Patent · US Active

Actuation system for an active element in a rotor blade

US9180965B2 · kind B2 · utility

0Cited by
9References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 28, 2012
Grant dateNov 10, 2015
Priority date
Expiry dateMay 21, 2034

Classification

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

Abstract

In accordance with one embodiment of the present application, an actuation system is configured for actuation of an airfoil member with a flap mechanism. The actuation system can include an upper drive tape and a lower drive tape, each partially wrapped around a first bearing and second bearing. An inboard frame can be actuated by at least one linear actuator. Similarly, an outboard frame can be actuated by at least one linear actuator. The inboard frame is coupled to the upper drive tape, while the outboard frame is coupled to the lower drive tape. An actuation of the inboard frame and outboard frame in a reciprocal manner acts move a flap input lever reciprocally upward and downward. A flap mechanism is configured to convert the movement of the flap input lever into rotational movements of the airfoil member.

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