Low-height tunable tilt rotor downstop

Details Low-height tunable tilt rotor downstop Low-height tunable tilt rotor downstop

B - Operations, Transporting

64

C

B64C 27/28 (2006.01) B64C 27/32 (2006.01) B64C 29/00 (2006.01)

Patent

CA 2314835

A improved tilt rotor aircraft comprising an airframe, at least one wing member coupled to the airframe, and at least one tilt rotor assembly carried by the at least one wing member. The improved tilt rotor aircraft includes a low-height tunable downstop assembly for isolating static and dynamic lateral loads between the tilt rotor assemblies and the wings. The low-height tunable downstop assembly comprises a pivotable striker assembly having an adjustable stiffness, and a cradle assembly adapted to releasably receive the striker assembly. The low-height tunable downstop assembly isolates yaw loads while providing a stiff vertical support.

Affiliated with

Also associated with

Rating

Low-height tunable tilt rotor downstop does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Low-height tunable tilt rotor downstop, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Low-height tunable tilt rotor downstop will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1702831