Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1993-11-02
1996-07-23
Barefoot, Galen L.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
244225, 244 75R, 244 78, 244 90R, B64C 1336
Patent
active
055382029
ABSTRACT:
A hydraulic actuation system for an aircraft control surface such as an elevon. A pair of spaced pivot points are provided to alternately rotate the control surface either clockwise or counterclockwise.
REFERENCES:
patent: 1935004 (1933-11-01), Winther, Jr.
patent: 2404045 (1946-07-01), Flader
patent: 2643833 (1953-06-01), Ambroise
patent: 2861758 (1958-11-01), Howard
patent: 2863321 (1958-12-01), Weiland
patent: 2899152 (1959-08-01), Weiland
patent: 2972898 (1961-02-01), Hartel
patent: 3051137 (1962-08-01), Kutzler
patent: 3911847 (1975-10-01), Worthing
patent: 4034334 (1977-07-01), Allyn
patent: 4395007 (1983-07-01), Owl, Jr.
patent: 4412666 (1983-11-01), Grob
patent: 4544118 (1985-10-01), Robinson
patent: 4773620 (1988-09-01), Seidel
patent: 4793137 (1988-12-01), Munk
Anderson Terry J.
Barefoot Galen L.
Hoch Jr. Karl J.
Northrop Grumman Corporation
LandOfFree
Hydraulic actuation system for aircraft control surfaces does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Hydraulic actuation system for aircraft control surfaces, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Hydraulic actuation system for aircraft control surfaces will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-707959