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  • MECHANICAL ENGINEERING  (3)
  • 1985-1989  (3)
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Year
  • 1
    facet.materialart.
    Unknown
    Filament winding - Waking the sleeping giant (1985)
    In:  Other Sources
    Details
    Publication Date: 2011-08-19
    Description: The use of filament winding (FW) in the production of aerospace composite structures is examined. The FW process applies spools of fiber and prepreg tow or prepreg tape to a male mandrel; the process is more efficient and cost effective than metallic construction. The fibers used in FW and the curing process are explained. The reduced storage and fabrication costs that result from FW are discussed. The use of FW to produce a filament-wound case for a solid rocket motor and the substructure and skin of an aircraft fuselage are described. Areas which require further development in order to expand the use of FW are listed and discussed.
    Keywords: MECHANICAL ENGINEERING
    Type: Aerospace America (ISSN 0740-722X); 24; 44-46
    Format: text
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 2
    facet.materialart.
    Unknown
    Rapid adhesive bonding of thermoplastic composites and titanium with thermoplastic adhesives (1986)
    In:  Other Sources
    Details
    Publication Date: 2011-08-19
    Keywords: MECHANICAL ENGINEERING
    Type: Journal of Aircraft (ISSN 0021-8669); 23; 545
    Format: text
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 3
    facet.materialart.
    Unknown
    Rapid adhesive bonding of advanced composites and titanium (1985)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: Rapid adhesive bonding (RAB) concepts utilize a toroid induction technique to heat the adhesive bond line directly. This technique was used to bond titanium overlap shear specimens with 3 advanced thermoplastic adhesives and APC-2 (graphite/PEEK) composites with PEEK film. Bond strengths equivalent to standard heated-platen press bonds were produced with large reductions in process time. RAB produced very strong bonds in APC-2 adherend specimens; the APC-2 adherends were highly resistant to delamination. Thermal cycling did not significantly affect the shear strengths of RAB titanium bonds with polyimide adhesives. A simple ultrasonic non-destructive evaluation process was found promising for evaluating bond quality.
    Keywords: MECHANICAL ENGINEERING
    Type: AIAA PAPER 85-0750
    Format: text
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
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