Method of making gas turbine engine blades

Metal working – Means to assemble or disassemble – Puller or pusher means – contained force multiplying operator

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Details

29423, 29463, 164 35, 164516, 228182, 228193, 416233, B23P 1702

Patent

active

044173814

ABSTRACT:
A method of making a two part aerofoil gas turbine engine blade consisting of casting each individual part separately, the parts being cast by the lost wax process, and subsequently joining the parts together after machining.

REFERENCES:
patent: 3239897 (1966-03-01), Lirones
patent: 3241200 (1966-03-01), Lirones
patent: 3422880 (1969-01-01), Brown et al.
patent: 3596703 (1971-08-01), Bishop et al.
patent: 3656222 (1972-04-01), Jones
patent: 3981344 (1976-09-01), Hayes et al.

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