Control system for rotor aircraft

Details Control system for rotor aircraft Control system for rotor aircraft

B - Operations, Transporting

64

C

B64C 27/52 (2006.01) B64C 13/28 (2006.01) B64C 27/02 (2006.01)

Patent

CA 2314655

A rotor aircraft has an adjusting mechanism that controls the sensitivity of the control stick relative to fore and aft tilt of the rotor. The control stick is pivotable between fore and aft directions as well as laterally about a control stick pivot point. A rotor linkage is connected between the control stick and the rotor rotor head. The rotor linkage assembly tilts the rotor head in response to tilting movement of the control stick. The linkage assembly has a control point that rotates at a radius about the control stick pivot point. An adjusting member located between the control stick and the linkage assembly can be moved to change the radius of the control point to the control stick pivot point. The change in radius corresponds to the amount of tilt that the rotor head make while the control stick moves between full aft and full forward positions. The control stick also controls ailerons and a horizontal stabilizer but these control services are not affected by the adjusting member.

Affiliated with

Also associated with

Rating

Control system for rotor aircraft does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Control system for rotor aircraft, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Control system for rotor aircraft will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-2033344