Patent · US Active

Device for mechanical connection of a control surface to a fixed structural element of an aircraft and aircraft wing element equipped with said device

US9376203B2 · kind B2 · utility

4Cited by
3References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 25, 2013
Grant dateJun 28, 2016
Priority date
Expiry dateSep 12, 2034

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/40
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A device for mechanically connecting a control surface to a fixed structural element of an aircraft, including a rotary actuator for driving an element that is securely connected to the control surface in rotation in relation to an element securely connected to the fixed structural element, around an articulation axis, as well as articulation elements for articulating this control surface around this axis. These articulation elements are able to support the control surface independently of the rotary actuator. This arrangement permits taking benefit from the advantageous properties of rotary actuators while allowing removal of the rotary actuator without having first to remove the control surface.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.