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The mechanical structure of an aircraft is known as the airframe. This structure is typically considered to include the fuselage, undercarriage, empennage and wings, and excludes the propulsion system.
History, Alloys for airframe components & Safety
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aircraft alloys first alloy aluminum used developed strength structure light fuselage resistance primary sheet design also metal castings structures made
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| the Spirit of St | instance of | Some were produced as single copies or in small quantity | 0.80 | text |
| 355 | instance of | Time-honored alloys | 0.80 | text |
| 356 have been modified to produce higher levels of strength | instance of | Time-honored alloys | 0.80 | text |
| ductility | instance of | Time-honored alloys | 0.80 | text |
| 354 | instance of | New alloys | 0.80 | text |
| A356 | instance of | New alloys | 0.80 | text |
| A357 | instance of | New alloys | 0.80 | text |
| 359 | instance of | New alloys | 0.80 | text |
| Tens 50 were developed for premium-strength castings | instance of | New alloys | 0.80 | text |
| sea-water immersion | instance of | adhesive bonding has withstood adverse exposures | 0.80 | text |
| atmospheres.Fusion welded aluminum primary structures in airplanes are virtually nonexistent | instance of | adhesive bonding has withstood adverse exposures | 0.80 | text |
| because the high-strength alloys utilized have low weldability | instance of | adhesive bonding has withstood adverse exposures | 0.80 | text |
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