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. 06, 2022

Filed:

Oct. 05, 2018
Applicant:

Leonardo S.p.a., Rome, IT;

Inventors:

Roberto Vanni, Samarate, IT;

Davide Gagliostro, Samarate, IT;

Davide Casola, Samarate, IT;

Assignee:

LEONARDO S.P.A., Rome, IT;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/00 (2006.01); G05D 1/08 (2006.01); B64C 13/04 (2006.01); B64C 13/30 (2006.01); B64C 13/40 (2006.01); B64C 13/50 (2006.01); F15B 18/00 (2006.01); G05G 11/00 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0816 (2013.01); B64C 13/04 (2013.01); B64C 13/30 (2013.01); B64C 13/40 (2013.01); B64C 13/50 (2013.01); F15B 18/00 (2013.01); G05D 1/0808 (2013.01); G05G 11/00 (2013.01);
Abstract

A stability and command augmentation system for controlling an aircraft, comprising: a first member moveable by a pilot input device to a first position defining a first input; a second member moveable to a second position associated with a second input; and an adder device configured to add the first and second inputs and supply an output signal defining a command for an element to be controlled of the aircraft; the stability and command augmentation system comprises: a casing, a first and a second piston integrally movable with one another inside the casing and operatively connected to the second member; and control means configured to exert a first force on the first piston and a second force on the second piston; the second force is independent of the first force.


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