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AIRCRAFT CABIN WITH SECONDARY AIRCRAFT CABIN STRUCTURE MOUNTED WITH ROTARY JOINTS AND METHOD FOR MOUNTING A SECONDARY AIRCRAFT CABIN STRUCTURE IN AN AIRCRAFT CABIN
The present invention pertains to an aircraft cabin (100) comprising a primary structure (40), a secondary aircraft cabin structure (50), and a plurality of interconnecting struts (20) coupling the primary structure (40) to the secondary aircraft cabin structure (50), each of the plurality of interconnecting struts (20) comprising engaging members (21,22) at the respective end portions for insertion into strut holding fixtures (11) of corresponding rotary joints (10) attached at each opposing end. Each of the rotary joints (10) comprises an outer shell segment (1) having the outer shape of a segment of a solid of revolution, the outer shell segment (1) having an opening (4) arranged in the outer surface, an inner shell segment (2) having the outer shape of the segment of the solid of revolution of the outer shell segment (1), the inner shell segment (2) being aligned concentrically with the outer shell segment (1) and spaced apart from the outer shell segment (1) by a compensation gap, and a strut holding fixture (11) having a hollow interior and a flange portion (13) and being arranged in the opening (4) so that the flange portion (13) extends within the compensation gap between the inner shell segment (2) and the outer shell segment (1).
AIRCRAFT CABIN WITH SECONDARY AIRCRAFT CABIN STRUCTURE MOUNTED WITH ROTARY JOINTS AND METHOD FOR MOUNTING A SECONDARY AIRCRAFT CABIN STRUCTURE IN AN AIRCRAFT CABIN
The present invention pertains to an aircraft cabin (100) comprising a primary structure (40), a secondary aircraft cabin structure (50), and a plurality of interconnecting struts (20) coupling the primary structure (40) to the secondary aircraft cabin structure (50), each of the plurality of interconnecting struts (20) comprising engaging members (21,22) at the respective end portions for insertion into strut holding fixtures (11) of corresponding rotary joints (10) attached at each opposing end. Each of the rotary joints (10) comprises an outer shell segment (1) having the outer shape of a segment of a solid of revolution, the outer shell segment (1) having an opening (4) arranged in the outer surface, an inner shell segment (2) having the outer shape of the segment of the solid of revolution of the outer shell segment (1), the inner shell segment (2) being aligned concentrically with the outer shell segment (1) and spaced apart from the outer shell segment (1) by a compensation gap, and a strut holding fixture (11) having a hollow interior and a flange portion (13) and being arranged in the opening (4) so that the flange portion (13) extends within the compensation gap between the inner shell segment (2) and the outer shell segment (1).
AIRCRAFT CABIN WITH SECONDARY AIRCRAFT CABIN STRUCTURE MOUNTED WITH ROTARY JOINTS AND METHOD FOR MOUNTING A SECONDARY AIRCRAFT CABIN STRUCTURE IN AN AIRCRAFT CABIN
FLUGZEUGKABINE MIT SEKUNDÄRER FLUGZEUGKABINENSTRUKTUR, DIE MIT DREHGELENKEN ANGEBRACHT IST, UND VERFAHREN ZUR MONTAGE EINER SEKUNDÄREN FLUGZEUGKABINENSTRUKTUR IN EINER FLUGZEUGKABINE
CABINE D'AVION AVEC STRUCTURE DE CABINE D'AÉRONEF SECONDAIRE MONTÉE AVEC DES JOINTS ROTATIFS ET PROCÉDÉ DE MONTAGE D'UNE STRUCTURE DE CABINE D'AÉRONEF SECONDAIRE DANS UNE CABINE D'AVION
BENTHIEN HERMANN (Autor:in) / SCHAEFER BASTIAN (Autor:in)
17.10.2018
Patent
Elektronische Ressource
Englisch
Cabin door locking device, aircraft or spacecraft cabin door and aircraft or spacecraft
Europäisches Patentamt | 2024
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