Wing sweep control system

Aeronautics and astronautics – Aircraft control – Automatic

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

244 42A, 244 77M, 244 77SE, B64C 1318

Patent

active

039400948

ABSTRACT:
A system for controlling the wing sweep angle of the wings of an aircraft over their entire sweep range, including a detector for determining aircraft speed and altitude, a digital computer for receiving signals from the detector to produce output signals in response to the input signals therefrom, control apparatus responsive to signals from the computer, an actuator for moving the wings of the aircraft in response to the control apparatus, and a cross-shaft for synchronizing the movement of the wings. A manual controller is also included for manual control of the actuator.

REFERENCES:
patent: 2428934 (1947-10-01), Gille et al.
patent: 2448167 (1948-08-01), Baak
patent: 2736515 (1956-02-01), Dolan et al.
patent: 2924400 (1960-02-01), Ruget
patent: 2936134 (1960-05-01), Miller et al.
patent: 3027878 (1962-04-01), Keyt et al.
patent: 3044002 (1962-07-01), Lejohn
patent: 3064928 (1962-11-01), Toll
patent: 3171615 (1965-03-01), Patterson
patent: 3252675 (1966-05-01), Close et al.
patent: 3447761 (1969-06-01), Whitener et al.
patent: 3501114 (1970-03-01), DePlante
patent: 3522729 (1970-08-01), Miller

LandOfFree

Say what you really think

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

Rating

Wing sweep control system does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

     

Profile ID: LFUS-PAI-O-2077052

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