Metal deforming – With temperature modification of tool or of specified... – Cooling
Patent
1979-09-10
1981-09-29
Larson, Lowell A.
Metal deforming
With temperature modification of tool or of specified...
Cooling
291568B, 2940221, B21K 304
Patent
active
042915660
ABSTRACT:
A worn titanium blade for a gas turbine engine has metal displaced at its aerofoil tip, so that the aerofoil can be dressed to restore it to length. The titanium is not amenable to cold forging, or to being entirely heated, a forge is therefore provided which has dies which contact only the immediate area containing the metal to be displaced. The dies are heatable so as to heat the said area by conduction and powered so as to apply suitable pressure in a way which brings about isothermal displacement of the titanium.
REFERENCES:
patent: 2741469 (1956-04-01), Wallerus
patent: 2760543 (1956-08-01), Wood
patent: 3461709 (1969-08-01), McMillen
patent: 4095451 (1978-06-01), Watton
Larson Lowell A.
Rolls-Royce Limited
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