Patent · US Active

Aircraft flap actuator assembly

US8763953B2 · kind B2 · utility

18Cited by
6References
7Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 14, 2010
Grant dateJul 1, 2014
Priority date
Expiry dateDec 25, 2030

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/30
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An aircraft flap actuator assembly includes at least one fixed support, at least one track having a curvilinear track surface connected to the fixed support, at least one flap support adapted to traverse the curvilinear track surface, a trailing edge flap connected to the at least one flap support and a flap actuator engaging the at least one flap support.

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