Advanced Flight Control Actuation System (AFCAS-E/P). Feasibility Investigation of an Electro/Pneumatic Dual Power Driven Concept.

Abstract

This is a report of design study on Dual-Mode Dynavector Actuator for use as control-surface actuator on aircraft. Actuator operates on pneumatic power and /or electric power. Operation within specifications continues despite loss of either electric or pneumatic power, providing survivability feature for aircraft. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1978
Accession Number
ADA063992

Entities

People

  • Philip Forman
  • Rex W. Presley
  • Richard Krehely
  • Robert E. Feucht

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Actuators
  • Air Gaps
  • Brushless Dc Motors
  • Computer Programs
  • Control Systems
  • Dynamic Response
  • Eddy Currents
  • Electric Motors
  • Failure Mode And Effect Analysis
  • Flux Density
  • Frequency Response
  • Materials
  • Modulus Of Elasticity
  • Pneumatic Actuators
  • Reliability
  • Roller Bearings
  • Test Methods

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Robotics and Automation.