Patent · US Active

Torque limiter in particular for an actuator of the nacelle of an aircraft turbojet engine

US9010204B2 · kind B2 · utility

1Cited by
10References
4Claims
0Family size

Assignee

Inventor

Key dates

Filing dateApr 7, 2010
Grant dateApr 21, 2015
Priority date
Expiry dateJan 16, 2032

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T403/32951
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

The invention relates to a torque limiter for an actuator including a screw (101), a nut mounted on said screw, an actuation tube (105) rigidly connected to the nut and means (109, 133) for rotating said screw, said limiter being characterized in that it includes an abutment (115, 110) capable of: preventing the rotation of said tube (105) by friction simply by an axial force exerted by said screw (101) onto said nut during the movement thereof; and enabling the rotation of said tube (105) when said nut arrives at an axial abutment of said screw beyond a predetermined torque threshold defined by the axial force.

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