Overlapping twisted radial aerofoil blades or vanes are formed on a compressor rotor or turbine disk or the like (102) by electro-discharge machining with a curved tool electrode which is in the form of an elongate and substantially rigid element other than a wire (150) which is turned by a tool holder (130) as it is advanced on a helical path to form the inner surface of each blade or vane with the outer curve of the electrode, or the outer surface of each blade or vane with the inner curve of the electrode, the disk being indexed to a next rotary position after each blade surface is machined.
申请公布号
WO2006027608(A1)
申请公布日期
2006.03.16
申请号
WO2005GB03491
申请日期
2005.09.09
申请人
BLADON JETS LIMITED;BLADON, CHRISTOPHER, GEORGE;BLADON, PAUL, DOUGLAS