MATERIAL - BRAZED HONEYCOMB PANELS - STRUCTURAL REPAIR - EVALUATION OF
Abstract
On the basis of static shear and flexure fatigue tests, it is recommended that 97Ag-3Li braze all foil be used when repair TIG spot welding of 17-7PH stainless steel. This alloy can produce a spot welded-brazed joint which has 11% more static lap shear strength and 114% more flexure fatigue strength. TIG braze joints should not be used as they have less strength than normal TIG spot welded 17-7PH. The filler wire added to the weld nugget should be 17-7PH in preference to Type 308.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 11, 1963
- Accession Number
- AD0423075
Entities
People
- R. L. Jones
Organizations
- General Dynamics