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:
Jan. 21, 2020

Filed:

Dec. 21, 2016
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Jan A. Kordel, Redmond, WA (US);

Jacob Daniel Virnig, Woodinville, WA (US);

Michael Albert Balzer, Bellevue, WA (US);

Bruce Detert, Seattle, WA (US);

Emanuel Rizal Setiawan, Kent, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/50 (2006.01); B64C 9/20 (2006.01); B64C 3/44 (2006.01); B64C 9/14 (2006.01);
U.S. Cl.
CPC ...
B64C 3/50 (2013.01); B64C 9/20 (2013.01); B64C 2003/445 (2013.01); B64C 2009/143 (2013.01);
Abstract

A high-lift device surface and associated method of designing the high-lift device surface is described. The flap can be attached to a wing on aircraft. The method can involve determining a manufactured shape of the flap. The manufactured flap shape can be deflected in some manner, such as bent or twisted, so that under selected flight conditions, such as cruise, the manufactured flap shape morphs into a second desired shape that satisfies specified constraints, such as geometric and sealing constraints. An advantage of the approach is that the flap doesn't have to be mechanically forced, using mechanical elements, into the second desired shape. The elimination of the mechanical elements results in weight and cost savings to aircraft on which the flap is deployed.


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