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:
Oct. 19, 2021

Filed:

Mar. 29, 2020
Applicant:

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

Inventors:

Daniel Bryan Robertson, Southlake, TX (US);

Kirk Landon Groninga, Keller, TX (US);

Steven Ray Ivans, Ponder, TX (US);

Matthew Edward Louis, Fort Worth, TX (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/22 (2006.01); B64C 29/00 (2006.01); B64C 27/26 (2006.01); B64D 33/04 (2006.01); B64C 15/14 (2006.01); B64C 27/30 (2006.01); B64C 21/00 (2006.01); B64C 3/10 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0025 (2013.01); B64C 15/14 (2013.01); B64C 21/00 (2013.01); B64C 27/26 (2013.01); B64C 27/30 (2013.01); B64D 33/04 (2013.01); B64C 3/10 (2013.01); B64C 2230/04 (2013.01); B64C 2230/06 (2013.01); B64C 2230/16 (2013.01);
Abstract

An aircraft operable to transition between thrust-borne lift in a VTOL orientation and wing-borne lift in a forward flight orientation. The aircraft has a blended wing body and includes an engine, a trinary lift fan system, a forced air bypass system and an exhaust system. The engine has a turboshaft mode and a turbofan mode. The lift fan system includes a plurality of ducted fans in a tandem lateral and forward orientation. In the VTOL orientation of the aircraft, the engine is in the turboshaft mode coupled to the lift fan system such that the engine provides rotational energy to the ducted fans generating the thrust-borne lift. In the forward flight orientation of the aircraft, the engine is in the turbofan mode coupled to the forced air bypass system such that bypass air combines with engine exhaust in the exhaust system to provide forward thrust generating the wing-borne lift.


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