Patent · US Active

Mechanical flight control auxiliary power assist system

US7890222B1 · kind B1 · utility

5Cited by
6References
11Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 8, 2010
Grant dateFeb 15, 2011
Priority date
Expiry dateJan 8, 2030

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C27/59
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A mechanical flight control system for a rotary-wing aircraft is disclosed. The flight control system comprises an upstream portion, a downstream portion, and an assembly for connecting the upstream portion to the downstream portion. The assembly may comprise dual concentric valve actuators and/or a variety of system load limiting features.

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