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. 07, 2020

Filed:

Feb. 09, 2017
Applicant:

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

Inventors:

Troy Cyril Schank, Fort Worth, TX (US);

Carlos Alexander Fenny, Fort Worth, TX (US);

Andrew Maresh, Fort Worth, TX (US);

Chyau-Song Tzeng, Fort Worth, TX (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/54 (2006.01); B64C 11/28 (2006.01); B64C 29/00 (2006.01); B64C 27/30 (2006.01); B64D 27/20 (2006.01);
U.S. Cl.
CPC ...
B64C 11/28 (2013.01); B64C 27/30 (2013.01); B64C 29/0033 (2013.01); B64D 27/20 (2013.01);
Abstract

A mechanism for transitioning a tiltrotor aircraft between rotary and non rotary flight modes. The mechanism includes a gimbal lock positioned about a mast that is operable to selectively enable and disable a gimballing degree of freedom of a rotor assembly relative to the mast. A blade stop assembly, positioned about the mast, includes a plurality of arms having a radially contracted orientation and a radially extended orientation. A blade lock assembly is operably associated with each rotor blade assembly. Each blade lock assembly is operable to selectively enable and disable a folding degree of freedom and a pitching degree of freedom of the respective rotor blade assembly. A swash plate is operable to change the pitch of the rotor blade assemblies in the rotary flight mode and fold the rotor blade assemblies in the non rotary flight mode.


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