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 (102) to a left side (200) of the airframe (102) 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(106). The pressure deck (118) and the floor-panel support (110) 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 (110) and the pressure deck (118). Theplurality of transport elements (112) is associated with at least one high-level system (114) of the aircraft (100). 174 ) 60 172 172 102 112 116 110 112 198 248 118 248 200 104 --176 180 178-, ~ 228 124 _228
Nose structure for an aircraft and method of making an aircraft
2025-06-05
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
NOSE STRUCTURE FOR AIRCRAFT AND METHOD OF MAKING AIRCRAFT
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