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Control of Helicopter Rotorblade Aerodynamics

Control of Helicopter Rotorblade Aerodynamics

          
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About the Book

The results of a feasibility study of a method for controlling the aerodynamics of helicopter rotorblades using stacks of piezoelectric ceramic plates are presented. A resonant mechanism is proposed for the amplification of the displacements produced by the stack. This motion is then converted into linear displacement for the actuation of the servoflap of the blades. A design which emulates the actuation of the servoflap on the Kaman SH-2F is used to demonstrate the fact that such a system can be designed to produce the necessary forces and velocities needed to control the aerodynamics of the rotorblades of such a helicopter. Estimates of the electrical power requirements are also presented. A Small Business Innovation Research (SBIR) Phase 2 Program is suggested, whereby a bench-top prototype of the device can be built and tested. A collaborative effort between AEDAR Corporation and Kaman Aerospace Corporation is anticipated for future effort on this project. Fabunmi, James A. Unspecified Center...


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Product Details
  • ISBN-13: 9781730746826
  • Publisher: Independently Published
  • Publisher Imprint: Independently Published
  • Height: 279 mm
  • No of Pages: 62
  • Spine Width: 3 mm
  • Width: 216 mm
  • ISBN-10: 1730746829
  • Publisher Date: 02 Nov 2018
  • Binding: Paperback
  • Language: English
  • Returnable: N
  • Weight: 168 gr


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