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:
Feb. 18, 2020

Filed:

Mar. 22, 2018
Applicants:

Robert N. Dunn, Austin, TX (US);

Lawrence R. Dunn, Austin, TX (US);

Inventors:

Robert N. Dunn, Austin, TX (US);

Lawrence R. Dunn, Austin, TX (US);

Assignee:

Other;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 39/08 (2006.01); B64C 3/38 (2006.01); B64C 3/54 (2006.01); B64C 39/10 (2006.01); B64C 3/28 (2006.01);
U.S. Cl.
CPC ...
B64C 39/08 (2013.01); B64C 3/385 (2013.01); B64C 3/54 (2013.01); B64C 3/28 (2013.01); B64C 2039/105 (2013.01);
Abstract

A tandem wing aircraft having a fore wing, an aft wing, and a middle wing, attached relative to the aircraft and each other such that the middle wing provides a substantial portion of the total lift at landing speeds, and a minimal portion of the total lift at cruise speeds. At cruise speeds, induced drag is minimized, permitting higher speeds, greater fuel efficiency, and/or greater payload. Advantageously, the wing loading at cruise speeds is higher providing better passenger comfort while still providing controllability and safety at landing speeds.


Find Patent Forward Citations

Dunn, Robert. (2020). Tandem wing aircraft with variable lift and enhanced safety (U.S. Patent No. 10562626). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10562626

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

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