Integrale Schaufel-Rotoreinheit

A method of making an integrally bladed disc for a gas turbine engine, the disc having at least one blade the radially outermost surface of which is coated with a material harder than that of the blade, the method comprising the steps of: providing a forged disk blank of a first material; friction s...

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Bibliographische Detailangaben
Hauptverfasser: FOSTER, DEREK JOHN, BRISTOL BS17 6DE, GB, MOLONEY, KEITH CHARLES, OLDBURY ON SEVERN, BRISTOL BS12 1QD, GB, GILLBANKS, PETER JOHN, BRISTOL BS15 5PW, GB
Format: Patent
Sprache:ger
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Beschreibung
Zusammenfassung:A method of making an integrally bladed disc for a gas turbine engine, the disc having at least one blade the radially outermost surface of which is coated with a material harder than that of the blade, the method comprising the steps of: providing a forged disk blank of a first material; friction surfacing at least part of the circumference of the blank with a second material harder than the first material; and machining the blank so as to provide an integrally balded disc wherein the radially outermost surface of at least one blade is coated with said second material.