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:
May. 17, 2022

Filed:

Aug. 29, 2019
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Sergey D. Barmichev, Kirkland, WA (US);

Mithra M. K. V. Sankrithi, Edmonds, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 5/10 (2006.01); B64C 9/00 (2006.01); B64C 5/02 (2006.01);
U.S. Cl.
CPC ...
B64C 5/10 (2013.01); B64C 5/02 (2013.01); B64C 9/00 (2013.01);
Abstract

Provided are vertical tail structures with symmetry action slat systems. Specifically, a vertical tail structure comprises a main element and a leading edge element. The leading edge element comprises a first slat body and a second slat body that are symmetrically positioned on either side of a longitudinal centerline of the vertical tail structure. Each slat body is configured to move between a retracted position and an extended position to increase a camber sag of an airfoil of the vertical tail structure and thereby increase a maximum aerodynamic yawing moment provided by the vertical tail structure. In a first operable mode, each of the slat bodes are in the respective retracted position. In a second operable mode, one of the slat bodies is in the respective extended position. The extended position of each of the slat bodies includes a pitch angle and an extension distance from the main element.


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