Patent · US Active

Engine fastener for an aircraft

US9573694B2 · kind B2 · utility

0Cited by
5References
6Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 22, 2015
Grant dateFeb 21, 2017
Priority date
Expiry dateJul 8, 2035

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16C2326/43
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

An engine fastener for an aircraft, to secure an engine to a pylon and comprising a fastener body fixed to the pylon and having a cylindrical extension, and a fixing assembly comprising a paddle fixed to the engine and a connection arrangement joined to the paddle and arranged on the cylindrical extension to form a ball-and-socket joint between the cylindrical extension and the paddle. The connection arrangement comprises a ball, formed in one piece, having a central bore in which the cylindrical extension fits, and of which the outer surface is a spherical portion, a fixing element fixing the ball on the cylindrical extension, and two cages, each having an inner surface assuming the form of a spherical portion. The two inner surfaces are arranged opposite one another to house the ball, and for each cage, a joining element joins the cage to the paddle.

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