Airplane Floor Beam

In this i section beam is picked for designing the fuselage floor beam which is better in comparison.

Airplane floor beam.

1 a and it is composed of cabin floor strut frame cargo floor skin under floor beam sine wave beam stringer etc. The geometrical model of aircraft fuselage with the sine wave beam is exhibited in fig. The occupant seat and structure above the cabin floor have little influence on the crashworthiness of aircraft and they are simplified as two rigid blocks symmetrically distributed on. Customized ready to install floor panels optimized for the high loaded entrance and aisle areas of passenger cabin for a320 family aircraft.

Instead of structural hard points intercostal or optional beams or tracks etc. Beam region flanges preceding truss prior art date 2010 07 14 legal status the legal status is an assumption and is not a legal conclusion. Floor beam is a structural element of fuselage which is mainly used for providing horizontal space to aircraft crew and is fixed with fuselage skin. On the other hand efw engineering offers a variety of modifications and changes to aircraft cabin and.

Us8240606 b2 by willard n. In this project the design of aircraft floor beam which is optimized design for the improved strength 0manufacturing ability reduced cost and weight reduction. 5 integrated aircraft floor with longitudinal beams. Google has not performed a legal analysis and makes no.

Aircraft fuselage comprises frames 1 with outer skin 2 stringers 3 jointed with skin 2 and frames 1 and passenger cabin floor beams 4 located nearby fuselage neutral surface cargo floor transverse beams 5 and transverse ceiling beams 6. A floor beam assembly system and method for installing floor beams within a structure are provided. The floor beam has selected of i shape and connection provided to 0 fuselage with attachment bracket and other methods of joining.