| |
 |
|
Class Information
Number: 416/106
Name: Fluid reaction surfaces (i.e., impellers) > Sustained ancillary movement of rotary working member (e.g., cyclic feathering, etc.) > Lead-lag type rotor blade movement > With movement restraining means (i.e., damping)
Description: Apparatus provided with means to limit the extent or reduce the frequency of blade movement about the lead-lag axis.
Sub-classes under this class:
Patents under this class:
| Patent Number |
Title Of Patent |
Date Issued |
| 7607892 |
Rotorcraft rotor with blades hinged in flap and in lag |
Oct. 27, 2009 |
| 6827553 |
Flexbeam damper assembly having transition shim clamp device |
Dec. 7, 2004 |
| 6676074 |
Dual piston drag damper for rotary-wing aircraft rotor |
Jan. 13, 2004 |
| 6398496 |
Minimizing wind forces on helicopter blades |
Jun. 4, 2002 |
| 6050778 |
Semi-articulated rotor system |
Apr. 18, 2000 |
| 6045328 |
Fluid damper including flexible damping plate |
Apr. 4, 2000 |
| 5636970 |
Device for damping the drag of the blades of a rotor |
Jun. 10, 1997 |
| 5628620 |
Main rotor system for helicopters |
May. 13, 1997 |
| 5407325 |
Rotor head for rotary wing aircraft |
Apr. 18, 1995 |
| 5372478 |
Helicopter rotor damper |
Dec. 13, 1994 |
| 5267833 |
Gyrocraft rotor hub body |
Dec. 7, 1993 |
| 5266005 |
Rotor head for rotary wing aircraft |
Nov. 30, 1993 |
| 5219430 |
Hydraulic damper and elastic-return strut comprising such a damper |
Jun. 15, 1993 |
| 5116209 |
Device of retractable stops for rotor blades of giroplanes, and rotor head including such a device |
May. 26, 1992 |
| 5116201 |
Adjustment means for helicopter rotor blade viscous damper |
May. 26, 1992 |
| 4808075 |
Helicopter rotor |
Feb. 28, 1989 |
| 4695226 |
Helicopter rotor backup damper system |
Sep. 22, 1987 |
| 4551067 |
Helicopter rotor |
Nov. 5, 1985 |
| 4241814 |
Mechanical-hydraulic damper for a load subject to shocks and vibrations |
Dec. 30, 1980 |
| 4084668 |
Redundant damper seals |
Apr. 18, 1978 |
|
|
|
