Patent · US Active

Methods and apparatus for a distributed aircraft actuation system

US11591070B2 · kind B2 · utility

0Cited by
3References
28Claims
0Family size

Assignee

Inventors

Key dates

Filing dateOct 21, 2019
Grant dateFeb 28, 2023
Priority date
Expiry dateMar 22, 2041

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D2045/001
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

Methods, apparatus, and articles of manufacture for a distributed aircraft actuation system are disclosed. An example apparatus includes a non-responsive component detector to determine a position difference between a first position of a first control surface of an aircraft and a second position of a second control surface of the aircraft, the first position lagging the second position, and a command generator, in response to determining that the position difference satisfies a threshold, the command generator is to cease movement of the second control surface at the second position, attempt to move the first control surface to the second position, and cease movement of the first control surface when moved to the second position.

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