EP2358590A2 - Système de montage pour fixer un monument à une position désirée dans une cabine d'aéronef - Google Patents

Système de montage pour fixer un monument à une position désirée dans une cabine d'aéronef

Info

Publication number
EP2358590A2
EP2358590A2 EP09760753A EP09760753A EP2358590A2 EP 2358590 A2 EP2358590 A2 EP 2358590A2 EP 09760753 A EP09760753 A EP 09760753A EP 09760753 A EP09760753 A EP 09760753A EP 2358590 A2 EP2358590 A2 EP 2358590A2
Authority
EP
European Patent Office
Prior art keywords
mounting system
coupling element
coupling
receiving device
struts
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Withdrawn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
EP09760753A
Other languages
German (de)
English (en)
Inventor
Iwan Pangalila
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 EP2358590A2 publication Critical patent/EP2358590A2/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/04—Galleys

Definitions

  • the present invention relates to a mounting system for mounting a structural monument in a desired position in an aircraft cabin. Furthermore, the invention relates to the use of such a mounting system for fastening an aircraft galley in a desired position in an aircraft cabin.
  • a modular aircraft galley which comprises a main body with a plurality of subjects.
  • various devices such. an oven or a microwave oven.
  • different sized boxes are accommodated in the compartments of the base body, in which service products required to supply the passengers on board the aircraft, such as e.g. Food or drinks can be accommodated.
  • the invention has for its object to provide a mounting system for mounting a Strukturmonuments in an aircraft cabin, which allows a more flexible positioning of the Strukturmonuments in the aircraft cabin and a more flexible design of the Strukturmonuments.
  • a mounting system for fastening a structural monument in a desired position in an aircraft cabin comprises a rich of Strukturmonuments connectable to a body of the Strukturmonuments carrier element.
  • the carrier element may be provided to be connected to the structural monument base body on an underside of the structural monument base body in the region of a base element of the structural monument base body.
  • the carrier element can also be embodied integrated with the main body of the structural monument and form, for example, a part of a bottom of the structural monument main body. In the state connected to the main body of the structural monument, a bottom element of the structural monument main body is preferably supported by the carrier element.
  • the mounting system comprises a receiving device which can be fastened in the region of a floor of the aircraft cabin.
  • the receiving device may be provided for, in the region of a cross member of the aircraft structure supporting a floor panel of the aircraft cabin at the one of the
  • Cross beams supported floor panel and / or directly attached to the cross members of the aircraft structure are provided.
  • a first coupling element is mounted, which is adapted to connect the carrier element with the attachable in the region of a floor of the aircraft cabin receiving device.
  • the mounting system according to the invention can also be equipped with a plurality of first coupling elements. If the carrier element is intended to be connected to the basic body of the structural monument to be fastened in a desired position in an aircraft cabin, the structural monument main body and thus the entire structural monument can be connected via the carrier element and the first coupling element with receiving device and thus anchored in the floor area of the aircraft cabin. The support element and the first coupling element thus provide for a decoupling of the Strukturmonumentgrund stressess of the receiving device.
  • the mounting system according to the invention for fastening a structural monument to a desired position in an aircraft cabin further comprises a retaining element that can be connected to the base body of the structural monument in a ceiling region of the structural monument.
  • a second coupling element is mounted, which is adapted to connect the holding element with a structurally fixed component of the aircraft.
  • the mounting system according to the invention can also be equipped with a plurality of second coupling elements.
  • the structurally solid component may be a component rigidly connected to the aircraft structure, but also a part of the aircraft structure itself. Similar to the carrier element and the first coupling element, the holding element and the second coupling element attached to the holding element also ensure decoupling of the structured monument base body from an attachment point on the structurally fixed component. The design of the Strukturmonuments can thus be designed regardless of the position of the attachment point to the structurally solid component.
  • the mounting system according to the invention thus enables a more flexible design of the structural monument, so that the design of the structural monument can, if required, be adapted more easily to specific customer requirements. Furthermore, a greater flexibility in the choice of the positions of the attachment points can be achieved by the decoupling of the Strukturmonumentgrund stressess of the ground and Deckenssei- term attachment points. As a result, if necessary, the position of the structural monument in the aircraft cabin can be varied much more easily and adapted to specific customer requirements.
  • the receiving device may comprise at least one rail.
  • the rail may for example be designed in the form of a conventional seat rail and comprise an anchoring element for anchoring the rail in the region of the floor of the aircraft passenger cabin and a receiving area.
