Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1989-07-31
1992-11-10
Steinberger, Brian S.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
244213, B64C 916
Patent
active
051617579
ABSTRACT:
Novel means for deploying airplane wing flaps feature a bent shaft which is translatable fore and aft in the fairing cavity. The shaft has an adjacent follower member which travels in a concentric curved flap track to rotate shaft as it extends. The bent shaft has a support ball fitting and end roller which provide flap deflection with respect to the fixed wing as the shaft is extended aft and rotated. The subject flap deployment means are mechanically elegant resulting in lower manufacturing and installation cost and high reliability.
REFERENCES:
patent: 2670909 (1954-03-01), Replogle
patent: 3126173 (1964-03-01), Alvarez-Calderon
patent: 3721406 (1973-03-01), Hurbert
Donahue B. A.
Harasek Elizabeth F.
Steinberger Brian S.
The Boeing Company
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