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:
Jun. 26, 2018

Filed:

Jun. 12, 2015
Applicant:

Safran Electronics & Defense, Boulogne Billancourt, FR;

Inventors:

Oleg Gomolko, Boulogne Billancourt, FR;

Etienne Merlet, Boulogne Billancourt, FR;

Assignee:

Safran Electronics & Defense, Boulogne Billancourt, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 13/30 (2006.01); B64C 13/50 (2006.01);
U.S. Cl.
CPC ...
B64C 13/30 (2013.01); B64C 13/50 (2013.01);
Abstract

An actuator for hinging a first element to a second element about a first pivot axis (A), the actuator comprising a motor-drive device, a first mounting plate () connected to a body () of the motor-drive device, a second mounting plate () connected to the second element, the second mounting plate being mounted in the first mounting plate in order to pivot about the first axis, and a bush () mounted in the second mounting plate to pivot about a second axis (A) perpendicular to the first axis. The motor-drive device has an outlet shaft () pivotable about a third axis (A) perpendicular to the first axis and intersecting the first axis, and it is extended by a pin () that is pivotally received in the bush and that has a central axis (A) intersecting the first axis and the third axis, and forming an acute angle with the third axis. An aircraft guidance assembly including such an actuator.


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