Patent · US Active

Rotorcraft blade provided with a tiltable flap

US7578654B2 · kind B2 · utility

3Cited by
6References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateOct 24, 2006
Grant dateAug 25, 2009
Priority date
Expiry dateJan 8, 2028

Classification

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

Abstract

A rotorcraft rotor blade (1) includes at least one tiltable trailing-edge flap (5), 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 it is provided with at least one main ball joint (30) provided with an inner cage (32) together with a first pin (31) and an outer cage (33), the front portion (33′) of the outer cage (33) of the main ball joint (30) being connected to a linear actuator (10, 10′) arranged in the blade (1) and serving to pivot the flap (5), the first pin (31) of the main ball joint (30) being substantially perpendicular to the virtual hinge axis (Y′) about which the flap (5) pivots.

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