Patent · US Active

Acoustic panel for a turbojet engine nacelle, with in-built fasteners

US8579078B2 · kind B2 · utility

2Cited by
3References
10Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 24, 2013
Grant dateNov 12, 2013
Priority date
Expiry dateJan 24, 2033

Classification

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

Abstract

An acoustic panel is provided that includes at least one cellular core arranged between at least an internal skin and an external skin, wherein the external skin incorporates at least one fastener able to collaborate in a disconnectable fashion with a complementary fastener associated with a structure to which it is to be attached.

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