Thermoplastic Rotorcraft Driveshafts Provide Weight Reduction with Improved Survivability

F-0070-2014-9556

5/20/2014

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Abstract
Content
ABSTRACT

A recent Phase II SBIR program focused on improving the survivability of driveshafts in rotorcraft applications while decreasing their weight. Thermoplastic composites were identified as a candidate material for achieving the goals of the program and a design was developed utilizing data from many previous sources and designs. Driveshafts were manufactured and validated against predicted static torque loads after withstanding a ballistic impact. The shafts showed a significant improvement in post-damaged strength over the legacy aluminum design with a weight reduction greater than 30%, exceeding all program goals. Automated Dynamics utilized recent process advancements in manufacturing both test coupons and driveshafts. This process takes advantage of unique aspects of in-situ composite consolidation to improve the bond affected between subsequent plies of pre-impregnated fiber reinforced thermoplastic materials on a continuous basis. Coupon test results demonstrated a 52% reduction in void content and greatly improved mechanical properties, further improving the performance over aluminum and thermoset composite driveshafts.

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DOI
https://doi.org/10.4050/F-0070-2014-9556
Citation
Michasiow, J. and August, Z., "Thermoplastic Rotorcraft Driveshafts Provide Weight Reduction with Improved Survivability," Vertical Flight Society 70th Annual Forum & Technology Display, Montréal, Québec, May 20, 2014, https://doi.org/10.4050/F-0070-2014-9556.
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Publisher
Published
5/20/2014
Product Code
F-0070-2014-9556
Content Type
Technical Paper
Language
English