  • the receiving region of the rail can be formed by a C-profile element, in which alternately circular and slot-shaped openings are formed.
  • the first coupling element can be connected to the receiving device at different positions along the rail.
  • a stable base-side attachment of the structure monument is made possible on flexible, selectable positions.
  • a particularly flexible positioning of the Strukturmonuments is possible if the recording device several Includes rails that extend in different directions, that are aligned at different angles relative to a longitudinal axis of the aircraft cabin.
  • the receiving device may also include a plurality of 5 can be fastened in the region of the bottom of the aircraft cabin individual receiving elements.
  • the receiving elements can be fastened in a specific pattern in the region of the floor of the aircraft cabin.
  • the pattern formed by the receptacles may be a uniform or irregular dot grid having rectangular or square soles, or a dot pattern defining a curved arcuate structure, an oval structure, or a circular structure.
  • the first coupling element may comprise a support structure for supporting the support element and a fastening element.
  • the fastening element is designed to be complementary to a receiving region of the receiving device and serves to connect the first coupling element to the receiving device.
  • the receiving device comprises a seat rail
  • the fastening element of the first coupling element preferably has a head which, for receiving in a circular opening of the receiving region of the
  • seat rail is suitable.
  • the fastening element can then be displaced relative to the rail until the head of the fastening element is arranged in a section of the receiving region of the rail which has a merely slot-shaped opening.
  • the head of the fastener is then passed through the slot-shaped opening of the fastener.
  • the first coupling element preferably further comprises a locking device.
  • the fastening element In the unlocked state of the locking device, the fastening element is preferably displaceable relative to the support structure of the first coupling element in the receiving region of the receiving device.
  • the locked state of the locking device the fastening element is fixable in a desired position in the receiving area of the receiving device and relative to the support structure.
  • the locking device in the unlocked state, can release a spring, which displaces the fastening element in the receiving region of the receiving device and relative to the supporting structure of the first coupling element, until the fastening element in the receiving element is in the locked state. rich of the receiving device has reached a position in which the fastener can be fixed in the receiving area of the receiving device.
  • the locking device may also be designed so that, in the unlocked state, it allows a manual displacement of the fastening element in the receiving region of the receiving device and relative to the support structure.
  • a locking of the locking device can only cause the fastening element to be fixed relative to the support structure of the first coupling element and thus also no longer be displaceable in the receiving region of the receiving device.
  • an additional attachment means such as e.g. a screw or the like may be provided for fixing the fastening element in the receiving area of the receiving device.
  • the fastening element i5 is fixed in the locked state of the locking device by the locking device itself in a desired position in the receiving area of the receiving device.
  • the locking means may be configured such that its locking causes the fastener to be raised or lowered relative to the support structure and thereby in the receiving area
  • the recording device is anchored.
  • raising the fastener relative to the support structure may cause a head of the fastener to be urged against a slot-shaped opening of the receptacle of the receptacle defining arms of a c-shaped member forming the receptacle of the receptacle and thereby in position
  • the support structure of the first coupling element may comprise a base element, which is supported in a connected to the receiving device state of the first coupling element on the receiving device.
  • the base element may be formed, for example, in the form of a frame.
  • the first coupling element preferably comprises a connecting element which serves to connect the first coupling element to the carrier element.
  • the connecting element may for example be provided with suitable bores which serve to receive corresponding fastening devices, such as screws for fastening the connection element to the carrier element.
  • a damping element is preferably arranged between the base member and the connecting element.
  • the carrier element of the mounting system according to the invention for fastening a structural monument in a desired position in an aircraft cabin may comprise a plurality of support struts.
  • the support struts are preferably shaped and positioned such that forces transmitted via outer and / or intermediate walls of the structural monument base body are introduced at least partially into the support element in the region of the support struts in the state of the support element connected to the main body of the structural element.
  • the support struts of the support element are preferably shaped and positioned such that they carry at least sections of outer and / or intermediate walls of the Strukturmonu- ment basic body when the support member is intended to be connected to the Strukturmonumentgroundianu.
  • the carrier element of the mounting system may comprise a plurality of stiffening struts for stiffening the carrier element and thus increasing its mechanical load capacity.
