Dynamic and Crashworthy Evaluation of the UH-1B, C, D, H, Medical Attendant's Seat

Abstract

The challenge was to evaluate the crashworthiness of the UH-1 Medical Attendant's Seat and investigate the feasibility of modifications to improve the seat and its restraint system. This report is a record of USAARL's involvement, from researching the background to achieve a proper direction for study, through accident statistics, stress analysis, dynamic test program, reduction of data, interpretation conclusion and finally feasible recommendations. The seat was found to be completely noncrashworthy and a direct contributor of serious injuries to its occupants mostly to the upper torso and head because of poor occupant restraint. Its construction and manufacture did not meet all of the design criteria of military seat specifications. The dynamic tests of the seat demonstrated that with the addition of an inertia reel, shoulder harness, and attachment of the lap belt to the floor a seat occupant could be satisfactorily restrained despite serious seat failure during a crash. The proposed modifications in kit form will provide the seat's occupant with the greatest increase in safety and retention, should crash occur, for the lowest dollar investment and 'down time' required for its installation.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1972
Accession Number
AD0737197

Entities

People

  • Errol B. Barber
  • Felix T. Aguilar
  • G. E. Tornquist
  • S. P. Desjardins
  • Stanley C. Knapp

Organizations

  • United States Army Aeromedical Research Lab

Tags

Communities of Interest

  • Biomedical

DTIC Thesaurus Topics

  • Accidents
  • Aircrafts
  • Biological Sciences
  • Cameras
  • Design Criteria
  • Dynamic Tests
  • Hazards
  • Helicopters
  • Load Cells
  • Materials
  • Measurement
  • Military Aircraft
  • Recording Systems
  • Shoulder
  • Tape Recording
  • Tensile Strength
  • Test And Evaluation

Readers

  • Aviation Safety Risk Assessment.
  • Explosive Engineering.
  • Software Engineering