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:
Dec. 13, 2022

Filed:

Dec. 18, 2017
Applicant:

Bombardier Inc., Dorval, CA;

Inventors:

Claude Tessier, Sainte-Adele, CA;

Gabriel Meunier, Saint-Bruno, CA;

Assignees:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G06F 30/15 (2020.01); B64F 5/60 (2017.01); G06F 30/20 (2020.01); G06F 113/28 (2020.01); B64C 13/00 (2006.01);
U.S. Cl.
CPC ...
G06F 30/15 (2020.01); B64F 5/60 (2017.01); G06F 30/20 (2020.01); B64C 13/00 (2013.01); G06F 2113/28 (2020.01);
Abstract

Methods and systems relating to the design and testing of systems that include hinged flight control surfaces of aircraft are disclosed. The systems and methods disclosed herein make use of a structural model representing a structural environment of the system in a relatively simple manner. In various embodiments, the structural model comprises one or more actuation branches having a common linear actuation direction, a load mass, and a massless connector representative of a hinge line of the flight control surface. The massless connector is connected to and disposed between the one or more actuation branches and the load mass and is movable along the common linear actuation direction so that linear movement of the massless connector is correlated to rotational movement of the hinged flight control surface.


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