Method for casting a directionally solidified article
View Patent ↗A method of casting a directionally solidified (DS) or single crystal (SX) article with a casting furnace having a heating chamber ( 4 ), a cooling chamber ( 5 ), a separating baffle ( 3 ) between the both chambers includes a first step in which the shell mould ( 12 ) is filled with liquid metal ( 15 ), and the liquid metal ( 15 ) is directionally solidified by withdrawing the shell mould ( 12 ) from the heating to the cooling chamber ( 4, 5 ). An inert gas impinges from nozzles ( 8 ) arranged below the baffle ( 3 ) on the shell mould ( 12 ) and in steep transitions in outer surface area of the shell mould ( 12 ) the flow of the inert gas ( 9 ) is reduced or even stopped and when a protruding geometrical feature has passed the impingement area of the gas jets, the gas flow ( 9 ) is restored to a value adjusted to the geometry of the cast part presently passing the impingement area.
1. A method of casting a directionally solidified (DS) or single crystal (SX) article with a casting furnace having a heating chamber with at least one heating element, a cooling chamber, and a separating baffle between the heating and the cooling chamber, the method comprising:
feeding the shell mould within the heating chamber with liquid metal through a filling device;
withdrawing the shell mould from the heating chamber through the baffle to the cooling chamber and thereby directionally solidifying the liquid metal forming the cast article;
after withdrawing an initial 5–50 mm of the shell mould into the cooling chamber, impinging an inert gas from nozzles arranged below the baffle on the shell mould and thereby forming an impingement area;
at least reducing, in steep increase in outer surface area or a protruding geometrical feature of the shell mould, the flow of the inert gas; and
when the steep increase or protruding geometrical feature has passed the impingement area of the gas jets, restoring the gas flow to a value adjusted to the geometry of the cast part presently passing the impingement area.
2. The method of claim 1 , further comprising:
directing the gas flow around the circumference of at least one article in the shell mould cluster in a homogeneous manner at a constant height below the baffle.
3. The method of claim 1 , comprising:
directing the gas flow downwards along the shell mould surface.
4. The method of claim 1 , further comprising:
casting the article in the casting furnace having a controlled background pressure of the inert gas.
5. The method of claim 1 , further comprising:
casting the article in the casting furnace with an inert gas comprising a mixture of different noble gases, and/or nitrogen.
6. The method of claim 1 , further comprising:
closing mechanical gas flow connections between the heating and cooling chamber during said withdrawing of the shell mould with a baffle having flexible fingers or brushes towards the shell mould, by closing the filling device with a movable lid and by a seal between the baffle and the heating element.
7. The method of claim 1 , further comprising:
casting the article in a shell mould with a controlled open porosity having pores which are filled with the inert gas.