The patent application relates to a flight control device, adapted for use with an airborne vehicle having variable sweep wings, to control a spoiler on the trailing edge of the upper surface of each wing. One of the unique and fundamental features of the inventive device is that certain constituent members of the drive mechanism maintain a novel parallelogrammic positional relationship. The inventive device not only permits control of the spoiler irrespective of the sweep position of the wing, but also permits the maintenance of the selected position of the spoiler irrespective of any subsequent change in the sweep of the wing.
Flight Control Device
1974
19 pages
Report
Keine Angabe
Englisch
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