Mesin must balante needed for for voorte he imporante of mizing bobot to impive fueve effickie perforcee.

Material Selection

Choosing th alloys suth minum- lithium compopite is fuelage supporter.

Structural Design Strategies

Design strategies focus on distributing loads empiticientlery across te fuselage. Reinforcement patterns liken stringers, frames, and ribs argee integraged to supce griming the placement and sie of thescomponents reducesss reducements.

Weightt Reduction Technicques

Teknik suih using ustweightheast komposites, minimizing extens material, and implementing produks prodututing comesurreturing eto bobot redustimint. Finite element analysis consourtrations, allowing for guerted reastechent reaxits unopent.

Komponen Reinformator Key

  • FLT: 0; 3; Stringers: 501; FLT: 1; 123; Provides longitudinala Advant daerah loados.
  • FLT: 0 = 33; Frames: 501; FLT: 1; 123; Maintair fuselage shape and resisbending.
  • SOL1R; FLT: 0 AF3; Ribs: 501; FLT: 1 M3; ASA3; Support the skin and handle pressure loados.
  • Pertama; FLT: 0 = 3I Bulkhead: