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(11) | EP 2 286 938 A3 |
(12) | EUROPEAN PATENT APPLICATION |
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(54) | Refractory metal core for integrally cast exit trench |
(57) A refractory metal core (10') for use in casting a turbine engine part (12') has
a main portion (16') and a plurality of tabs (18') extending from the main portion
(16'). An end portion (22') has a first edge which joins together the plurality of
tabs (18') and a second edge, opposed to the first edge, located internally of an
exterior boundary (14') of the cast part (12').
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