Method for the manufacture of metal vanes for turbomachinery

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

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Details

291568R, 291635R, 29412, 29415, 29DIG15, 29DIG37, 72177, 72180, 72203, 72206, 416223R, B21K 304, B23P 1502

Patent

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045312702

ABSTRACT:
To make vane airfoils for an axial flow compressor metal strip is first contour rolled to a cross section comprised of two opposing airfoils separated by a center rib, where one of the faces of the strip is kept planar. The rib is used to guide the strip into dies where it is notched and slotted to define individual airfoils. Next, die stamping makes concave the planar surface of each airfoil.

REFERENCES:
patent: 450836 (1891-04-01), Evans
patent: 814804 (1906-03-01), Rateau et al.
patent: 881409 (1908-03-01), Jude
patent: 1035545 (1912-08-01), Dake
patent: 1072233 (1913-09-01), Imle
patent: 1127740 (1915-02-01), Dake
patent: 2148672 (1939-02-01), Arentzen
patent: 4320647 (1982-03-01), Kummeling et al.
patent: 4357819 (1982-11-01), Elley

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