Patent · US Active

Take-up device for thrust forces with connecting rods for aircraft engine attachment pylon, integrating three aligned ball joints

US8613404B2 · kind B2 · utility

4Cited by
7References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 22, 2011
Grant dateDec 24, 2013
Priority date
Expiry dateDec 2, 2031

Classification

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

Abstract

The present invention relates to a take-up device for thrust forces (14) for an aircraft engine attachment pylon (4), comprising a first fitting (194) attached to a rigid structure (108) of the attachment pylon, and two lateral connecting rods (14a) for take-up of thrust forces. It also comprises an axis system (190) bearing three first ball joint organs (192a, 196a) arranged along the latter and belonging respectively to a primary ball joint (192) and two secondary ball joints (196) arranged on either side of the primary ball joint, the first fitting (194) integrating a second ball joint organ (192b) cooperating with the first organ (192a) of the primary ball joint (192), and an end of each of the two connecting rods (14a) integrating a second ball joint organ (196b) cooperating respectively with the first organs (196a) of the two secondary ball joints (196).

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