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. 20, 2026

Filed:

Jan. 10, 2022
Applicant:

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

Inventors:

Brent C. Ross, Flower Mound, TX (US);

Kirk L. Groninga, Keller, TX (US);

Steven R. Ivans, Ponder, TX (US);

Steve R. Schafer, Fort Worth, TX (US);

Brad Joseph Passe, Irving, TX (US);

Nicholas Ralph Carlson, Dallas, TX (US);

Kip Gregory Campbell, Hurst, TX (US);

Bradley Paul Regnier, Fort Worth, TX (US);

Steven G. Hagerott, Wichita, KS (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 9/20 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 29/00 (2013.01); B64C 9/20 (2013.01);
Abstract

One embodiment is an aircraft including a fuselage; a wing connected to the fuselage; first and second booms connected to the wing on opposite sides of the fuselage; first and second forward propulsion systems attached to forward ends of the first and second booms; first and second aft propulsion systems fixedly attached proximate aft ends of the first and second booms; and first and second wing-mounted propulsion systems connected to outboard ends of wings; wherein the first and second wing-mounted propulsion systems are tiltable between a first position when the aircraft is in a hover mode and a second position when the aircraft is in a cruise mode.


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