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. 05, 2019

Filed:

Jun. 08, 2014
Applicant:

Israel Aerospace Industries Ltd., Lod, IL;

Inventors:

Michael Shepshelovich, Ganei Tikva, IL;

Danny Abramov, Rehovot, IL;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 9/20 (2006.01); B64C 3/14 (2006.01); B64C 9/32 (2006.01); B64C 3/50 (2006.01); B64C 21/02 (2006.01);
U.S. Cl.
CPC ...
B64C 9/20 (2013.01); B64C 3/14 (2013.01); B64C 3/50 (2013.01); B64C 9/323 (2013.01); B64C 21/02 (2013.01); B64C 2003/147 (2013.01); B64C 2230/20 (2013.01); Y02T 50/12 (2013.01); Y02T 50/32 (2013.01);
Abstract

Two element aerofoils are provided, having an aerofoil chord, a primary element having a first leading edge and a first trailing edge, a secondary element having a second leading edge and a second trailing edge, a gap between the primary element and the secondary element, and an axial overlap between the first trailing edge and the second leading edge. The secondary element is deflectable with respect to the primary element about a fixed hinge point by a flap deflection angle. The secondary element is configured to operate in airbrake mode when deflected by a respective the flap deflection angle corresponding to a design airbrake deflection angle wherein to generate an airbrake drag. In at least some examples, the axial overlap is numerically greater than −0.5% of the aerofoil chord, at least for the design airbrake deflection angle. Also disclosed are methods for operating air vehicles, and methods for designing two-element aerofoils.


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