A selected aerospace structure (F-14 wing beam) was successfully SSEB welded, thus demonstrating equipment capability to fabricate production parts. Tensile, fatigue and fracture toughness results are presented for a welded wing beam. Recommendations for further improvement or refinement of the SSEB welding equipment are included. A recommended industry equipment and a welding specification for aluminum, titanium and steel alloys are also included.
Sliding-Seal Electron-Beam Welding
1976
202 pages
Report
No indication
English
Manufacturing Processes & Materials Handling , Electron beam welding , Butt welding , Seam welding , Seals(Stoppers) , Sliding , Wear , Life expectancy , Fatigue tests(Mechanics) , Fracture(Mechanics) , Tensile strength , Test and evaluation , Wings , Beams(Structural) , Plates , Cylinders , Weldments , Aluminum alloys , Titanium alloys , Steel , Fighter aircraft , F-14 aircraft
Sliding-seal electron-beam welding
Tema Archive | 1976
|NTRS | 1980
|SAE Technical Papers | 2022
SAE Technical Papers | 1992
SAE Technical Papers | 1975