Non-line of sight electro discharge machined part

US9561555B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9561555-B2
Application numberUS-201213729286-A
CountryUS
Kind codeB2
Filing dateDec 28, 2012
Priority dateDec 28, 2012
Publication dateFeb 7, 2017
Grant dateFeb 7, 2017

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A method of machining cooling holes in a component includes the steps of inserting an electro discharge machining guide that houses an electrode into an internal cavity of a component, and machining a cooling hole into a wall of the component with the electrode. A gas turbine engine component includes first and second spaced apart walls providing an internal cavity. The first wall has outer and inner surfaces. The inner surface faces the internal cavity. A cooling hole extends through the first wall from the inner surface to the outer surface. The cooling hole includes entry and exit openings respectively provided in the inner and outer surfaces. The exit opening includes a cross-sectional area that is smaller than a cross-sectional area of the entry opening.

First claim

Opening claim text (preview).

What is claimed is: 1. A method of machining cooling holes in a component comprising the steps of: inserting an electro discharge machining guide that houses an electrode into an internal cavity of a component; machining a cooling hole into a wall of the component with the electrode; and applying a non-conductive thermal barrier coating on the wall on a surface opposite the internal cavity, the applying step performed before the machining step. 2. The method according to claim 1 , wherein the guide includes first and second portions that are non-colinear with respect to one another. 3. The method according to claim 1 , wherein the component includes an airfoil, and the internal cavity is a cooling passage within the airfoil. 4. The method according to claim 3 , wherein the component is a turbine stator vane. 5. The method according to claim 4 , wherein the turbine stator vane is a doublet. 6. The method according to claim 1 , wherein the wall is obstructed by a structure on a side opposite the internal cavity.

Assignees

Inventors

Classifications

  • Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles · CPC title

  • B23H1/00Primary

    Electrical discharge machining, i.e. removing metal with a series of rapidly recurring electrical discharges between an electrode and a workpiece in the presence of a fluid dielectric · CPC title

  • Working turbine blades or nozzles · CPC title

  • Cooled platforms · CPC title

  • Moving electrode in the feed direction (B23H7/32 takes precedence) · CPC title

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What does patent US9561555B2 cover?
A method of machining cooling holes in a component includes the steps of inserting an electro discharge machining guide that houses an electrode into an internal cavity of a component, and machining a cooling hole into a wall of the component with the electrode. A gas turbine engine component includes first and second spaced apart walls providing an internal cavity. The first wall has outer and…
Who is the assignee on this patent?
United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification B23H1/00. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Feb 07 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).