  • the stiffening struts may extend at an angle to the support struts of the support member, for example perpendicular to the support struts or diagonally to the support struts.
  • the carrier element may further comprise a plurality of positioning struts for positioning an outer and / or intermediate wall of the
  • the carrier element 20 comprise structural monument body relative to the carrier element.
  • two mutually parallel positioning struts may be provided to sandwich an outer or an intermediate wall of the structural monument main body or portions of an outer or intermediate wall of the structural monument main body.
  • the carrier element may have a plurality of
  • the second coupling element of the mounting system may comprise a connecting element for connecting the second coupling element to the holding element.
  • the connecting element of the second coupling element is designed in the form of a tripod or a four-leg.
  • the legs of the connecting element of the second coupling element 5 can extend from an upper side of the retaining element that can be connected to the base body of the structural element in a ceiling region of the structural element.
  • the connecting element of the second coupling element can be rigid be fixed to the holding element.
  • the connecting element of the second coupling element and the retaining element are designed such that the connecting element of the second coupling element can be fastened to the retaining element at different positions.
  • the attachment of the connecting element of the second coupling element to the holding element can be effected by means of suitable fastening devices, such as screws.
  • the second coupling element preferably further comprises a variable in length fastener for connecting the holding member with the structural member of the aircraft.
  • the possible length variation of the fastener is greater than 2.5 cm.
  • the fastening element of the second coupling element may comprise a first tension rod pivotally connected to the connecting element of the second coupling element.
  • the second coupling element may comprise a second tension rod pivotally connected to the first tension rod.
  • the tension rods pivotably connected to the connecting element of the second coupling element allow a relatively flexible choice of the fastening position of the second coupling element on the structure-fixed component or the aircraft structure itself. If the second coupling element comprises a first and a second tension rod, only the second tension rod can be used to connect the second second coupling element with the structure-fixed component, the aircraft be provided. Alternatively, however, it is also possible to fix both an end remote from the connecting element of the second coupling element of the first tie rod and an end facing away from the first tie rod end of the second tie rod on a structurally solid component of the aircraft.
  • the first and / or second tension rod of the second coupling element is / are telescopically formed.
  • the holding element may also comprise a plurality of support struts which are shaped and positioned such that forces 5 transmitted via outer and / or intermediate walls of the structure monument base body in the state of the holding element connected to the main body of the structure monument are at least partially in the region of the support struts be introduced into the holding element.
  • the holding element may have a plurality of stiffening struts for stiffening the holding element, which may be similar to the stiffening struts of the carrier element at an angle, preferably perpendicular or diagonal to the support struts.
  • the holding element may comprise a plurality of connecting struts for fixing the second coupling element to the holding element.
  • the holding element for each second coupling element may have three mutually parallel struts, which are formed as connecting struts and / or support struts. The legs of a formed in the form of a four leg connecting element of the second coupling element can then be supported on the connecting struts and / or support struts.
  • the above-described mounting system can be used in a particularly advantageous manner for fastening an aircraft galley in a desired position in an aircraft cabin.
  • FIG. 1 shows a basic body of a structural monument, which is connected to a carrier element and to a holding element of a mounting system for fastening the structural monument in a desired position in an aircraft cabin,
  • FIGS. 2a to 2d show different embodiments of a carrier element and a receiving device of a mounting system for fastening a structural monument in a desired position in an aircraft cabin
  • FIG. 3 shows a three-dimensional illustration of a first coupling element for connecting a carrier element to a receiving device of a mounting system for fastening a structural monument in a desired position in an aircraft cabin
  • FIG. 4 shows a cross-sectional view of the first coupling element according to FIG. 3 and FIG. 4
  • FIG. 5 shows a detail of a second coupling element for connecting a holding element of a mounting system for fastening a
  • Structure monument in a desired position in an aircraft cabin with a structurally fixed component of an aircraft shows.
  • the structural monument may be, for example, an aircraft galley.
  • a lower side of a base plate 16 of the structural monument base 14 rests on the carrier element 12.
  • Outer walls 18, 20, 22 of the structural element main body 14 extend around a circumference of the carrier element 12.
  • the shape of the carrier element 12 can be adapted to the design of the structural element main body 14.
