Recommended Design Modifications to the CH-47 Forward Rotor-Drive Gearbox

Abstract

The report describes the results of a study of modifications to existing helicopter power-train hardware for the purpose of reducing acoustic- frequency vibrations and noise. Mechanical vibration analysis methods were put to further tests by applying them to the redesign of CH-47C gearbox components. This program was undertaken carefully and methodically to avoid the excessive costs which often accompany hit-or-miss approaches to gearbox noise reduction. The results include vibration reduction predictions for a number of carefully documented designs. The key products in this overall effort are reduced bearing radial dynamic forces; thus, the results of this program are expected to have major impact upon bearing and gear lifetimes, in addition to the obvious benefits in the area of gearbox noise.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1973
Accession Number
AD0769062

Entities

People

  • Robert H. Badgley

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Sensors

DTIC Thesaurus Topics

  • Acoustic Frequencies
  • Aircrafts
  • Amplitude
  • Bearings
  • Frequency
  • Gear Noise
  • Gears
  • Helicopters
  • New York
  • Noise
  • Noise Reduction
  • Resonant Frequency
  • Short Takeoff Aircraft
  • Spiral Bevel Gears
  • Structural Components
  • Thrust Bearings
  • Vibration

Readers

  • Acoustics.
  • Aerospace Engineering
  • Systems Analysis and Design