Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1982-09-30
1984-09-04
Barefoot, Galen L.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
B64C 924
Patent
active
044692978
ABSTRACT:
An actuation and extension mechanism for aerodynamic high-lift devices such as a wing leading edge slat or a wing trailing edge flap; wherein an aerodynamic panel is connected to one end of an extendible track member that is supported and guided by its other end through rollers fixedly mounted to wing rib structure. The track member incorporates a cable and drum arrangement as part of the extension or retraction mechanism; and this combination of track, cable and drum provides the primary support and drive means for the high-lift device without compromising the structural strength or the stress safety of said combination.
REFERENCES:
patent: 1917428 (1933-07-01), Burnelli
patent: 2235146 (1941-03-01), Fowler
patent: 2298264 (1942-10-01), Czurles et al.
patent: 2702676 (1955-02-01), Delaney, Jr.
patent: 2938680 (1960-05-01), Greene et al.
patent: 3087343 (1963-04-01), Wubbe
patent: 3089666 (1963-05-01), Quenzler
patent: 4286649 (1981-09-01), Rokop et al.
Barefoot Galen L.
Donahue B. A.
Hartmann H. Gus
The Boeing Company
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