  • the carrier element 12 has a plurality of support struts 26 which, in the state of the carrier element 12 connected to the base body 14 of the structure monument, support sections of intermediate walls 28 of the structured monument base body 14 (see FIG. 1). The forces transmitted to the carrier element 12 via the sections of the intermediate walls 28 are thus introduced into the carrier element 12 in the region of the reinforced support struts 26.
  • the carrier element 12 is provided with diagonally extending stiffening struts 33. Furthermore, the carrier As will be explained in more detail later, serve the connecting struts 34, 36 to fasten a first coupling element 38 to the support member 12 (see Figure 3). Relative to outer struts 40, 42 form the connecting struts 34, 36 5 together with the connecting struts 34, 36 connecting intermediate struts 44, 46 on the outer struts 40, 42 adjacent Vorspr ⁇ nge 48. The projections 48 are connected to the Strukturmonumentground manipulate 14 state of the support member 12 in received corresponding recesses which are formed in the outer walls 18, 24 of the Strukturmonumentgrund stressess 14.
  • the mounting system 10 further comprises a mounting device 50 which can be fastened in the area of the floor of the aircraft cabin.
  • the mounting device 50 comprises a plurality of rails 52 which can be fastened in the area of the floor of the aircraft cabin.
  • the i5 rails 52 can be fastened to a floor panel supported by cross members of the aircraft structure, but also directly to the cross members of the aircraft structure itself.
  • the rails 52 can be fastened at different positions in the region of the floor of the aircraft cabin.
  • the receiving device 50 may have a different number of
  • 2o rails 52 include.
  • the first coupling element 38 serves to connect the carrier element 12 to a rail 52 of the receiving device 50.
  • the first coupling element 38 5 illustrated in FIGS. 3 and 4 comprises a support structure 54, which comprises a base element 56, a connecting element 58 serving to connect the first coupling element 38 to the carrier element 12, and a damping element 60 positioned between the base element 56 and the connecting element 58 ,
  • the first coupling element 38 comprises a fastening element 62.
  • the rail 52 of the receiving device 50 0 comprises a receiving region 64 formed by a C-profile element, in which alternately circular and slot-shaped openings 66, 68 are formed.
  • the fastening element 62 is designed to be complementary to the receiving region 64 of the rail 52.
  • the fastening element 62 may have a head 5 which is provided for receiving in a circular opening 66 of the receiving region 64.
  • the first coupling element 38 furthermore comprises a locking device 70.
  • the fastening element 62 In the unlocked state of the locking device 70, the fastening element 62 can be displaced relative to the support structure 54 in the receiving region 64 of the rail 52. As a result, for example, a head of the fastening element 62 can be brought into a position where it is held by a slot-shaped opening 38 of the receiving region 64 of the rail 52 delimiting arms of the C-profile element in the receiving region 64 of the rail 52.
  • the locking device 70 ensures that the fastening element 62 is fixed relative to the support structure 54 of the first coupling element and the rail 52.
  • the connecting struts 34, 36 of the carrier element 12 are provided with bores 72, 74.
  • the connecting element 58 of the first coupling element 38 corresponding holes are formed.
  • the mounting system further comprises a retaining element 76, which, as can be seen in FIG. 1, can be connected to the structural monument main body 14 in a ceiling region of the structural monument.
  • the holding element 76 comprises a plurality of support struts 78 which, in the state of the holding element 76 connected to the structure monument base body 14, are directly separated from outer walls 18, 24 or individually
  • the retaining element 76 comprises connecting struts 82, 84, which each serve to connect a second coupling element 86 to the retaining element 76.
  • the mounting system 10 comprises two second coupling elements 86.
  • each second coupling element 86 serves to fasten the retaining element 76 and thus the structural monument main body 14 to a structural component of the aircraft.
  • the structurally solid component may be a rigidly fixed to the aircraft structure Component or the aircraft structure itself.
  • each second coupling element 86 comprises a four-legged connector 88.
  • the four legs 90, 92, 94, 96 of the connector 88 are braced on a support strut 78 and two connecting struts adjacent to the support strut 78 82, 84 of the holding element 76 from.
  • a variable in length fastener 97 for connecting the support member 76 is connected to a structural component of the aircraft.
  • the fastening element 97 comprises a first pull rod 98 which is pivotally connected to the connecting element 88.
  • a second pull rod 100 is pivotably articulated on an end of the first pull rod 98 facing away from the connecting element 88.
  • An end of the second tension rod 100 facing away from the first tension rod 98 can be connected to the structural component of the aircraft.
  • the end of the first pull rod 98 facing away from the connecting element 88 in the region of the connection of the first pull rod 98 with the second pull rod 100 can be connected to a structure-fixed component of the aircraft.
  • the first and / or the second pull rod 98, 100 is / are telescopically formed. As a result, tolerances can be compensated. Furthermore, it is possible to move the structural monument base body with the holding element 76 fastened thereto and fix it in a different position, without it being necessary for this purpose to release the connection of the holding element 76 made via the connecting element 88 with the structural component of the aircraft.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)

