Floor Beam Aircraft

On the other hand efw engineering offers a variety of modifications and changes to aircraft cabin and.

Floor beam aircraft. Figure 7 shows the floor beam of figure 6 where the height of the mid section is substantially the same as the height of the end regions. Google has not performed a legal analysis and makes no. Instead of structural hard points intercostal or optional beams or tracks etc. According to one embodiment a floor beam assembly for installing a floor beam within a structure is provided.

Detailed description of embodiment s figure 3 is a schematic view of an i beam 20 for an aircraft fuselage floor the beam 20 comprising upper and lower flanges 23 24. A typical wood frame floor covered with carpet or vinyl flooring has a dead load of about 8 pounds per square foot. In this i section beam is picked for designing. The dead load on a floor is determined by the materials used in the floor s construction.

5 integrated aircraft floor with longitudinal beams. A floor beam assembly system and method for installing floor beams within a structure are provided. Tata group controlled tal manufacturing solutions ltd tal a wholly owned subsidiary of tata motors has dispatched 5 000th advanced composite floor beam acfb to plane maker boeing co. The floor beam which is fixed to the fuselage skin by the 0attachment bracket.

Here the floor beam has selected of i shape and connection provided to 0 fuselage with attachment bracket and other methods of joining. If there s wall board covered ceiling suspended from the underside of that floor the dead load increases to about 10 pounds per square foot. Us8240606 b2 by willard n. Customized ready to install floor panels optimized for the high loaded entrance and aisle areas of passenger cabin for a320 family aircraft.

Ep2593360b1 beam for an aircraft fuselage floor google patents beam for an aircraft fuselage floor download pdf info publication number. 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. Primary structure trump just boeing s new global airliner to 06 ch5 struct ion trusses a now i know how bridges an essment of the state art in design and new life to old jumbos 747 400bcf and bdsfs yesterday s. 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.

In this project the design of aircraft floor beam which is optimized design for the improved.