Torque linkage damper

Details Torque linkage damper Torque linkage damper

B - Operations, Transporting

64

C

B64C 25/58 (2006.01) B64C 25/50 (2006.01) F16F 9/19 (2006.01)

Patent

CA 2084838

An aircraft landing gear damping mechanism improvement of a damper containing piston means in a chamber of a housing, an orifice in the piston means and Belleville springs disposed in the chamber between the wall of the chamber and the piston means on opposite sides thereof. The improvement comprises means (e.g., in the form of a member having slots therein) and disposed between one end of the Belleville springs and the adjacent chamber wall, providing fluid communication of the inner cavity and outer cavity of the chamber below and above the Belleville springs.

Affiliated with

Also associated with

Rating

Torque linkage damper does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Torque linkage damper, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Torque linkage damper will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1461338