Oscillating flap lift enhancement device
First Claim
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1. An apparatus for increasing the lift of an aircraft comprising:
- a) a wing having a leading edge and a trailing edge, the wing capable of providing lift;
b) a flap having a leading edge and a trailing edge, the leading edge of the flap pivotally attached to said trailing edge of said wing;
c) means for oscillating said flap;
wherein said wing, said flap and said oscillating means communicate to maintain said flap in a predetermined stationary position at angles of attack less than 10 degrees and cause said flap to oscillate at angles of attack equal to or greater than 10 degrees.
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Abstract
A lift enhancing device for a solid wing is disclosed wherein a where a mr driven, flap dynamically oscillating flap mechanism produces an increase in the lifting capabilities of the wing.
114 Citations
8 Claims
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1. An apparatus for increasing the lift of an aircraft comprising:
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a) a wing having a leading edge and a trailing edge, the wing capable of providing lift; b) a flap having a leading edge and a trailing edge, the leading edge of the flap pivotally attached to said trailing edge of said wing; c) means for oscillating said flap;
wherein said wing, said flap and said oscillating means communicate to maintain said flap in a predetermined stationary position at angles of attack less than 10 degrees and cause said flap to oscillate at angles of attack equal to or greater than 10 degrees. - View Dependent Claims (2, 3, 4)
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5. A method for increasing the lift of an airfoil, the airfoil having a fixed forwardly portion for providing lift and a rearwardly portion for oscillating, the rearwardly portion pivotally attached to the forwardly portion, and also having means for oscillating said rearwardly portion, the method comprising the steps of:
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a) maintaining said rearwardly portion in a fixed relationship with respect to said forwardly portion at angles of attack less than 10 degrees; b) oscillating said rearwardly portion with respect to said forwardly portion at angles of attack equal to or greater than 10 degrees. - View Dependent Claims (6, 7, 8)
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Specification