by means of a road transport vehicle.
  • this pushing together is performed via a rolling guide using a roller 18 on which a support member of the part 7 of the module base 3 is mounted and with the help of the part 7 can be very easily inserted into the part 6 of the module base 3.

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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)
EP12156496.7A 2011-03-09 2012-02-22 Installation d'exercice anti-incendie mobile sous forme de fuselage d'avion Active EP2497537B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE201110013464 DE102011013464A1 (de) 2011-03-09 2011-03-09 Mobile Feuerlöschübungsanlage in Form eines Flugzeugrumpfes

Publications (3)

Publication Number Publication Date
EP2497537A2 true EP2497537A2 (fr) 2012-09-12
EP2497537A3 EP2497537A3 (fr) 2012-10-10
EP2497537B1 EP2497537B1 (fr) 2014-04-16

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Application Number Title Priority Date Filing Date
EP12156496.7A Active EP2497537B1 (fr) 2011-03-09 2012-02-22 Installation d'exercice anti-incendie mobile sous forme de fuselage d'avion

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EP (1) EP2497537B1 (fr)
DE (1) DE102011013464A1 (fr)
ES (1) ES2470973T3 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107038945A (zh) * 2017-05-09 2017-08-11 中安（天津）航空设备有限公司 一种分体式演练装置

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102020119705A1 (de) * 2020-07-27 2022-01-27 Airbus Operations Gmbh Löscheinrichtung zum Anbringen an dem Gehäuse eines elektrischen Geräts, an einem Monument in der Kabine eines Flugzeugs oder in einem Hohlraum in der Struktur eines Flugzeugs

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69227682T2 (de) 1992-01-06 1999-06-10 Symtron Systems, Inc., Fair Lawn, N.J. Modularer brandbekaempfungstrainer

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2901282A (en) * 1957-01-15 1959-08-25 Stanley B Meaker Trailer construction
US5316480A (en) * 1993-02-10 1994-05-31 Ellsworth Thayne N Portable multiple module simulator apparatus
US5688136A (en) * 1995-12-15 1997-11-18 Symtron Systems, Inc. Fire fighting trainer

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69227682T2 (de) 1992-01-06 1999-06-10 Symtron Systems, Inc., Fair Lawn, N.J. Modularer brandbekaempfungstrainer

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107038945A (zh) * 2017-05-09 2017-08-11 中安（天津）航空设备有限公司 一种分体式演练装置

Also Published As

Publication number Publication date
DE102011013464A1 (de) 2012-09-13
EP2497537B1 (fr) 2014-04-16
ES2470973T3 (es) 2014-06-24
EP2497537A3 (fr) 2012-10-10

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