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. 18, 2016

Filed:

Apr. 26, 2013
Applicant:

The Boeing Company, Chicago, IL (US);

Inventor:

Jian Dong, Irvine, CA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/56 (2006.01); B64C 3/38 (2006.01); B64C 3/54 (2006.01); B64C 23/06 (2006.01); B64C 9/34 (2006.01);
U.S. Cl.
CPC ...
B64C 3/56 (2013.01); B64C 3/385 (2013.01); B64C 3/54 (2013.01); B64C 3/546 (2013.01); B64C 23/065 (2013.01); B64C 9/34 (2013.01);
Abstract

An adaptive wing for an aircraft includes a first wing portion, a second wing portion, and a third wing portion. The second wing portion is telescopically attached to the first wing portion to selectively change an overall length of the wing based on real-time flight conditions or airport space constraints. The third wing portion is rotate-ably attached to one end of the second wing portion, and a dihedral angle between the second wing portion and the third wing portion is changeable based on real-time flight conditions or airport space constraints.


Find Patent Forward Citations

Dong, Jian. (2016). Adaptive wing for an aircraft (U.S. Patent No. 9469391). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9469391

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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