Lined centrifugal mould with controlled thermal inertia

Patent metadata

Field	Value
Publication number	US-9764382-B2
Application number	US-201515115218-A
Country	US
Kind code	B2
Filing date	Jan 28, 2015
Priority date	Jan 31, 2014
Publication date	Sep 19, 2017
Grant date	Sep 19, 2017

Abstract

The invention concerns a unit comprising a mold ( 4 ) adapted to receive a molten metal alloy and the said metal alloy poured therein. The alloy is TiAl. The mold is rotational and comprises receiving recesses ( 135 ) made of steel, metal alloy and/or ceramic, and, at the location of a plurality of section planes each passing through the mold and the poured metal alloy, the mold has a surface heat capacity less than that of the poured metal alloy.

First claim

The invention claimed is:

1. Unit comprising:
a mould rotating around an axis, for centrifuge casting,
and a TiAl metal alloy poured thereinto,
the mould including:
receiving recesses made of soft steel, steel, metal alloy and/or ceramic, adapted to receive the centrifuge casting of the said molten TiAl metal alloy, the recesses extending radially around the axis, and
liners defining all the recesses and which are housed in at least one hollow soft steel, steel or metal alloy exoskeleton, and
at the location of a plurality of section planes each passing through the mould and the poured metal alloy, the mould having a surface heat capacity less than that of the poured metal alloy,
of which:
the exoskeleton or exoskeletons is/are open-worked, or
an empty space exists around the periphery between each liner and the exoskeleton that surrounds it, or
an alveolar structure exists around the periphery between each liner and the exoskeleton that surrounds it.

2. A centrifuge casting mould, specific for the unit of claim 1 , the mould being rotational around an axis and comprising:
several receiving recesses to receive a molten TiAl alloy extending radially around the axis, and
liners defining all the recesses and which are housed in at least one hollow exoskeleton, the exoskeleton or exoskeletons being made of soft steel, steel or metal alloy, and the liner being made of soft steel, steel or metal alloy and/or ceramic, and
the exoskeleton or exoskeletons is/are open worked, or
an empty space exists around the periphery between each liner and the exoskeleton that surrounds it, or
an alveolar structure exists around the periphery between each liner and the exoskeleton that surrounds it.

3. The mould of claim 2 , comprising a central block having ducts through which the alloy is poured and which are connected to the interior liners, and at least one fixing, preferably removable, is implemented:
between each liner and the exoskeleton that surrounds it, and/or
between each liner and/or the exoskeleton that surrounds it and the central block.

4. The mould of claim 2 , wherein the liners being filled with molten metal alloy, the said mould has a surface heat capacity less than that of the contained metal alloy, this occurring at a plurality of section planes passing respectively through at least one of the said liners and the exoskeleton that surrounds it and the contained metal alloy.

Assignees

• Safran Aircraft Engines

Inventors

• Martin Guillaume
• Fargeas Serge
• Soisson Marc
• Piaton Valéry

Classifications

• B22D13/101

  Moulds · CPC title

• B22D27/20

  Measures not previously mentioned for influencing the grain structure or texture; Selection of compositions therefor · CPC title

• B22D13/102 Primary

  Linings for moulds (making or lining moulds B22C) · CPC title