• DocumentCode
    1370251
  • Title

    Weight analysis of aircraft actuators

  • Author

    Geyer, M. Howard ; Treseder, R. C.

  • Author_Institution
    General Motors Corporation, Dayton, Ohio
  • Volume
    71
  • Issue
    2
  • fYear
    1952
  • fDate
    4/1/1952 12:00:00 AM
  • Firstpage
    118
  • Lastpage
    126
  • Abstract
    THE work that must be expended to actuate adjustable flight surfaces and to operate the landing gear, bomb doors, and other movable structures on aircraft often exceeds pilot capabilities. At the same time, the increase in physical size of aircraft in recent years has all but ruled out mechanical transmission systems. To provide for power amplification and to eliminate mechanical links, the aircraft designer uses a multitude of remotely controlled actuating devices, known more simply to the aircraft industry as actuators.
  • Keywords
    Actuators; Aircraft; Batteries; Compressors; Fasteners; Fluids; Generators;
  • fLanguage
    English
  • Journal_Title
    American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
  • Publisher
    ieee
  • ISSN
    0097-2185
  • Type

    jour

  • DOI
    10.1109/TAI.1952.6371255
  • Filename
    6371255