Patent · US Active

Rotary-shaft brake system, in particular for an aircraft rotor or propeller, including a linear actuator

US9157496B2 · kind B2 · utility

5Cited by
6References
13Claims
0Family size

Assignee

Inventor

Key dates

Filing dateNov 20, 2012
Grant dateOct 13, 2015
Priority date
Expiry dateApr 2, 2033

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16D2129/08
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

Rotary-shaft brake system includes a rotary braking member attached to a rotary shaft, first and second friction members arranged on either side of the rotary braking member, each friction member being moveable between a first braking position when the friction members are in contact with the rotary braking member and a second idle position away from the rotary braking member, a bracket holding the friction members and guiding device and control device controlling movement of the friction members on the bracket. The control device comprises a linear actuator acting on at least a first lever and a solid elastically deformable element.

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