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:
Oct. 10, 2017

Filed:

May. 27, 2016
Applicant:

X Development Llc, Mountain View, CA (US);

Inventors:

Damon Vander Lind, Alameda, CA (US);

Thomas Van Alsenoy, Oakland, CA (US);

Richard Wayne DeVaul, Mountain View, CA (US);

Assignee:

X Development LLC, Mountain View, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F03D 9/00 (2016.01); H02P 9/04 (2006.01); B63H 9/06 (2006.01); C07C 29/141 (2006.01); B64C 31/06 (2006.01); F03D 5/00 (2006.01); B64C 27/00 (2006.01); B64C 39/02 (2006.01); B64D 3/00 (2006.01); B64D 47/00 (2006.01); B64F 3/02 (2006.01); H02K 7/18 (2006.01);
U.S. Cl.
CPC ...
F03D 9/002 (2013.01); B63H 9/0685 (2013.01); B64C 27/00 (2013.01); B64C 31/06 (2013.01); B64C 39/022 (2013.01); B64D 3/00 (2013.01); B64D 47/00 (2013.01); B64F 3/02 (2013.01); C07C 29/141 (2013.01); F03D 5/00 (2013.01); H02K 7/1838 (2013.01); B63H 2009/0692 (2013.01); B64C 2201/021 (2013.01); B64C 2201/024 (2013.01); B64C 2201/028 (2013.01); B64C 2201/145 (2013.01); B64C 2201/205 (2013.01); B64C 2201/206 (2013.01); B64C 2201/208 (2013.01); F05B 2240/917 (2013.01); F05B 2240/921 (2013.01); Y02E 10/70 (2013.01); Y02E 10/725 (2013.01); Y02E 10/728 (2013.01);
Abstract

A vehicle-based airborne wind turbine system having an aerial wing, a plurality of rotors each having a plurality of rotatable blades positioned on the aerial wing, an electrically conductive tether secured to the aerial wing and secured to a ground station positioned on a vehicle, wherein the aerial wing is adapted to receive electrical power from the vehicle that is delivered to the aerial wing through the electrically conductive tether; wherein the aerial wing is adapted to operate in a flying mode to harness wind energy to provide a first pulling force through the tether to pull the vehicle; and wherein the aerial wing is also adapted to operate in a powered flying mode wherein the rotors may be powered so that the turbine blades serve as thrust-generating propellers to provide a second pulling force through the tether to pull the vehicle.


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