Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1986-06-23
1988-08-16
Peters, Jr., Joseph F.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
244213, B64C 906
Patent
active
047638621
ABSTRACT:
A flap is pivotally mounted on a roller that runs in a track; a three point control lever has one point connected to the roller, a second point to the front of the flap, and a third point is variably connected to a turning lever that drives the flap. The variation is obtained either by providing a secondary lever on the turning lever to obtain a cycloidal path, or a spindel drive just varies the distance between the third point of the control lever and the axis of the turning lever. The turning lever is hollow to accommodate the drive elements for the third point variation.
REFERENCES:
patent: 3987983 (1976-10-01), Cole
patent: 4312486 (1982-01-01), McKinney
patent: 4381093 (1983-04-01), Rudolph
patent: 4544118 (1985-10-01), Robinson
Martens Walter
Steinhauer Hans-Juergen
Corl Rodney
MBB GmbH
Peters Jr. Joseph F.
Siegemund Ralf H.
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