Patent · US Active

Fastening device particularly suitable for the fastening between an air intake and an engine of an aircraft nacelle

US9139306B2 · kind B2 · utility

1Cited by
11References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 3, 2012
Grant dateSep 22, 2015
Priority date
Expiry dateAug 3, 2032

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

An aircraft nacelle with a connecting device between a first conduit of an air intake and a second conduit of a motor, both conduits being arranged end-to-end, the connecting device including an annular flange connected to the air intake, an annular flange connected to the motor pressed against annular flange of the air intake, the flanges extending in a plane perpendicular to the longitudinal axis of the nacelle; bolt holes formed in annular flanges and disposed plumb to one another; and connecting elements located in bolt holes, for connecting the annular flanges, wherein at least one flange includes at least one opening interposed between a bolt hole and junction zone of the flange and/or between a bolt hole and outer edge of the flange.

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