DEVELOPMENT OF A HIGH STRENGTH BRAZING ALLOY FOR THE AFT RETAINER
Technical Report
·
OSTI ID:4840237
Design and initial stress requirements established for the aft retainer necessitated the utilization of brazing for part joining and the development of a brazing filler to meet stress requirements. A brazing filler was developed which gained a part of its strength through precipitation hardening. The brazing alloy exhibited excellent 1000 hour rupture strength, tensile properties, and oxidation resistance to temperatures of 1700 deg F. Its brazing temperature is 2150 to 2175 deg F. The alloy met or exceeded the properties required for service in the aft retainer. Preliminary specifications for application of the alloy to parts manufactured were developed and are reported. (auth)
- Research Organization:
- General Electric Co. Aircraft Nuclear Propulsion Dept., Cincinnati
- NSA Number:
- NSA-16-019243
- OSTI ID:
- 4840237
- Report Number(s):
- DC-61-3-34
- Country of Publication:
- United States
- Language:
- English
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