Method for forming cooling slot in airfoil blades

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

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291568B, B23P 1504, B23P 1302

Patent

active

039343227

ABSTRACT:
A cooling slot for passing cooling fluid through a heated plate such as an airfoil blade for use in gas turbine engines is created by forming a first plurality of passages within the blade, and then forming a second plurality of passages within the blade, wherein preselected of the passages of the second plurality intersect at least one of the passages of the first plurality to define a number of nodes between the points of intersection. When cooling fluid is passed through the blade, the nodes act as turbulence promoters and area increasers for improving convective heat transfer between the blade and the cooling fluid.

REFERENCES:
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patent: 1884612 (1932-10-01), Dinzl
patent: 3026605 (1962-03-01), Turner
patent: 3329596 (1967-07-01), Abt et al.
patent: 3420502 (1969-01-01), Howald
patent: 3527543 (1970-09-01), Howald
patent: 3688833 (1972-09-01), Bykov et al.
patent: 3700348 (1972-10-01), Corsmeier et al.
patent: 3825984 (1974-07-01), Linko et al.

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