Brazed borsic/aluminum structural panels
Technical Report
·
OSTI ID:7317032
A fluxless brazing process has been developed that minimizes degradation of the mechanical properties of Borsic/aluminum composites. The process, which employs 718 aluminum alloy braze, is being used to fabricate full scale Borsic/aluminum-titanium honeycomb-core panels for Mach 3 flight testing on the YF-12 aircraft and ground testing in support of the Supersonic Cruise Aircraft Research (SCAR) Program. The manufacturing development and results of shear tests on full scale panels are presented. Nondestructive evaluation of brazed Borsic/aluminum honeycomb wing panel is discussed; the variables include shear strain, loads (forces), brazing temperature, and brazing time (min).
- Research Organization:
- National Aeronautics and Space Administration, Langley Station, VA (USA). Langley Research Center
- OSTI ID:
- 7317032
- Report Number(s):
- N-77-18220; NASA-TM-X-3432; L-11075
- Country of Publication:
- United States
- Language:
- English
Similar Records
Effects of fabrication and joining processes on compressive strength of boron/aluminum and borsic/aluminum structural panels
TF30 third-stage composite fan blade service program. Final technical report 1 Jul 1970--31 Dec 1977. [BORSIC/aluminum]
Fluxless aluminum brazing
Technical Report
·
Fri Mar 31 23:00:00 EST 1978
·
OSTI ID:6486567
TF30 third-stage composite fan blade service program. Final technical report 1 Jul 1970--31 Dec 1977. [BORSIC/aluminum]
Technical Report
·
Mon May 15 00:00:00 EDT 1978
·
OSTI ID:6446785
Fluxless aluminum brazing
Patent
·
Mon Dec 31 23:00:00 EST 1973
·
OSTI ID:4330556