Patent · US Active

Connection arrangement, particularly for aircraft structure parts

US8950707B2 · kind B2 · utility

3Cited by
13References
8Claims
0Family size

Assignee

Inventor

Key dates

Filing dateMay 31, 2012
Grant dateFeb 10, 2015
Priority date
Expiry dateJun 10, 2032

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49956
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

A connection arrangement for at least two abutting components to be firmly connected to one another, includes a self-piercing rivet having a rivet head for punching of a hole and subsequent riveting of the components, wherein a washer is allocated to the self-piercing rivet at the distal end region opposite to the rivet head, with the washer including a frontal area for the insertion of a circular indentation to create a firm compression connection between a hole in the washer and the distal end region of the self-piercing rivet.

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