Method of manufacturing an article by diffusion bonding and superplastic forming
AssigneeROLLS-ROYCE plc
InventorStephen Nicholson
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AssigneeROLLS-ROYCE plc
InventorStephen Nicholson
Estimating the term…
A method of manufacturing a gas turbine engine fan blade (10) comprises forming three metal workpieces (50,52,54). A metal slab (30) is upset forged at both ends (32,34) to produce a metal block (40) with increased thickness (42,44) extending from opposite surfaces (36,38). The metal block (40) is cut in an inclined path to form two of the metal workpieces (50,52). The metal workpieces (50,52,54) are assembled into a stack (56) so that the flat surfaces (38,42,46,48) are in mating abutment. Heat and pressure is applied across the thickness of the metal workpieces (50,52,54) to diffusion bond the metal workpieces (53,52,54) together to form an integral structure (100). The integral structure (100) is hot creep formed and superplastically formed to produce the required aerofoil shape and the thickened end is machined to form the blade root (26). The method enables thinner metallic workpieces with better microstructure to be used and increases the yield of metallic workpieces.
A method of manufacturing an article of predetermined finished profile by diffusion bonding and superplastic forming at least two metal workpieces comprising the steps of:
Dependencies are inferred from the claim text.