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:
Dec. 24, 2018

Filed:

Dec. 19, 2013
Applicant:

Rehco, Llc, Chicago, IL (US);

Inventors:

Jeffrey Rehkemper, Chicago, IL (US);

Keith Johnson, Roberts, WI (US);

Nicholas Grisolia, Lake Geneva, WI (US);

Assignee:

Rehco, LLC, Chicago, IL (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/32 (2005.12); B64C 27/43 (2005.12); B64C 27/52 (2005.12); B64C 27/473 (2005.12); B64C 27/14 (2005.12); A63H 27/133 (2005.12); A63H 27/00 (2005.12);
U.S. Cl.
CPC ...
B64C 27/32 (2012.12); A63H 27/12 (2012.12); B64C 27/14 (2012.12); B64C 27/43 (2012.12); B64C 27/473 (2012.12); B64C 27/52 (2012.12);
Abstract

A propeller related vehicle in accordance with one embodiment of the present invention is described as a helicopter having an airframe housing a motor mechanism for powering a main propeller attached to a main drive shaft that extends vertically through the airframe and for powering a tail rotor. The helicopter further includes a horizontal stabilizing mechanism attached between the main propeller and the main drive shaft, which permits the main propeller to freely pivot about the main drive shaft independently from the airframe. As such when the main propeller is rotating and the main propeller begins to pitch, the rotating main propeller has a centrifugal force created by the rotation thereof and will tend to pivot about the horizontal stabilizing mechanism in a manner that offsets the pitch such that the helicopter remains in a substantially horizontal position. In addition various main propeller configurations may be employed that provide additional self-stabilization.


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