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:
Mar. 26, 2019

Filed:

Dec. 04, 2013
Applicant:

Tamarack Aerospace Group, Inc., Sandpoint, ID (US);

Inventor:

Nicholas R. Guida, Sagle, ID (US);

Assignee:

Tamarack Aerospace Group, Inc., Sandpoint, ID (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 23/00 (2006.01); B64C 23/06 (2006.01); B64C 3/14 (2006.01);
U.S. Cl.
CPC ...
B64C 23/069 (2017.05); B64C 2003/148 (2013.01); Y02T 50/12 (2013.01); Y02T 50/164 (2013.01);
Abstract

A flow interrupting device may cause a flow to separate from a wingtip device at a desired angle of attack. The flow interrupting device may be coupled to a leading edge of a wingtip device where a flow disruptor may be configured to alleviate a load on the wingtip device. The flow disrupter may comprise an edge that extends into a boundary layer at a threshold angle of attack that may disrupt the boundary layer and cause a flow to separate from the wingtip device. This separated flow may reduce stresses experienced by the wingtip device and wing during various flight conditions where a transverse flow is encountered.


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