Abstract

L'invention concerne un système de montage (10) pour la fixation d'un monument à une position désirée dans une cabine d'aéronef. Le système de montage selon l'invention comprend un élément support (12) pouvant être relié à un corps de base (14) du monument dans une zone de socle du monument. Le système de montage (10) selon l'invention comprend également un dispositif récepteur (50) pouvant être fixé dans la zone du sol de la cabine d'aéronef, ainsi qu'un premier élément d'accouplement (38) monté sur l'élément support (12) et conçu pour relier l'élément support (12) au dispositif récepteur (50) pouvant être fixé dans la zone du sol de la cabine d'aéronef. Le système de montage (10) selon l'invention comprend enfin un élément de retenue (76) pouvant être relié au corps de base (14) du monument dans une zone de paroi supérieure du monument, ainsi qu'un deuxième élément d'accouplement (86) monté sur l'élément de retenue (76) et conçu pour relier l'élément de retenue (76) à un élément fixe de la structure de l'aéronef.
EP09760753A 2008-12-19 2009-11-23 Système de montage pour fixer un monument à une position désirée dans une cabine d'aéronef Withdrawn EP2358590A2 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US20312908P 2008-12-19 2008-12-19
DE200810064120 DE102008064120A1 (de) 2008-12-19 2008-12-19 Montagesystem zur Befestigung eines Strukturmonuments in einer gewünschten Position in einer Flugzeugkabine
PCT/EP2009/008326 WO2010078884A2 (fr) 2008-12-19 2009-11-23 Système de montage pour fixer un monument à une position désirée dans une cabine d'aéronef

Publications (1)

Publication Number Publication Date
EP2358590A2 true EP2358590A2 (fr) 2011-08-24

Family

ID=42220883

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09760753A Withdrawn EP2358590A2 (fr) 2008-12-19 2009-11-23 Système de montage pour fixer un monument à une position désirée dans une cabine d'aéronef

Country Status (4)

Country Link
US (1) US8882032B2 (fr)
EP (1) EP2358590A2 (fr)
DE (1) DE102008064120A1 (fr)
WO (1) WO2010078884A2 (fr)

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FR2975372B1 (fr) * 2011-05-19 2013-07-05 Airbus Operations Sas Aeronef comprenant des moyens ameliores de support d'une structure de plancher
US8727686B2 (en) 2012-03-23 2014-05-20 B/E Aerospace, Inc. Device for attaching an aircraft monument
DE102012005934A1 (de) * 2012-03-26 2013-09-26 Sell Gmbh Befestigungsstruktur für eine Flugzeug-Galley
DE102012005933A1 (de) * 2012-03-26 2013-09-26 Sell Gmbh Modulare Flugzeug-Galley
US9359078B2 (en) * 2012-03-28 2016-06-07 B/E Aerospace, Inc. Aircraft galley monument structure
US9599138B2 (en) 2012-03-28 2017-03-21 B/E Aerospace, Inc. Aircraft monument integrated attachment device
USD711305S1 (en) * 2012-04-13 2014-08-19 B/E Aerospace, Inc. Aircraft galley
US9108716B2 (en) 2012-11-06 2015-08-18 The Boeing Company Aircraft having a recessed cavity in an aft pressure bulkhead wall surface and a galley moved rearwardly into the recessed cavity increasing floor space in front of the galley
EP2815972A1 (fr) * 2013-06-17 2014-12-24 Airbus Operations GmbH Conteneur de transport comprenant un module d'étagère de stockage et un module de transport, véhicule avec un tel conteneur et méthode d'utilisation d'un tel conteneur
DE102015206707A1 (de) * 2015-04-15 2016-10-20 Airbus Operations Gmbh Monument für eine Kabine eines Fahrzeugs und Befestigungsanordnung
DE102015206713A1 (de) 2015-04-15 2016-10-20 Airbus Operations Gmbh Bausatz und Verfahren für einen Gehäuseaufbau eines Monuments für eine Fahrzeugkabine
US10933967B2 (en) 2017-12-15 2021-03-02 Airbus Americas, Inc. Partition wall in cabin of aircraft supporting monuments
DE102019108748A1 (de) * 2019-04-03 2020-10-08 Airbus Operations Gmbh Verstau- und Entnahmesystem für Behälter in einem Fahrzeug sowie ein Fahrzeug mit einem derartigen System
US11407484B2 (en) * 2019-06-14 2022-08-09 Airbus Americas, Inc. Standard cabin monument sub-structure

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Also Published As

Publication number Publication date
WO2010078884A2 (fr) 2010-07-15
WO2010078884A3 (fr) 2010-09-30
DE102008064120A1 (de) 2010-07-01
WO2010078884A4 (fr) 2010-11-25
US8882032B2 (en) 2014-11-11
US20110309194A1 (en) 2011-12-22

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