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. 04, 2020

Filed:

May. 12, 2017
Applicant:

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

Inventors:

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

Rohn Lee Olson, Hurst, TX (US);

Andrew James Zahasky, North Richland Hills, TX (US);

Assignee:

BELL HELICOPTER TEXTRON INC., Fort Worth, TX (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 39/06 (2006.01); B64C 27/08 (2006.01); B64C 11/28 (2006.01); B64C 27/50 (2006.01); B64C 29/00 (2006.01); B64C 3/10 (2006.01); B64C 27/12 (2006.01); B64D 27/24 (2006.01); B64D 31/00 (2006.01); B64C 29/02 (2006.01); B64C 1/06 (2006.01); B64C 39/02 (2006.01); B64C 1/00 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64C 39/062 (2013.01); B64C 1/068 (2013.01); B64C 3/10 (2013.01); B64C 11/28 (2013.01); B64C 27/08 (2013.01); B64C 27/12 (2013.01); B64C 27/50 (2013.01); B64C 29/0025 (2013.01); B64C 29/02 (2013.01); B64C 39/024 (2013.01); B64C 39/06 (2013.01); B64D 27/24 (2013.01); B64D 31/00 (2013.01); B64C 2001/0045 (2013.01); B64D 2027/026 (2013.01);
Abstract

An aircraft capable of vertical takeoff and landing and stationary flight includes a distributed airframe coupled to a modular fuselage. The modular fuselage has a longitudinal axis substantially parallel to a rotational axis of three or more propellers. The modular fuselage includes a rear module substantially disposed within a perimeter of the distributed airframe, a front module removably connected to the rear module and substantially aligned with the longitudinal axis. One or more engines or motors are disposed within or attached to the distributed airframe or fuselage. The three or more propellers are proximate to a leading edge of the distributed airframe, distributed along the distributed airframe, and operably connected to the one or more engines or motors to provide lift whenever the aircraft is in vertical takeoff and landing and stationary flight.


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