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:
Jan. 10, 2017

Filed:

Oct. 06, 2014
Applicant:

Aurora Flight Sciences Corporation, Manassas, VA (US);

Inventors:

James Donald Paduano, Boston, MA (US);

Paul Nils Dahlstrand, Newton, MA (US);

John Brooke Wissler, Waltham, MA (US);

Adam Woodworth, Melrose, MA (US);

Assignee:
Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/52 (2006.01); B64C 29/04 (2006.01); B64C 29/02 (2006.01); B64C 39/02 (2006.01); B64C 29/00 (2006.01); B64C 3/42 (2006.01); B64C 5/02 (2006.01); B64C 9/00 (2006.01); B64C 25/10 (2006.01); B64D 27/02 (2006.01); B64D 43/00 (2006.01);
U.S. Cl.
CPC ...
B64C 27/52 (2013.01); B64C 3/42 (2013.01); B64C 5/02 (2013.01); B64C 9/00 (2013.01); B64C 25/10 (2013.01); B64C 29/00 (2013.01); B64C 29/0033 (2013.01); B64C 29/0091 (2013.01); B64C 29/02 (2013.01); B64C 29/04 (2013.01); B64C 39/024 (2013.01); B64D 27/02 (2013.01); B64D 43/00 (2013.01); B64C 2201/021 (2013.01); B64C 2201/088 (2013.01); B64C 2201/102 (2013.01); B64C 2201/108 (2013.01); B64C 2201/162 (2013.01); B64C 2201/187 (2013.01);
Abstract

A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends.


Find Patent Forward Citations

Loading…