Active control of multi-element rotor blade airfoils

Fluid reaction surfaces (i.e. – impellers) – Method of operation

Reexamination Certificate

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C416S024000, C416S155000, C416S23100A

Reexamination Certificate

active

06932569

ABSTRACT:
A multi-element rotor blade includes an individually controllable main element and fixed aerodynamic surface in an aerodynamically efficient location relative to the main element. The main element is controlled to locate the fixed aerodynamic surface in a position to increase lift and/or reduce drag upon the main element at various azimuthal positions during rotation.

REFERENCES:
patent: 2095734 (1937-10-01), Dornier
patent: 2624531 (1953-01-01), Stalker
patent: 2642143 (1953-06-01), Miller
patent: 2716460 (1955-08-01), Young
patent: 4655685 (1987-04-01), Fradenburgh
patent: 5482383 (1996-01-01), Gantt et al.
patent: 5681032 (1997-10-01), Hofmann
patent: 5741116 (1998-04-01), Hudson
patent: 5860382 (1999-01-01), Hobdy
patent: 5905212 (1999-05-01), Moses et al.
patent: 5915842 (1999-06-01), Redinger
patent: 5957662 (1999-09-01), Aoki et al.
patent: 5961290 (1999-10-01), Aoki et al.
patent: 6135713 (2000-10-01), Domzalski et al.
patent: 6168144 (2001-01-01), Bruehl
patent: 6168379 (2001-01-01), Bauer
patent: 6190132 (2001-02-01), Yamakawa et al.
patent: 6200096 (2001-03-01), Kohlhepp
patent: 6224047 (2001-05-01), Gwinn
patent: 6231013 (2001-05-01), Jaenker
patent: 6231308 (2001-05-01), Kondo et al.
Narramore, J.C., McCroskey, W.J. & Noonan, K.W., Design and Evaluation of Multi-Element Airfoils for Rotorcraft, Presented at the American Helicopter Society 55th Annual Forum, May 25-27, 1999, Montreal, Quebec, Canada, American Helicopter Society, Inc., 1999.
Chaffin, SR., Mark S., Application of Adjoint Optimization Method to Multi-Element Rotorcraft Airfoils, Presented at the American Helicopter Society Vertical Lift Aircraft Design Conference, San Francisco, CA, American Helicopter Society, Inc. 2000.
Noonan, Kevin W., Evaluation of Model Helicopter Main Rotor Blade With Slotted Airfoils at the Top, Presented at the American Helicopter Society 55th Annual Forum, May 25-27, 1999, Montreal, Quebec, Canada, American Helicopter Society, Inc., 1999.
Ham, Norman D., Helicopter Individual-Blade-Control and Its Applications, Presented at the 39th Annual Forum of the American Helicopter Society, May 9-11, 1983, St. Louis, MO, American Helicopter Society, Inc. 1983.
Kunze, Olivier, Arnold, Uwe T.P. & Waaske, Stefan, Development and Design of an Individual Blade Control System for the Sikorsky CH-52G Helicopter, Presented at the American Helicopter Society 55th Annual Forum, May 25-27, 1999, Montreal, Quebec, Canada, American Helicopter Society, Inc. 1999.
Bernhard, Andreas P.F. & Chopra, Inderjit, Development of a Smart Moving-Blade-Tip and an Active-Twist Rotor Blade Driven by a Piezo-Induced Bending-Torsion Coupled Beam, Presented at the American Helicopter Society 53rd Forum, Apr. 1997, Virginia Beach, VA, American Helicopter Society, Inc. 1997.
Schimke, D., Janker, P., Blaas, A., Kube, R., Schewe, G. & Kebler, CH., Individual Blade Control by Servo-Flap and Blade Root Control a Collaborative Research and Development Programme, Presented at the 23rd European Rotorcraft Forum in Dresden, Germany, Sep. 16-18, 1997.

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