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. 23, 2014

Filed:

Jun. 17, 2011
Applicants:

Arnaud Boucaud, Paris, FR;

Philippe Elie, Paris, FR;

Alexandre Guyamier, Paris, FR;

Van Lam Nguyen, Paris, FR;

Pascal Nauroy, Paris, FR;

Marc Pontrucher, Paris, FR;

Jean-francois Weibel, Paris, FR;

David Wong, Paris, FR;

Inventors:

Arnaud Boucaud, Paris, FR;

Philippe Elie, Paris, FR;

Alexandre Guyamier, Paris, FR;

Van Lam Nguyen, Paris, FR;

Pascal Nauroy, Paris, FR;

Marc Pontrucher, Paris, FR;

Jean-Francois Weibel, Paris, FR;

David Wong, Paris, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 13/50 (2006.01); B64C 25/24 (2006.01); B64C 13/04 (2006.01); H02J 4/00 (2006.01);
U.S. Cl.
CPC ...
H02J 4/00 (2013.01); B64C 25/24 (2013.01); B64C 13/04 (2013.01); B64C 13/50 (2013.01); B64D 2221/00 (2013.01);
Abstract

A power supply and control device for a plurality of electric actuators, the device comprising a control circuit and a power circuit, the power circuit having an inverter module connected to a switch module provided with connection means for connection to the actuators, the control circuit being connected to the switch module to operate it so as to connect the actuators sequentially to the inverter module, wherein the control circuit is arranged to control the inverter module and the switch module sequentially, and wherein the control circuit includes a monitoring module arranged to detect a malfunction of the device. An actuator assembly comprising a plurality of actuators and such a power supply and control device, and an aircraft including a plurality of actuators and such a power supply and control device of the above-specified type.


Find Patent Forward Citations

Loading…