Patent · US Active

Rotorcraft blade provided with a flap that is tiltable with the help of at least one main ball joint having a first shaft that is secured to said flap

US7585151B2 · kind B2 · utility

2Cited by
7References
8Claims
0Family size

Assignee

Inventors

Key dates

Filing dateOct 24, 2006
Grant dateSep 8, 2009
Priority date
Expiry dateJan 10, 2028

Classification

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

Abstract

The present invention relates to a rotorcraft rotor blade (1) having at least one trailing edge flap (5) that is tiltable, the flap (5) being suitable for pivoting about a virtual hinge axis (Y′) extending substantially along the span of the blade (1) and of the flap (5). The blade (1) is remarkable in that the flap (5) is provided with at least one main ball joint (30) having an inner cage (32) and an outer cage (33), and a first shaft (31) secured to the flap (5), the front portion (33′) of the outer cage (33) of the main ball joint (30) being connected to a linear actuator (10) which is arranged in the blade (1) and which enables the flap (5) to be pivoted, the first shaft (31) of the main ball joint (30) extending substantially perpendicularly to the virtual hinge axis (Y′) about which the flap (5) pivots.

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