Method of manufacturing a blade or vane for a gas turbine engine

Metal founding – Process – Shaping liquid metal against a forming surface

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Details

164 34, 164 35, 164 36, B29D 2900, B29C 102

Patent

active

043846076

ABSTRACT:
A method of casting a blade or vane for a gas turbine engine which enables the production of more complex internal shapes than those which may be made by prior art methods. The method of the invention includes the steps of:

REFERENCES:
patent: 3961010 (1976-06-01), Holmes
patent: 3985176 (1976-10-01), Wamester

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