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.
Patent No.:
Date of Patent:
Oct. 02, 2018
Filed:
Jul. 13, 2016
Applicant:
Embraer S.a., São José dos Campos-SP, BR;
Inventors:
Gustavo Jose Zambrano, São José dos Campos, BR;
Tiago Francisco Gomes Da Costa, São José dos Campos, BR;
Fernando Antonio Pavão, São José dos Campos, BR;
Assignee:
Embraer S.A., São José dos Campos, BR;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/16 (2006.01); B64C 25/34 (2006.01); B64C 25/42 (2006.01); B64C 25/50 (2006.01); B60T 7/04 (2006.01); B60T 8/17 (2006.01); B64D 45/00 (2006.01); B60T 8/32 (2006.01); B60T 8/18 (2006.01);
U.S. Cl.
CPC ...
B64C 13/16 (2013.01); B60T 7/042 (2013.01); B60T 8/1703 (2013.01); B60T 8/325 (2013.01); B64C 25/34 (2013.01); B64C 25/42 (2013.01); B64C 25/50 (2013.01); B64D 45/00 (2013.01); B60T 8/18 (2013.01); B60T 2230/03 (2013.01); B60T 2230/04 (2013.01);
Abstract
A flight control law enhances braking efficiency through the operation of aircraft elevators (or another pitch control system) using measured longitudinal acceleration and/or pedal position as references to the control law. Through this solution, it is possible to increase the vertical load in the main landing gear and consequently enhance braking efficiency.