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. 08, 2019

Filed:

May. 26, 2018
Applicant:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Inventors:

Steven Ray Ivans, Ponder, TX (US);

Nathan Gabriel Wu, Euless, TX (US);

Assignee:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/22 (2006.01); B64C 29/00 (2006.01); B64C 11/00 (2006.01); B64C 3/38 (2006.01); B64C 7/02 (2006.01); B64C 5/08 (2006.01); B64C 27/28 (2006.01); B64C 29/02 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 3/38 (2013.01); B64C 5/08 (2013.01); B64C 7/02 (2013.01); B64C 11/00 (2013.01); B64C 27/28 (2013.01); B64C 29/02 (2013.01);
Abstract

A pylon assembly for a tiltrotor aircraft includes a fixed pylon having an outboard end. A rotor assembly is rotatably coupled to the fixed pylon and is operable to rotate between a a vertical takeoff and landing orientation and a forward flight orientation. The rotor assembly includes a proprotor operable to produce a slipstream. A wing extension is rotatably coupled to the outboard end of the fixed pylon. The wing extension is operable to rotate generally with the rotor assembly such that a minimal dimension of the wing extension remains in the slipstream of the proprotor.


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