US2008105656A1PendingUtilityA1
Method for fabricating a nozzle
Est. expiryDec 15, 2023(expired)· nominal 20-yr term from priority
B24B 55/02B24B 19/14F05B 2230/10B23H 9/10F05B 2220/30B24B 19/009Y10T29/49996Y10T29/49432
48
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Claims
Abstract
A system for machining a component with complex contour. The machining system includes a coolant flow nozzle with an interior passage with a first portion having a first cross-sectional shape, and a second portion having a second cross-sectional shape, with the second cross-sectional shape selected so that fluid discharged from the nozzle has a selected cross-sectional shape. A method of fabricating a coolant flow nozzle with an interior passage that has a varying cross sectional shape.
Claims
exact text as granted — not AI-modified1 . A method for fabricating a nozzle including at least one piece, said method comprising:
forming at least a portion of an exit aperture in at least one piece of the nozzle, wherein the at least a portion of the exit aperture has a first cross-sectional shape configured to discharge a fluid with a shape that substantially matches a portion of a contour of a component to be fabricated using the nozzle; and forming at least a portion of an inlet aperture in the at least one piece of the nozzle, wherein the at least a portion of the inlet aperture has a second cross-sectional shape, and such that a fluid passage formed between the inlet and exit apertures transitions gradually between the first cross-sectional shape and the second cross-sectional shape.
2 . A method in accordance with claim 1 wherein forming at least a portion of an exit aperture further comprises forming at least a portion of the exit aperture using an electro-discharge machining process.
3 . A method in accordance with claim 1 wherein forming at least a portion of an inlet aperture further comprises forming the fluid passage using an electro-discharge machining process.
4 . A method in accordance with claim 1 wherein forming at least a portion of an exit aperture further comprises extending a portion of the exit aperture along an axial length of the nozzle such that the second cross-sectional shape remains substantially constant for a distance.
5 . A method in accordance with claim 1 further comprising forming a starter hole within a piece of stock material prior to forming the at least a portion of the exit aperture.
6 . A method in accordance with claim 1 further comprising coupling a first piece of the nozzle to a second piece of the nozzle.
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