FIELD: aeronautical engineering. SUBSTANCE: device includes mechanical pendula located on either side of each blade at different distances from the flexural center. Pendula are made in form of levers of different length with weights at the ends of different mass; they are mounted on blade shank. EFFECT: enhanced efficiency of dampening vibrations due to independence of swinging axles of pendula which are mounted at different angles relative to chord of section. 4 dwg
Title | Year | Author | Number |
---|---|---|---|
DEVICE FOR DAMPENING VIBRATIONS OF HELICOPTER MAIN ROTOR BLADES | 1992 |
|
RU2077454C1 |
DEVICE FOR DAMPING VIBRATION IN BLADES OF HELICOPTER MAIN ROTOR | 1989 |
|
SU1792078A1 |
DEVICE FOR DAMPENING VIBRATIONS OF HELICOPTER MAIN ROTOR BLADES | 1994 |
|
RU2078008C1 |
METHOD FOR LOCATION OF HELICOPTER CENTER OF MASS | 2003 |
|
RU2241637C1 |
HELICOPTER MAIN ROTOR BLADE | 1999 |
|
RU2148532C1 |
METHOD OF BALANCING HELICOPTER ROTORS | 2001 |
|
RU2180735C1 |
HELICOPTER ROTOR AND PRODUCTION OF ROTOR FROM COMPOSITES | 2013 |
|
RU2541574C1 |
PROPELLER BLADE AND METHOD OF ITS FABRICATION | 2014 |
|
RU2561827C1 |
METHOD OF DETERMINATION OF INERTIA MOMENT OF ARTICLE | 1999 |
|
RU2164671C1 |
METHOD OF PROPELLER BLADES STATIC ALIGNMENT | 2007 |
|
RU2336508C1 |
Authors
Dates
1998-07-20—Published
1996-10-17—Filed