Sliding-Seal Electron-Beam Welding.
Abstract
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1976
- Accession Number
- ADA031901
Entities
People
- Harold P. Ellison
- Robert H. Witt
Organizations
- Grumman