Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1995-01-09
1996-11-05
Barefoot, Galen L.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
244113, 244215, 416 23, 416 14, B64C 2772
Patent
active
055708595
ABSTRACT:
A spoiler flap is pivotably mounted to the rearward portion of a wind turbine blade or wing to control or influence air flow over the surface of the blade or wing. The spoiler flap has forward and rearward edges. The spoiler flap can be pivoted to simultaneously raise the forward edge (into low pressure flow) and lower the rearward edge of the spoiler flap (into high pressure flow). The extent to which the spoiler flap is pivoted determines the extent to which the air flow over the surface of the blade or wing is influenced. When the spoiler flap is fully deployed or pivoted, it serves as a braking device. When it is only partially pivoted, it serves the function of power modulation.
REFERENCES:
patent: 1293228 (1919-02-01), Sopwith
patent: 1389757 (1921-09-01), Haynes
patent: 1423131 (1922-07-01), McNamara
patent: 2138326 (1938-11-01), Pouit
patent: 4015787 (1977-04-01), Maieli et al.
patent: 4297076 (1981-10-01), Danham et al.
Barefoot Galen L.
Edmundson Dean P.
LandOfFree
Aerodynamic braking device does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Aerodynamic braking device, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aerodynamic braking device will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-2008952