A nose structure (160) of an aircraft (100) includes an airframe (102). A wheel well assembly (194) is coupled to the airframe (102) and forms a portion of a nose landing gear bay (124). The wheel well assembly (194) includes a pressure deck (118) that extends from a right side (198) of the airframe to a left side (200) of the airframe and that forms a portion of a pressure boundary (104) delimiting a pressurized space (106) and a non-pressurized space (108). A floor-panel support (110) is supported by the pressure deck (118) in the pressurized space. The pressure deck and the floor-panel support form a portion of a flight deck floor (120) of a flight deck (122) of the aircraft (100). A plurality of transport elements (112) is located between the floor-panel support and the pressure deck. The plurality of transport elements is associated with at least one high-level system (114) of the aircraft (100).
NOSE STRUCTURE FOR AN AIRCRAFT AND METHOD OF MAKING AN AIRCRAFT
NASENSTRUKTUR FÜR EIN FLUGZEUG UND VERFAHREN ZUR HERSTELLUNG EINES FLUGZEUGS
STRUCTURE DE POINTE AVANT POUR UN AÉRONEF ET PROCÉDÉ DE FABRICATION D'UN AÉRONEF
2023-10-04
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
NOSE STRUCTURE FOR AIRCRAFT AND METHOD OF MAKING AIRCRAFT
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