Electrical flight control system for an airplane, with attitude

Details Electrical flight control system for an airplane, with attitude Electrical flight control system for an airplane, with attitude

1994-09-29

1996-06-18

Barefoot, Galen L.

Aeronautics and astronautics

Aircraft control

Automatic

244195, B64C 1316

Patent

active

055270026

ABSTRACT:
According to the invention, attenuator means (8) are provided, making it possible to limit the rate of rotation of the airplane on takeoff, so as to avoid the tail of the airplane striking the ground and to reduce the dispersion of the rotation rates.

REFERENCES:
patent: 3216676 (1969-11-01), Brown et al.
patent: 3594553 (1971-07-01), McElroy
patent: 3945590 (1976-03-01), Kenney, Jr. et al.
patent: 3963197 (1976-06-01), Oberlerchner
patent: 4763266 (1988-08-01), Schultz et al.

Affiliated with

Also associated with

Rating

Electrical flight control system for an airplane, with attitude does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Electrical flight control system for an airplane, with attitude , we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Electrical flight control system for an airplane, with attitude will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-217681