Fatigue Test of the Main Rotor Retention Components Used on Model OH- 58A/206A-1 Helicopter

Abstract

The report presents the results of a fatigue test conducted on eight sets of main rotor retention components used in the main rotor hub assembly of the MOdel OH-58A/206A-1 helicopter. The test was conducted to justigy an extension of the recommended service life of the retention components.

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Document Details

Document Type
Technical Report
Publication Date
Apr 30, 1971
Accession Number
AD0746984

Entities

People

  • R. Amancharla

Organizations

  • Bell Flight

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Assembly
  • Axial Loads
  • Centrifugal Force
  • Conformity
  • Diameters
  • Electric Motors
  • Engineering
  • Fatigue Life
  • Fatigue Tests (Mechanics)
  • Fretting
  • Helicopters
  • Hydraulic Cylinders
  • Hydraulic Tests
  • Inboard
  • Materials
  • Photographs
  • Tensile Strength

Readers

  • Aerospace Engineering
  • Instructional Design and Training Evaluation.