Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1988-06-24
1990-06-12
Peters, Jr., Joseph F.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
74 8916, 475334, 475342, 475344, B64C 902
Patent
active
049326139
ABSTRACT:
A rotary hinge actuator, for instance for rotating a wing flap relative to a wing in an aircraft, has a sun gear, several spindle gears around the sun gear and several annular gear sleeves around the sun gear and spindle gears. Each spindle gear has sections with external helical gear teeth which are slanted in the same direction and which respectively mesh with internal helical gear teeth on the annular gear sleeves. At least one of the sleeves is connected to the wing and at least another to the wing flap. Upon rotating the spindle gears the wing flap is rotated relative to the wing.
REFERENCES:
patent: 2982144 (1961-05-01), Wallgren
patent: 3008355 (1961-11-01), Grudin
patent: 3333482 (1967-08-01), Wildhaber
patent: 3486394 (1969-12-01), Heidrich
patent: 3640150 (1972-02-01), Leiner et al.
patent: 4721016 (1988-01-01), Burandt
patent: 4742730 (1988-05-01), Dorn et al.
patent: 4751855 (1988-06-01), Hudson et al.
Leuze William C.
Seipel Arnold G.
Tiedeman Robert K.
Curtiss-Wright Flight Systems, Inc.
Peters Jr. Joseph F.
Sartelle Anne
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