Patent · US Active

Fibre-reinforced metal component for an aircraft or spacecraft and production methods for fibre-reinforced metal components

US10399657B2 · kind B2 · utility

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11References
9Claims
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Key dates

Filing dateOct 25, 2016
Grant dateSep 3, 2019
Priority date
Expiry dateJul 26, 2037

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02P10/25
  • WIPO fieldMaterials, metallurgy
  • WIPO sectorChemistry

Abstract

Production methods for producing a fiber-reinforced metal component having a metal matrix which is penetrated by a plurality of reinforcing fibers are provided. One method includes depositing in layers reinforcing fibers in fiber layers, depositing in layers and liquefying a metal modelling material in matrix material layers, and consolidating in layers the metal modelling material in adjacently deposited matrix material layers to form the metal matrix of the fiber-reinforced metal component. Here, the metal component is formed integrally from alternately deposited matrix material layers and fiber layers. An alternative method includes introducing an open three-dimensional fiberwoven fabric consisting of reinforcing fibers into a casting mold, pouring a liquid metal modelling material into the casting mold and consolidating the metal modelling material to form the metal matrix of the fiber-reinforced metal component. Here, the metal component is formed integrally from the consolidated metal modelling material and the reinforcing fibers.

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