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. 18, 2020

Filed:

Apr. 14, 2016
Applicant:

Japan Aerospace Exploration Agency, Chofu-shi, Tokyo, JP;

Inventors:

Mitsuhiro Murayama, Chofu, JP;

Kazuomi Yamamoto, Chofu, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 9/20 (2006.01); B64C 23/06 (2006.01); B64C 3/10 (2006.01); B64C 9/18 (2006.01);
U.S. Cl.
CPC ...
B64C 9/20 (2013.01); B64C 3/10 (2013.01); B64C 9/18 (2013.01); B64C 23/06 (2013.01); Y02T 50/162 (2013.01);
Abstract

The present invention is directed to reducing noise resulting from a wing tip vortex of a wing such as a flap. A flap of an aircraft includes a flap main body provided to a parent wing in a deployable manner, and a vortex generation portion including a protruding member, the protruding member being provided to protrude from an upper surface at least at an end of the flap main body on an outboard side in a span direction and forming a predetermined angle to an axial direction of the aircraft. A rear end of the protruding member is located on the side adjacent to a side-end edge at the end of the flap main body in the span direction relative to a virtual line passing through a front end of the protruding member and being parallel to the axial direction.


Find Patent Forward Citations

Loading…