Flight control system for an aircraft

B - Operations – Transporting – 64 – C

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

B64C 9/00 (2006.01) B64C 13/40 (2006.01)

Patent

CA 2727592

The invention relates to a flight control system for an aircraft comprising control surfaces (111, 211, 331, 431, 541, 121-225), and actuators associated with said control surfaces to control flight functions of roll, yaw, pitching and aerodynamic braking of the aircraft. All of the actuators (111a1- 211a2, 121a-225a) associated with the control surfaces controlling at least one of said flight functions are electromechanical actuators. A part of said control surfaces associated with the electromechanical actuators are divided control surfaces (111, 211, 331, 431, 541), each of said divided control surfaces being composed of at least two independent surfaces (113, 114,..., 545)

LandOfFree

Say what you really think

Search LandOfFree.com for Canadian inventors and patents. Rate them and share your experience with other people.

Rating

Flight control system for an 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 Flight control system for an aircraft, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Flight control system for an aircraft will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFCA-PAI-O-1364655

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.