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:
Dec. 06, 2022

Filed:

May. 25, 2021
Applicant:

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

Inventors:

Brent Chadwick Ross, Flower Mound, TX (US);

Alan Carl Ewing, Keller, TX (US);

Steven Ray Ivans, Ponder, TX (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/26 (2006.01); B64C 27/06 (2006.01); B64C 27/82 (2006.01); B64C 3/10 (2006.01); B64C 5/02 (2006.01); B64D 27/14 (2006.01); B64D 27/02 (2006.01); F02C 6/00 (2006.01); F02K 3/04 (2006.01);
U.S. Cl.
CPC ...
B64C 27/26 (2013.01); B64C 3/10 (2013.01); B64C 5/02 (2013.01); B64C 27/06 (2013.01); B64C 27/82 (2013.01); B64D 27/02 (2013.01); B64D 27/14 (2013.01); B64C 2027/8209 (2013.01); B64C 2027/8263 (2013.01); B64D 2027/026 (2013.01); F02C 6/00 (2013.01); F02K 3/04 (2013.01); F05D 2220/329 (2013.01);
Abstract

A fully compounding rotorcraft includes a fuselage having first and second wings extending therefrom and configured to provide lift compounding responsive to forward airspeed. A twin boom includes first and second tail boom members that extend aftward from the first and second wings. An empennage is coupled between the aft ends of the tail boom members. An anti-torque system includes a tail rotor that is rotatably coupled to the empennage. An engine is disposed within the fuselage and is configured to provide torque to a main rotor assembly via an output shaft and a main rotor gearbox. An auxiliary propulsive system is coupled to the fuselage and is configured to generate a propulsive thrust to offload at least a portion of a thrust requirement from the main rotor during forward flight, thereby providing propulsion compounding to increase the forward airspeed of the rotorcraft.


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