Helicopter Troop/Passenger Restraint Systems Design Criteria Evaluation

Abstract

A systems analysis of a new restraint systems for troop restraint systems in helicopters was conducted. Hardware was designed and statically tested in accordance with the requirements of two proposed specifications. Design iterations were required on some hardware components, and three designs to be dynamically tested were developed. Dynamic testing of the restraint systems revealed additional weaknesses, design modifications were incorporated, and testing was reconducted until satisfactory results were obtained. The proposed specifications were modified and refined in accordance with the test results, with the net effect that the two specifications as they now stand define advanced restraint systems providing optimum restraint for occupants of Army aircraft which can be built within existing state of the art, are low in weight, and have reasonable cost.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1975
Accession Number
ADA012270

Entities

People

  • Richard W. Carr

Tags

Communities of Interest

  • Air Platforms
  • Human Systems

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircraft Industry
  • Aircrafts
  • Airframes
  • Army Aircraft
  • Drop Tests
  • Dynamic Tests
  • Failure Mode And Effect Analysis
  • Helicopters
  • Hydraulic Cylinders
  • Impact Tests
  • Load Cells
  • Rotary Wing Aircraft
  • Seats
  • Test And Evaluation
  • Test Methods
  • Two Dimensional

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