Results 191 to 200 of about 15,084 (235)
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Vibratory Ice Protection for Helicopter Rotor Blades.
1978Abstract : This report presents the results of a study on vibrational deicing of main and tail rotor blades through higher harmonic shaking of the blades with aerodynamic, mechanical, and hydraulic shakers. Studies were made of various locations for mounting shakers, the forces and frequencies to deice, types of shakers, concept effectiveness, energy ...
H. Upton, H. E. Lemont
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Active rotor control for helicopters: individual blade control and swashplateless rotor designs
CEAS Aeronautical Journal, 2011Modern helicopters still suffer from many problems that hinder a further increase in their efficiency, acceptance and hence their market share. The high level of vibrations and the noise generated by the rotor are the most important reasons for this. Vibrations are problematic not only for pilot and passenger comfort, but also give rise to an increase ...
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Failure of a Helicopter Main Rotor Blade
1992Abstract A Marine Corps helicopter crash was investigated. Efforts were directed to the failure of one of the main rotor blades that had apparently separated in the air. The apparent failure of a blade integrity monitor (BIM) system was also considered.
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Design and Production of Fiberglass Helicopter Rotor Blades
1980The design of a helicopter rotor blade requires close attention to aerodynamic, dynamic, structural and mechanical considerations, and manufacturing methodology.
C. E. Covington, P. S. Baumgardner
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Mechanical Stability of a Two-Bladed Cantilever Helicopter Rotor
Journal of the Aeronautical Sciences, 1956SUMMARY A theoretical analysis of the mechanical stability of a twobladed cantilever helicopter rotor, whose hub is mounted upon isotropic elastic supports in the horizontal plane and whose elastic blades employ fixed root attachments, has been made and is reported here.
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Solutions for Helicopter Rotor Blade Icing
Journal of the American Helicopter Society, 1958D. A. Richardson +2 more
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The Single-Rotor Helicopter with Rigidly-Mounted Blades
The Journal of the Royal Aeronautical Society, 1963For many years, studies of various light aircraft designs have been carried on by the Lockheed-California Company in search of a vehicle that had the potential of truly generating the “air age”—a vehicle which would perform a useful service to many people, in many jobs.
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The Heavy Lift Helicopter Rotor Blade
Journal of the American Helicopter Society, 1974T. Scarpati, R. Sandford, R. Powell
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Stabilizing helicopter rotor blades using delayed feedback
2021J.M. Krodkiewski, J.S. Faragher
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