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:
Sep. 01, 2015

Filed:

Aug. 02, 2010
Applicants:

Greg T. Kendall, Glendale, CA (US);

Derek L. Lisoski, Simi Valley, CA (US);

Walter R. Morgan, Simi Valley, CA (US);

John A. Griecci, Redondo Beach, CA (US);

Inventors:

Greg T. Kendall, Glendale, CA (US);

Derek L. Lisoski, Simi Valley, CA (US);

Walter R. Morgan, Simi Valley, CA (US);

John A. Griecci, Redondo Beach, CA (US);

Assignee:

AeroVironment Inc., Monrovia, CA (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 3/38 (2006.01); B64C 17/00 (2006.01); B64C 3/42 (2006.01); B64C 3/52 (2006.01); B64C 15/02 (2006.01); B64C 39/02 (2006.01); B64C 39/10 (2006.01); B64D 27/24 (2006.01); B64D 31/06 (2006.01); H04B 7/185 (2006.01);
U.S. Cl.
CPC ...
B64C 17/00 (2013.01); B64C 3/38 (2013.01); B64C 3/42 (2013.01); B64C 3/52 (2013.01); B64C 15/02 (2013.01); B64C 39/024 (2013.01); B64C 39/10 (2013.01); B64D 27/24 (2013.01); B64D 31/06 (2013.01); H04B 7/18504 (2013.01); B64C 2201/028 (2013.01); B64C 2201/042 (2013.01); B64C 2201/102 (2013.01); B64C 2201/122 (2013.01); B64C 2201/126 (2013.01); B64C 2201/127 (2013.01); B64C 2201/146 (2013.01); B64C 2201/165 (2013.01); B64D 2211/00 (2013.01); Y02T 50/12 (2013.01); Y02T 50/145 (2013.01); Y02T 50/44 (2013.01); Y02T 50/69 (2013.01);
Abstract

A span-loaded, highly flexible flying wing, having horizontal control surfaces mounted aft of the wing on extended beams to form local pitch-control devices. Each of five spanwise wing segments of the wing has one or more motors and photovoltaic arrays, and produces its own lift independent of the other wing segments, to minimize inter-segment loads. Wing dihedral is controlled by separately controlling the local pitch-control devices consisting of a control surface on a boom, such that inboard and outboard wing segment pitch changes relative to each other, and thus relative inboard and outboard lift is varied.


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