Improved Linear Actuator, OH-58A Helicopter.

Abstract

This report presents the results of Product Improvement Program, Task No 72-10, wherein the engine N11 linear actuator, P/N 206-062-721-1, as installed on the OH58A helicopter, was modified for the purpose of providing better field reliability. One prototype unit was built and briefly flight tested on an OH58 helicopter. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Sep 16, 1974
Accession Number
ADA036488

Entities

People

  • C. V. Harvey

Organizations

  • Bell Flight

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Actuators
  • Army Aviation
  • Assembly
  • Case Hardening
  • Control Systems
  • Data Rights
  • Engineers
  • Flight Testing
  • Helicopters
  • High Temperature
  • Manufacturing
  • Models
  • Prototypes
  • Reliability
  • Speed Regulators
  • Test And Evaluation
  • Test Facilities

Fields of Study

  • Physics

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Aviation Science / Aeronautics.
  • Internal Combustion Engine (ICE) Technology.