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:
May. 09, 2023

Filed:

Dec. 17, 2019
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Keyvan Sayyah, Santa Monica, CA (US);

Pamela R. Patterson, Los Angeles, CA (US);

Raymond Sarkissian, Studio City, CA (US);

Oleg M. Efimov, Thousand Oaks, CA (US);

Biqin Huang, Torrance, CA (US);

David L. Hammon, Simi Valley, CA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/00 (2006.01); G01S 17/89 (2020.01); G05D 1/08 (2006.01); G01S 7/481 (2006.01); G01S 17/66 (2006.01); G01S 17/88 (2006.01); G01S 17/06 (2006.01);
U.S. Cl.
CPC ...
B64C 27/008 (2013.01); G01S 7/4817 (2013.01); G01S 17/06 (2013.01); G01S 17/66 (2013.01); G01S 17/88 (2013.01); G01S 17/89 (2013.01); G05D 1/0816 (2013.01);
Abstract

A blade positioning system and method are provided to dynamically measure blade position during flight of a rotorcraft. In the context of a method, a blade of the rotorcraft is repeatedly illuminated by a light source during flight of the rotorcraft while the blade is rotating. The method also includes detecting radiation scattered from the blade in response to illumination of the blade. The method further includes determining at least one of a blade pitch angle, a blade flap angle, a blade leading position or a blade lagging position based upon the radiation that is scattered from the blade and detected. A rotorcraft is also provided that includes a chip-scale light detection and ranging (LIDAR) sensor configured to illuminate the plurality of blades while the blades are rotating in order to permit blade position to be measured or to illuminate terrain beneath the rotorcraft in order to provide an altitude measurement.


Find Patent Forward Citations

Loading…