LARGE SELF-CARRYING MONUMENT ASSEMBLY FOR AN AIRCRAFT AND AN AIRCRAFT HAVING SUCH A MONUMENT ASSEMBLY

A monument assembly (46) for an aircraft comprises at least one component of a primary structure of the aircraft, in particular a fuselage stiffening element (6, 84), a plurality of interconnected framework elements (12) for creating a self-carrying three-dimensional framework (13), wherein the at l...

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Bibliographische Detailangaben
Hauptverfasser:	RUETER, Jon, HEGENBART, Matthias, LERCHE, Thomas, SCHOPENHAUER, Wolfram, STURM, Ralph, BENTHIEN, Hermann, POPPE, Andreas, HAACK, Cord, SCHLIWA, Ralf, RADNY, Matthias
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	A monument assembly (46) for an aircraft comprises at least one component of a primary structure of the aircraft, in particular a fuselage stiffening element (6, 84), a plurality of interconnected framework elements (12) for creating a self-carrying three-dimensional framework (13), wherein the at least one fuselage stiffening element (6, 84) is attachable to a skin (4) of the aircraft and comprises at least one bracket, wherein the framework (13) is mechanically supported on the at least one bracket of the at least one component of the primary structure of the aircraft and wherein the framework (13) comprises a plurality of compartments (10, 15) accessible from an interior region of the aircraft, which compartments (10, 15) are adapted for receiving and holding cabin equipment modules. L'invention concerne un ensemble borne (46) pour un aéronef, qui comprend au moins un élément d'une structure principale de l'aéronef, en particulier un élément de raidissement de fuselage (6, 84), une pluralité d'éléments d'ossature reliés entre eux (12) pour créer une ossature tridimensionnelle autoportante (13), ledit élément de raidissement de fuselage (6, 84) pouvant être fixé à une enveloppe (4) de l'aéronef et comprenant au moins un support, l'ossature (13) étant supportée mécaniquement sur ledit support dudit élément de la structure principale de l'aéronef, et l'ossature (13) comprenant une pluralité de compartiments (10, 15) accessibles depuis une région intérieure de l'aéronef, lesquels compartiments (10, 15) sont conçus pour recevoir et retenir des modules d'équipement de cabine.