Patent · US Active

Insulation design for thermal and acoustic insulation of an aircraft

US8327976B2 · kind B2 · utility

4Cited by
37References
13Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 20, 2009
Grant dateDec 11, 2012
Priority date
Expiry dateNov 25, 2029

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

The invention pertains to an insulation structure for thermally and acoustically insulating an aircraft that features at least one heavy layer, wherein the insulation structure according to the invention is characterized in that the insulation structure comprises an additional absorption layer, in that the heavy layer is perforated at least in certain areas, and in that the perforated area ratio of the heavy layer is adapted in such a way that the heavy layer is essentially transparent to sound for frequencies below a double-wall frequency of the insulation structure. This makes it possible to dampen sound with low frequencies below the double-wall frequency as effectively as possible.

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