Helicopter Rotor Isolation Evaluation Utilizing the Dynamic Antiresonant Vibration Isolator

760894

02/01/1976

Event
Aerospace Engineering and Manufacturing Meeting
Authors Abstract
Content
Helicopters characterististically exhibit large amplitude vibration at low frequencies caused by the main rotor induced shears and moments. One means of reducing this vibration level is by rotor isolation. That is, the isolation of the fuselage from rotor induced shears and moments. Under sponsorship of Eustis Directorate, USAAMRDL, Kaman Aerospace has conducted rotor isolation programs utilizing the Dynamic Antiresonant Vibration Isolator (DAVI). A summary of the analytical, full scale shake test and flight test rotor isolation programs are discussed.
Meta TagsDetails
DOI
https://doi.org/10.4271/760894
Pages
20
Citation
Jones, R., and McGarvey, J., "Helicopter Rotor Isolation Evaluation Utilizing the Dynamic Antiresonant Vibration Isolator," SAE Technical Paper 760894, 1976, https://doi.org/10.4271/760894.
Additional Details
Publisher
Published
Feb 1, 1976
Product Code
760894
Content Type
Technical Paper
Language
English