Patent · US Active

Thrust reverser cascade for an aircraft nacelle

US11506144B2 · kind B2 · utility

0Cited by
4References
15Claims
0Family size

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Key dates

Filing dateFeb 7, 2020
Grant dateNov 22, 2022
Priority date
Expiry dateFeb 11, 2040

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldOther special machines
  • WIPO sectorMechanical engineering

Abstract

A thrust reverser cascade for an aircraft nacelle includes a plurality of blades having a first and a second surface, the blades being connected to members connected to attachment flanges for attaching the thrust reverser cascade to the nacelle. At least one of the surfaces of the blades is covered with at least one layer of fibers, each layer including a plurality of fiber pieces which are pre-impregnated with resin. The fiber pieces are superimposed on one another, positioned parallel to the aerodynamic surface of the blade and oriented in different directions.

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