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LASER JOINING OF CMC STACKS
A method of manufacturing a gas turbine engine component (10) and the component so formed. The method includes: stacking a plurality of CMC layers (16) along a metal core (30) to form a stack of disconnected CMC layers, wherein adjacent edge faces (46) of the layers define a surface (44); additively depositing ceramic material (14) to only selected portions of the surface (44) to bond together at least some of the layers at their respective edge faces; and selecting locations for the depositing of the ceramic material to achieve a predetermined mechanical characteristic of the resulting component.
LASER JOINING OF CMC STACKS
A method of manufacturing a gas turbine engine component (10) and the component so formed. The method includes: stacking a plurality of CMC layers (16) along a metal core (30) to form a stack of disconnected CMC layers, wherein adjacent edge faces (46) of the layers define a surface (44); additively depositing ceramic material (14) to only selected portions of the surface (44) to bond together at least some of the layers at their respective edge faces; and selecting locations for the depositing of the ceramic material to achieve a predetermined mechanical characteristic of the resulting component.
LASER JOINING OF CMC STACKS
LASERFÜGUNG VON CMC-STAPELN
ASSEMBLAGE PAR LASER D'EMPILEMENTS DE CMC
DASGUPTA ARINDAM (author) / KULKARNI ANAND A (author) / KAMEL AHMED (author)
2019-01-23
Patent
Electronic Resource
English
British Library Online Contents | 2018
|British Library Online Contents | 2018
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