Advanced Development of a Helicopter Rotor Isolation System for Improved Reliability. Volume I. Summary Report.

Abstract

This report includes the results of the analytical and experimental phases of a helicopter rotor isolation reliability and maintainability (R and M) program on a UH-1 helicopter, which was modified through the addition of a Dynamic Antiresonant Vibration Isolator (DAVI). The final flight test phase demonstrated that the DAVI-modified vehicle had substantially lower vibration levels than the standard vehicle. Vertically, the two-per-rev vibration level was reduced to less than one-fifth that of the standard vehicle through the transition speed range and less than one-half at high speeds. An R and M analysis indicated the Army could realize an annual cost savings of approximately $12,000,000 if 1000 Army UH-1Hs were equipped with DAVI isolation systems. This savings is predicated on the following assumptions: (1) vibration-induced failures will be reduced in proportion to the vibration reduction afforded by the DAVI isolation system, and (2) the UH-1Hs are utilized at the rate of 20 flight-hours per month.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1977
Accession Number
ADA051318

Entities

People

  • Joseph H. Mcgarvey
  • Robert T. Jones

Organizations

  • Kaman Corporation

Tags

Communities of Interest

  • Air Platforms
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Actuators
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Control Systems
  • Fabrication
  • Failure Mode And Effect Analysis
  • Fuselages
  • Helicopters
  • Level Flight
  • Maintenance
  • Military Operations
  • Resonant Frequency
  • Test And Evaluation
  • Test Vehicles
  • United States
  • Vibration Isolators

Readers

  • Aerospace Engineering
  • Life Cycle Cost Analysis
  • Structural Dynamics.