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:
Sep. 20, 2022

Filed:

May. 07, 2018
Applicant:

Insitu, Inc., Bingen, WA (US);

Inventors:

Peter Josef Kunz, Kirkwood, MO (US);

David Wayne Goodrich, Moses Lake, WA (US);

Jacob Scott Allen, Mosier, OR (US);

Matthew Jacob Bartow, Hood River, OR (US);

Assignee:

Insitu, Inc., Bingen, WA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 39/02 (2006.01); B64C 29/00 (2006.01); B64C 29/04 (2006.01);
U.S. Cl.
CPC ...
B64C 39/024 (2013.01); B64C 29/0025 (2013.01); B64C 29/04 (2013.01); B64C 2201/021 (2013.01); B64C 2201/042 (2013.01); B64C 2201/088 (2013.01); B64C 2201/104 (2013.01); B64C 2201/108 (2013.01); B64C 2211/00 (2013.01);
Abstract

An aircraft includes a fuselage module and at least two vertical lift rotor modules supporting at least four rotor assemblies. Each rotor assembly is supported by a rotor boom having at least one boom free end and a boom mounting portion. Each rotor assembly has at least one vertical lift rotor mounted on the boom free end. Each boom mounting portion is removably couplable to the fuselage module. The vertical lift rotor modules are configured such that when coupled to the fuselage module, a pair of the rotor assemblies are located on each of laterally opposite sides of the fuselage module, and the rotor assemblies of each pair are respectively located forward of and aft of a wing center portion. A pair of wings are configured to be removably couplable to the wing center portion. The aircraft includes a forward thrust module removably couplable to the fuselage body.


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