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:
Aug. 25, 2020

Filed:

Dec. 07, 2017
Applicant:

Textron Innovations Inc., Providence, RI (US);

Inventors:

Albert G. Brand, N. Richland Hills, TX (US);

Mark Loring Isaac, Fort Worth, TX (US);

Frank Bradley Stamps, Colleyville, TX (US);

Russell Lee Mueller, Coppell, TX (US);

Assignee:

Textron Innovations Inc., Providence, RI (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 11/28 (2006.01); B64C 27/54 (2006.01); B64C 11/48 (2006.01); B64C 27/28 (2006.01); B64C 27/30 (2006.01); B64D 35/06 (2006.01); F16H 48/10 (2012.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 11/28 (2013.01); B64C 11/48 (2013.01); B64C 27/28 (2013.01); B64C 27/54 (2013.01); B64D 35/06 (2013.01); F16H 48/10 (2013.01); B64C 27/30 (2013.01);
Abstract

A dual rotor propulsion system for a tiltrotor aircraft having VTOL and forward flight modes. The dual rotor propulsion system includes an engine operable to provide an input torque to a transmission that, responsive thereto, generates an output torque. A first output shaft is coupled to the transmission and is operable to receive a first portion of the output torque. A first rotor assembly is coupled to and rotatable with the first output shaft. A second output shaft is coupled to the transmission and is operable to receive a second portion of the output torque. A second rotor assembly is coupled to and rotatable with the second output shaft. In operation, the first and second rotor assemblies rotate coaxially, the first rotor assembly is a different diameter than the second rotor assembly and the first rotor assembly is stoppable and foldable in the forward flight mode.


Find Patent Forward Citations

Loading…