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:
Dec. 19, 2023

Filed:

Feb. 28, 2022
Applicant:

The Boeing Company, Chicago, IL (US);

Inventor:

Jeff S Siegmeth, Bothell, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 9/32 (2006.01); B64C 9/02 (2006.01); B64D 27/24 (2006.01); B64D 41/00 (2006.01); B64C 9/00 (2006.01); B60L 53/52 (2019.01); B60L 50/60 (2019.01); B60L 8/00 (2006.01);
U.S. Cl.
CPC ...
B60L 53/52 (2019.02); B60L 8/006 (2013.01); B60L 50/60 (2019.02); B64C 9/02 (2013.01); B64C 9/323 (2013.01); B64D 27/24 (2013.01); B64D 41/00 (2013.01); B64D 41/007 (2013.01); B60L 2200/10 (2013.01); B64C 2009/005 (2013.01); B64D 2221/00 (2013.01);
Abstract

Reactive spoilers for aircraft and associated methods. In one embodiment, a wing of an aircraft includes a leading edge, a trailing edge, and an upper surface and a lower surface between the leading edge and the trailing edge. The wing further includes a reactive spoiler disposed on the upper surface between the leading edge and the trailing edge. The reactive spoiler comprises one or more turbines configured to raise in relation to the upper surface into an airflow passing over the upper surface, and to reduce lift of a wing section behind the turbines. The turbines are configured to convert kinetic energy from the airflow into electrical energy.


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