Crash Testing of Helicopter Airframe Fittings

نویسندگان

  • Charles W. Clarke
  • William Townsend
چکیده

As part of the Rotary Wing Structures Technology Demonstration (RWSTD) program, a surrogate RAH-66 seat attachment fitting was dynamically tested to assess its response to transient, crash impact loads. The dynamic response of this composite material fitting was compared to the performance of an identical fitting subjected to quasi-static loads of similar magnitude. Static and dynamic tests were conducted of both smaller “bench level” and larger “full-scale” test articles. At the bench level, the seat fitting was supported in a steel fixture, and in the “full-scale” tests, the fitting was integrated into a surrogate RAH-66 forward fuselage. Based upon the lessons learned, an improved method to design, analyze, and test similar composite material fittings is proposed.

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تاریخ انتشار 2004