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Vertical-plane pendulum absorbers for minimizing helicopter vibratory loadsThe use of pendulum dynamic absorbers mounted on the blade root and operating in the vertical plane to minimize helicopter vibratory loads was discussed. A qualitative description was given of the concept of the dynamic absorbers and some results of analytical studies showing the degree of reduction in vibratory loads attainable are presented. Operational experience of vertical plane dynamic absorbers on the OH-6A helicopter is also discussed.
Document ID
19740026397
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Amer, K. B.
(Hughes Helicopters Culver City, CA, United States)
Neff, J. R.
(Hughes Helicopters Culver City, CA, United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1974
Publication Information
Publication: NASA. Ames Res. Center Rotorcraft Dyn.
Subject Category
Aircraft
Accession Number
74N34510
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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