RTM injection method and mould using symmetric anti-pinching sectors
AssigneeSafran Aircraft Engines
InventorsRaoul Jaussaud, Hubert Jean Marie Fabre, Brian Jensen
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AssigneeSafran Aircraft Engines
InventorsRaoul Jaussaud, Hubert Jean Marie Fabre, Brian Jensen
Estimating the term…
An injection mold for the manufacture of an axisymmetric part of composite material comprising a mandrel supporting a fibrous preform and comprising an annular wall, and a plurality of counter-mold angular sectors assembled to the mandrel and intended to close the mold and to compact the fibrous preform wound on the mandrel. Each angular sector comprises an annular base intended to come into contact with the fibrous preform. The plurality of angular sectors includes a first series of angular sectors and a second series of angular sectors, first and second lateral edges of the first series of sectors each including a protruding lower portion, the first and the second lateral edges of the second series of sectors each including a recessed lower portion.
An injection mold for the manufacture of an axisymmetric part of composite material comprising:
A method of closing an injection mold for the manufacture of an axisymmetric part of composite material, the mold comprising:
Dependencies are inferred from the claim text.