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. 24, 2023

Filed:

Jul. 15, 2020
Applicant:

Beta Air, Llc, South Burlington, VT (US);

Inventors:

Cody Spiegel, Charlotte, VT (US);

Dale Williams, Winooski, VT (US);

Assignee:

BETA AIR, LLC, South Burlington, VT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 31/04 (2006.01); G05G 9/047 (2006.01); B64C 29/00 (2006.01); B64D 31/12 (2006.01); B64C 39/02 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0025 (2013.01); B64D 31/04 (2013.01); B64D 31/12 (2013.01); G05G 9/047 (2013.01); B64C 39/024 (2013.01); B64C 2201/146 (2013.01); B64C 2201/165 (2013.01);
Abstract

A combined hover and forward thrust control assembly for a dual-mode aircraft includes a support structure attached to an aircraft frame of an aircraft having at least a vertical thrust propulsor and at least a forward thrust propulsor a throttle lever rotatably mounted to the support structure, wherein rotating the throttle lever in a first direction increases power to at least a vertical thrust propulsor and rotating the throttle lever in a second direction decreases power to at least a vertical thrust propulsor and a linear thrust control mounted on the throttle lever, wherein movement of the linear thrust control in a first direction increases forward thrust of at least a forward thrust propulsor, and movement of the linear thrust control in a second direction decreases forward thrust of the forward thrust propulsor.


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