The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Dec. 23, 2014

Filed:

Dec. 30, 2010
Applicant:

Carsten Hein Westergaard, Houston, TX (US);

Inventor:

Carsten Hein Westergaard, Houston, TX (US);

Assignee:

Vestas Wind Systems A/S, Aarhus N, DK;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/00 (2006.01); G01S 17/58 (2006.01); F03D 11/00 (2006.01); G01S 7/481 (2006.01); G01P 13/00 (2006.01); G01S 17/88 (2006.01); G01P 5/26 (2006.01); G01S 17/10 (2006.01); G01P 13/02 (2006.01);
U.S. Cl.
CPC ...
G01P 13/00 (2013.01); G01S 17/58 (2013.01); F03D 11/0091 (2013.01); G01S 7/4814 (2013.01); F05B 2270/328 (2013.01); G01S 17/88 (2013.01); G01P 5/26 (2013.01); G01S 17/107 (2013.01); Y02E 10/722 (2013.01); G01P 13/025 (2013.01); F05B 2270/804 (2013.01);
Abstract

Methods and apparatus for optically detecting an angle of attack for an airfoil using light detection and ranging (LIDAR). To determine the angle of attack, one or more light beam pulses may be emitted from the leading edge of the airfoil into an (apparently) flowing fluid at various emission angles. The emitted pulses may be backscattered by particles in the fluid, and the backscattered light may be received by a detector at the airfoil. By range gating the returning pulses of backscattered light, a fluid velocity may be determined for each of the emission angles. The angle of attack is identified as the emission angle corresponding to the maximum velocity. A parameter (e.g., pitch or speed) of the airfoil may be controlled based on the angle of attack. In this manner, the airfoil may be manipulated or the shape of the airfoil may be adjusted for increased performance or efficiency.


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