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:
May. 14, 2019

Filed:

May. 26, 2010
Applicants:

Amit Wolff, Zur Moshe, IL;

Guy Dekel, Kazir, IL;

Lior Zivan, Hadera, IL;

Inventors:

Amit Wolff, Zur Moshe, IL;

Guy Dekel, Kazir, IL;

Lior Zivan, Hadera, IL;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/22 (2006.01); B64C 29/00 (2006.01); B64C 39/02 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 27/22 (2013.01); B64C 39/024 (2013.01); B64C 2201/021 (2013.01); B64C 2201/042 (2013.01); B64C 2201/088 (2013.01); B64C 2201/126 (2013.01); B64C 2201/165 (2013.01); B64C 2211/00 (2013.01);
Abstract

In embodiments, a system and method for providing propulsion and control to an air vehicle, and for operating the vehicle, include at least three propulsion units that provide vertical thrust for vectored thrust flight, in which at least one or two of the propulsion units also provide thrust for vectored thrust cruising or aerodynamic flight by suitably tilting the respective propulsion units for changing the thrust vector. At the same time, the three or more propulsion units are operated to generate controlling moments to the air vehicle about three orthogonal axes, pitch, roll and yaw, during vectored thrust flight (hover, cruising, etc.) or during aerodynamic flight for controlling the vehicle.


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